FAA - PARTS MANUFACTURER APPROVAL (PMA ......FAA - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT...

-~.

FAA - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT

Higher Pl.anes 15001 Wal.den Rd., Suite 214B Montgomery, TX 77356

Name and Part No.

Part Name: Seal Disk P/N: HP867681-5

Part Name: Gasket P/N: HP868746-6

Approved Replacement

For

Allied Signal P/N: 867681-5


PMA No. PQ888SW

Suppl.ement No.

Approval Basis and Approved Design Data

Test and Computations per 14 CFR § 21.303 Dwg. No: HP867681-5 Rev: IR Date: 3/22/95 or later FAA approved revisions


1

Insta1lation El.igibil.ity

Allied Signal Turbo Prop Engine Models: TPE331-l-100F/ l-101B/l-101E/ l-101F/l-101Z/ l-151A/l-151G/ l-151K/2-201A/ 2-201C/2UA-203D/ 3U-303G/3UW-303G/ 3U-303V/3U-304G/ 5-251C/5-251K/ 5-252D/5-252K/ 5-252M/5-254K/ S-255K/6-251M/ 6-252B/6-252L/ 6-252M/6-252T/ 6A-251M/6A-252M/ 6-253B/8-401S/ 8-402S/8-403S/ 8-404S/8-406S/ 10-501C/10-501K/ 10-SOlM/10-SllC/ 10-SllK/10-SllM/ 10R-501C/10R-511C/ 10R-512C/10R-513C/ 10U-501G/10U-502G/ 10U-503G/10U-511G/ 10U-512G/10R-502C/ 10U-513G/10UA-501G/ 10UA-511G/10UF-501H/ 10UF-511H/10UF-512H/ 10UF-513H/10UG-513H/ 10UG-514H/ 10UGR-513H/ 10UGR-514H/ 10UR-513H/11U-601G/ 11U-611G/11U-602G/ 11U-612G/12UA-701G/ 12UAR-701G/ TSE331-3U-303N

Allied Signal Turbo Prop Engine Models: TPE331-1-100F/ l-101B/l-101E/ l-101F/l-101Z/

· l-151A/1-151G/ 1-151K/2-201A/ 2-201C/2UA-203D/ 3U-303G/3UW-303G/ 3U-303V/3U-304G/ 5-251K/5-252D/ 5-252K/S-252M/ 5-254K/5-255K/ 6-251M/6-252B/

of 4


Higher Planes 15001 Walden Rd., Suite 214B Montgomery, TX 77356

Name and Pkt No.

Part Name: Gasket P/N: HP867595-3


For


PMA No. PQ888SW

Supplement No.


Test and Computations per 14 CFR § 21.303 Dwg. No: HP867595-3 Rev: IR Date: 8/17/95 or"""Tater FAA approved revisions

1

Installation Eligibility

6-252L/6-252M/ 6-252T/6A-251M/ 6A-252M/6-253B/ 8-401S/8-402S/ 8-403S/8-404S/ 8-406S/10-501C/ 10-501K/10-501M/ 10-SllC/10-SllK/ 10-511M/10R-501C/ 10R-511C/10R-512C/ l0R-513C/10U-501G/ 10U-502G/10U-503G/ 10U-511G/10U-512G/ 10R-502C/10U-513G/ 10UA-511G/10UF-501H/ 10UF-511H/10UF-512H/ 10UF-513H/10UG-513H/ 10UG-514H/ 10UGR-513H/ 10UGR-514H/ 10UR-513H/11U-601G/ 11U-611G/11U-602G/ 11U-612G/331-25AA/ 25DA/25FA/43A/47A/ 25AB/25DB/43BL/ 331-55B/61A/5-252C/ 5A-252D/5-251C/ 12UA-701G/ 12UAR-701G/ 701H/702H/703H/704H/ 705H/706H/707H/708H/ TSE331-3U-303N

Allied Signal Turbo Prop Engine Models: TPE331-l-100F/ 1-101B/l-101E/ l-101F/l-101Z/ l-151A/1-151G/ 1-151K/2-201A/ 2-201C/2UA-203D/ 3U-303G/3UW~303G/ 3U-303V/3U-304G/ 5-251K/5-252D/ 5-252K/5-252M/ 5-254K/5-255K/ 6-251M/6-252B/ 6-252L/6-252M/ 6-252T/6A-251M/ 6A-252M/6-253B/ 8-401S/8-402S/ 8-403S/8-404S/ 8-406S/10-501C/ 10-501K/10-501M/ 10 -SllC/10-SllK/

of -1



N~ and Part No.

Part Name: Retainer P/N: HP865057-7


For


PMA No. PQ888SW

Supplement No.



1


10-SllM/lOR-SOlC/ 10R-511C/10R-512C/ 10R-513C/10U-501G/ 10U-502G/10U-503G/ lOU-511G/lOU-512G/ 10R-502C/10U-513G/ 10UA~511G/10UF-501H/ 10UF-511H/10UF-512H/ l0UF-513H/10UG-513H/ l0UG-514H/ 10UGR-513H/ 10UGR-514H/ 10UR-513H/11U-601G/ 11U-611G/11U-602G/ 11U-612G/331-25AA/ 25DA/25FA/43A/47A/ 25AB/25DB/43BL/55B/ 61A/5-252C/5A- 252D/ 5-251C/12UA-701G/ 12UAR-701G/701H/ 702H/703H/704H/705H/ 70 6H/707H/708H/ TSE331-3U-303N

Allied Signal Turbo Prop Engine Models: TPE331-l-l00F/ l-101B/1-101E/ 1-101F/l-101Z/ l-151A/l-151G/ l-151K/2-201A/ 2-201C/2UA-203D/ 3U-303G/3UW-303G/ 3U-303V/3U-304G/ 5-251C/5-251K/ 5-252D/l0UA-501G/ 10UA-511G/10UF-501H/ lOUF-511H/10UF-512H/ 10UF-513H/10UG-513H/ 10UG-514H/ 10UGR-513H/ 10UGR-514H/ 10UR-513H/11U-601G/ 11U-611G/11U-602G/ 11U-612G/12UA-701G/ 12UAR-701G/ TSE331-3U-303N

--------------------------------End of Listing-----------------------------

NOTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA·.

of 4

--~



Name and Part No.


For

PMA No. PQ888SW

Supplement No.

Approval Basis and.Approved Design Data

1


ij_ ~ D~te: 5/~9/0.'l, Edwin G. Cuevas, ProJect Engineer,

Special Certification Office, ASW-190

Date: ~/lfl/'ig Robert A. Robina

Attachment to PMA letter dated ~/,o/~a

Manager, Manufacturing Inspection District Office, MID0-43

Page-! of 4


Higher Pl.anes 15001 Wal.den Rd., Suite 214B Montgomery; TX 77356

Name and Part No.

Part Name: Bolt· P/N: 232-20268-503HP

Part Name: Bearing P/N: 45-12216-lHP

Part Name: Bearing P/N: 232-20260-lHP


For

Learjet P/N: 232-20268-503

Learjet P/N: 45-12216-1

Learjet P/N: 232-20260-1

PMA No. PQ888SW

Suppl.ement No. Date: 07/02/98

Approval. Basis and Approved Design Data

Test and computations per 14 CFR § 21.303 Dwg. No: 232-20268-503HP Rev: IR Date: 3/08/97 or later FAA approved revisions

Test and Computations per 14 CFR § 21.303 Dwg. No: 45-12216-lHP Rev: IR Date: 8/2 6/97 or later FAA approved revisions

Test and Computations per 14 CFR § 21.303 Dwg. No: 232-20260-lHP Rev: IR Date: 3/08/97 or later FAA approved revisions

2

Installation Eligibil.ity

Learjet Inc. Models: 35, 35A {C-21A), 36, 36A, 55, 55B, SSC Dassault Aviation Models: Fan·Jet Falcon, Fan.Jet Falcon Series C, D, E, F Modified per STC: SA2568WE Sabreliner Corp. Models: NA-265-80 Raytheon Aircraft Co. Models: HS.125 Series 700

Learjet Inc. Models: 35, 35A {C-21A), 36, 36A, 55, 55B, SSC Ratheon Aircraft Co. Models: HS.125 series 700

Dassault Aviation Models: Fan Jet Falcon, Fan Jet Falcon Series c, D, E, F Modified per STC: SA2568WE Sabreliner Corp. Models: NA-265-80

--------------------------------End of Listing-----------------------------

NOTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

Page 1 of 2



Name and Part No.


For

PMA No. PQ888SW

Supplement No. Date: 07/02/98


2


~J... ~ Date: b/li/9<;; ~ j~Date: ?h/92 _E_d_w_i_n_G_._C_u_e_v_a_s_, _P_r_o_j_e_c_t_E_n.,_g_i_n_e~~-r-,-=-- Robert A. Robino

Special Certification Office, Manager, Manufacturing Inspection ASW-190 District Office, MID0-43

Attachment to PMA letter dated 06/10/98.

Page 2 of 2



Name and Pa:rt No.

Part Name: Bushing P/N: 232-20426-lHP


For

Learjet P/N: 232-20426-1

PMA. No. PQ888SW



Test and Computations per 14 CFR § 21.303 Dwq. No: 232-20426-lHP Rev: IR Date: 3/08/97 or later FAA approved revisions

3


Learjet Inc. Models: 35, 35A {C-21A), 36, 36A, 55, 55B, SSC Dassaul.t Aviation Models: Fan Jet Falcon, Fan Jet Falcon Series c, D, E, F Modified per STC: SA2568WE Sabreliner Co:cp. Models: NA-265-80 Raytheon Aircraft Co. Models: HS.125 Series 700

--------------------------------End of Listing-----------------------------

NOTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA;_PMA.

Edwin G. Cuevas, Project Engineer, Special Certification Office, ASW-190

~ Jt:4/bvoate: 1,MJ Robert A. Robino Manager, Manufacturing Inspection District Office, MID0-43

Attachment to PMA letter dated 06/10/98.

Page 1 of 1


HIGHER PLANES 15001 WALDEN RD. STE 214B MONTGOMERY, TEXAS 77356

Name and Part No.

Part Name: Bearing-Sleeve P/N: HP865542-5


For


PMA No. PQ880SW



4



Allied Signal (Garrett) Engine Models: TPE 331-5-251C/-5-251K/-5-252C/-5-255K/-5B-252D/-5AB-252D/-10P-511D/-10GP-511D/-10T-513K/-10T-515K/-10T-516K/-10T-517K/-12B-701A/-12B-702A/-6-251M/-6A-251M/-8-401S/-8-402S/-1-151A/-1-151G/-2-201A/-5-252D/-5-252K/-5-252M/-5-254K/-6-252B/-6-252M/-6A-252M/-1-100F/-1-101B/-1-101E/-1-101F/-1-101Z/-2UA-203D/-3U-303V/-10-501C/-10-511C/-10R-501C/-10R-502C/-10R-511C/-10R-512C/-10R-513C/-151K/-3U-303G/-3UW-303G/-3U-304G/-5A-252D/-6-253B/-6-252L/-6-252T/-10-501K/-10-511K/-10-501M/-10-511M/-10U-501G/-10U-511G/-10U-502G/-10U-512G/10U-503G/-10U-513G/-10UA-511G/-10UF-501H/-10UF-511H/-10UF-512H/-10UF-513H/-10UF-514H/-10UF-515H/-10UF-516H/-10UG-513H/-10UG-514H/-10UG-515H/-10UG-516H/-10UGR-513H/-10UGR-514H/-10UGR-515H/-10UGR-516H/-10UR-513H/-10UR-516H/-11U-601G/-11U-611G/-11U-602G/-11U-612G/-12UA-701G/-12UAR-701G/-12UAR/-701H/-12UAR-702H/-12UAR-703H/-12UAR-704H/-

Page 1 of2

·"\

''\


HIGHER PLANES 15001 WALDEN RD. STE 214B MONTGOMERY, TEXAS 77356

Name and Part No.


For

PMA No. ;. PQ8!30S_W

Supplement No.

Date: 09/16/98


4


703H/-12UAR-704H/-12UAR-705H/-12UAR-706H/-12UAR-707H/-12UAR-708H/-2-201C/-8-403S/-8-404S/-8-406S/-10T-511D/-10T-511K/-10T-512K/-12UHR-701G/-12UHR-701H/-12UHR-702H/-12UHR-703H/-12UH-704H/l4A-801Y/-14B-801Y/-14A-801Z/-14F-801L/-14GR-801H/-14GR-802H/-14GR-803H/-14GR-804H/-14GR-805H/-14GR-806H/-14GR-807H/-14GR-901H/-14HR-801H/-14HR-802H/-14HR-803H/-14HR-804H/-14HR-805H/-14HR-806H/-14HR-807H/-14HR-901H/-14GR-801E/-15AW-801N/-15AW-801T

--------------------------------End of Listing-------------------------


£J_ ~ Date: q, /~.:'1 Jqg Project Engineer, Special Certification Office, ASW-190

Attachment to PMA letter dated: 06/10/98.

MID0-43

Page 2 of2

.. ~

FAA. - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT

HIGHER PLANES 15001 WALDEN RD., STE 214B MONT~MERY, TEXAS , .7 7 356

Name and Part No.



For


PMA No. PQ880~W.

Supplement No. ___ 5 ___ _ Date: 09/16/98


Test & Computations per 14 CFR § 21.303 Dwg. No: HP869615 Rev: IR Date: 12/13/97 or later FAA approved revisions

.•


Allied Signal (Garrett) Engine Models: TPE 33 l-25AA/-25DA/-25F A/-43A/-47 A/-25AB/-25DB/-43BL/-55B/-61A/-6-251M/-6A-25lM/-8-401 S/-8-402S/-l-15 IA/-l-151 G/-2-20IA/-5-252D/-5-252K/-5-252M/-5-254K/-6-252B/-6-252M/-6A-252M/-l-lOOF/-l-l01B/-1-101E/-l-101F/-1-l01Z/-2UA-203D/-3U-303V/-10-501 C/-10-511C/-10R-501 C/-10R-502C/IOR-511 C/-lOR-512C/-lOR-513C/-l-151K/-3U-303 G/-3UW-303G/-3U-304G/-5A-252D/-6-253B/-6-252L/-6-252T/-I0-501K/-l0-511K/-l0-501M/-10-511M/-10U-501G/-10U-511G/-10U-502G/-IOU-512G/10U-503G/-10U-513G/-10UA-511G/-10UF-501H/-10UF-511H/-IOUF-512H/-I0-513H/-10UF-514H/-10UF-515H/-IOUF-516H/-I0UG-513H/-1 OUG-514H/-10UG-515H/-I0UG-516H/-10UGR-513H/-10UGR-514H/-10UGR-515H/-10UGR-516H/-10UR- · 513H/-10UR-516H/-11U-60 I G/-11 U-611 G/-11 U-602G/-11U-612G/-12UA-701 G/-12UAR-701 G/-12UAR-701H/-12UAR-702H/-12UAR-703H/-12UAR-704H/-12UAR-705H/l2UAR-706H/-12UAR-707H/-12UAR-708H/-8-403S/-8-404S/-8-406S/-12B-701 A

Page I of 4

.~

FAA - PARTS MANUFACTURER APPROVAL (PMA) SUPP.LEMENT

HIGHER PLANES 15001 WALDEN RD. , STE 214B MONTGOMERY, TEXAS, 77356

Name and Part No.



For

Allied Signal P /N: 8 69615-2

PMA No. fQ880SW



5


-·


Allied Signal (Garrett) Engine Models: TPE 331-25AA/-25DA/-25F A/-43A/-47 A/-25AB/-25DB/-43BL/-55B/-61A/-6-251M/-6A-251M/-8-401S/-8-402S/-1-151A/-l-151 G/-2-201Ai-5-252D/-5-252K/-5-252M/-5-254K/-6-252B/-6-252M/-6A-252M/-1-100F/-1-101B/-1-10IE/-l-101F/-1-101Z/-2UA-203D/-3U-303V/-10-501C/-10-511 C/-1OR-501 C/-1 OR-502C/lOR-5 l l C/-10R-512C/-10R-513C/-1-151K/-3U-303G/-3UW-303G/-3U-304G/-5A-252D/-6-253B/-6-252L/-6-252T/-10-501K/-l0-5 l 1K/-10-501M/-10-511M/-10U-501G/-10U-511G/-10U-502G/-JOU-512G/10U-503G/-10U-513G/-10UA-511G/-10UF-501H/-10UF-511H/-10UF-512H/-10-513H/-10UF-514H/-10UF-515H/-10UF-516H/-10UG-513H/-10UG-514H/-10UG-515H/-1 OUG-516H/-1 OUGR-513H/-10UGR-514H/-10UGR-515H/-l0UGR-516H/-I0UR- · 513H/-I0UR.-516H/-11U-601 G/-11 U-611 G/-11 U-602G/-11 U-612G/-12UA-701 G/l2UAR-701G/-12UAR-701H/-12UAR-702H/-12UAR-703H/-12UAR-704H/-12UAR-705H/-12UAR-706H/-12UAR-707H/l2UAR-708H/-8-403S/-8-404S/-8-406S/-12B-701A

Page 2 of 4



Name and Part No.

Part Name: Bearing -Sleeve P/N: HP869616-1


For


PMA No. PQ880SW



5



Allied Signal (Garrett) Engine Models: TPE 3 31-25 AA/-25DA/-25F A/-43A/-47 A/-25AB/-25DB/-43BL/-55B/-61A/-6-25 IM/-6A-25 l M/-8-40 I S/-8-402S/-l-151 A/-l-l 5 l G/-2-201A/-5-252D/-5-252K/-5-252M/-5-254K/-6-252B/-6-252M/-6A-252M/-1-IOOF/-1-101B/-l-101E/-l-101F/-l-101Z/-2UA-203D/-3U-303V/-10-501 C/-10-511 C/-IOR-501 C/-IOR-502C/-10R-51 IC/-10R-512C/IOR-513C/-1-151K/-3U-303G/-3UW-303G/-3U-304G/-5A-252D/-6-253B/-6-252L/-6-252T/-I0-501K/-10-511K/-10-501M/-10-511M/IOU-501G/-10U-511 G/-10U-502G/-10U-512G/10U-503G/-10U-513G/-10UA-511G/-10UF-50IH/-10UF-511H/-10UF-512H/-10-513H/-10UF-514H/-10UF-515H/-10UF-516H/-10UG-513H/-I0UG-514H/-10UG-515H/-IOUG-516H/-10UGR-513H/-IOUGR-514H/-IOUGR-515H/-10UGR-516H/-10UR-513H/-I0UR-516H/-11U-601G/-l 1U-6I l G/-11 U-602G/-l 1 U-612G/-12UA-701 G/-I2UAR-701G/-12UAR-701H/-I2UAR-702H/-l2UAR-703H/-12UAR-704H/-12UAR-705H/-I2UAR-706H/-12UAR-707H/-l2UAR-708H/-8-403 S/-8-404S/-8-406S/-12B-701A

Page 3 of 4



Name and Part No.



For


PMA No. PQ880SW

Supplement No. ~=5 __ _ Date: 09/16/98




Allied Signal (Garrett) Engine Models: TPE 331-25AA/-25DA/-25FA/-43A/-47A/-25AB/-25DB/-43BL/-55B/-61A/-6-251M/-6A-251M/-8-401S/-8-402S/-1-151A/-1-151G/-2-201A/-5-252D/-5-252K/-5-252M/-5-254K/-6-252B/-6-252M/-6A-252M/-1-100F /-l-l 01B/-1-101E/l-l01F/-l-101Z/-2UA-203D/-3U-303V/-10-501C/-l0-511C/-l0R-501C/-10R-502C/-10R-511C/-10R-512C/-10R-513C/-l-151K/-3U-303G/-3UW-303G/-3U-304G/-5A-252D/-6-253B/-6-252L/-6-252T/-l 0-501K/-10-511K/-10-501M/-10-511M/-10U-501G/-10U-511G/-10U-502G/-l OU-512G/1 OU-503G/-l OU-513G/-10UA-5 l l G/-10UF-501H/-10UF-511H/-10UF-512H/-10-513H/-10UF-514H/-10UF-515H/-10UF-516H/-1 OUG-513H/-l OUG-5 l 4H/-1 OUG-515H/-1 OUG-516H/-l OUGR-513H/-l OUGR-514H/-10UGR-515H/-10UGR-516H/-1 OUR-513H/-1 OUR-516H/-11 U-601 G/-l 1 U-61 l G/-11 U-602G/-11 U-612G/-12UA-701 G/-12UAR-701 G/-12UAR-701H/-12UAR-702H/-12UAR-703H/-12UAR-704H/-12UAR- . 705H/-12UAR-706H/-l2UAR-707H/-12UAR-708H/-8-403S/-8-404S/-8-406S/-12B-70 IA

--------------------------------End of Listing-----------------------------

NOTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specifications be handled in the same manner as that for an original FAA-PMA.

tel_ ~ Date: ~ {~'=» /g '6 Project Engineer, Special

Certification Office, ASW-190

Attachment to PMA letter dated: 06/10/98.

Page 4 of 4

( ) )

Federal Aviation Administration - PAR'.1. ... .a.".l:ANUFACTURER APPROVAL (PMA) SUPPLEMENT Higher Planes 15001 Walden Road, Suite 214B Montgomery, TX 77356

PART NAME

Cable, Assy.

Cable, Assy.

Cable, Assy.

Cable, Assy.

Part Number

HP2411660 -13

HP2411660 -15

HP2411660 -18

HP2411660 -34

Approved Replacement For

Learjet 2411660-13

Learjet 2411660-15

Learjet 2411660-18

Learjet 2411660-34

APPROVAL BASIS AND APPROVED

DESIGN DATA

Test and Computations per 14 CFR § 21. 303 Dwg. No: HP2411660 Rev: IR Date: 7/16/97 or later FAA approved revisions Test and Computations per 14 CFR § 21. 303 Dwg. No: HP2411660 Rev: IR Date: 7/16/97 or later FAA approved revisions Test and Computations per 14 CFR § 21. 303 Dwg. No: HP2411660 Rev: IR Date: 7/16/97 or later FAA approved revisions Test and Computations per 14 CFR § 21. 303 Dwg. No: HP2411660 Rev: IR Date: 7/16/97 or later FAA approved revisions

PMA No. PQ880SW Supplement No. 6 Revision No. ACO PMA Project Numbe~: PM5543SC-T

INSTALLATION ELIGIBILITY (MAKE)

Learjet

Learjet

Learjet

Learjet

INSTALLATION ELIGIBILITY (MODEL)

24, 24A, 24B, 25B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 31, 31A, 35, 35A (C-21A), 36, 36A

24, 24A, 24B, 25B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 31, 31A, 35, 35A (C-21A), 36, 36A

24, 24A, 24B, 25B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, .25B, 25C, 25D, 25F,35, 35A (C-21A), 36, 36A

24, 24A, 24B, 25B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F,31, 31A, 35, 35A (C-21A), 36, 36A

---------------------------------------------------End of Listing-------------------------------------------NOTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes {reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specificatio andled in the same manner as that for an original FAA-PMA.

Date: gan Brookfield, Project Engine r

Spe ial Certification Office, ASW-190

This supplement is attached to your FAA-PMA approval letter dated 6/10/98.

Date: ?- 9-9'1

District Office,

Page 1 of 1

) ) ) FAA - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT

HIGHER PLANES 15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART PART NAME NUMBER

Bearing, Ball Annular



226433HP

226538HP

207460HP

APPROVED REPLACEMENT FOR

Intertechnique P/N:226433

Intertechnique P/N:226538

Intertechniq ue P/N:207460

APPROVAL BASIS AND APPROVED DESIGN DATA

Test and Computation per 14 CPR § 21.303. Dwg: 226433HP, Rev: IR, Dated: 11/10/98, or later FAA approved revisions

Test and Computation per 14 CPR § 21.303. Dwg: 226538HP, Rev: IR, Dated: 11/10/98, or later FAA approved revisions

Test and Computation per 14 CFR § 21.303. Dwg: 207460HP, Rev: IR, Dated: 11/10/98, or later FAA approved revisions

PMA No. PQ880SW Suppleni'"ent No. 7

Revision No. DateJUL 2] QS9

INSTALLATION INSTALLATION ELIGIBILITY ELIGIBILITY (MAKE) _(M_O_D_EL_) ____ _

Dassault

Dassault

Raytheon

Israel Aircraft Industries, Ltd.

Fan Jet Falcon, Fan Jet' Falcon Series C, D, E, F, Mystere-Falcon 20-C5,-D5, -ES, -FS, Mystere-Falcon 50, Mystere-Falcon 200

Fan Jet Falcon, Fan Jet Falcon Series C, D, E, F, Mystere-Falcon 20-C5,-D5, -ES, -FS, Mystere-Falcon 50, Mystere-Falcon 200

BH.125 Series 600, HS.125 Series 600, HS.125 Series 700, BAe.125 Series 800, BAe.125 Series 1000, Hawker 800, Hawker 1000, Hawker 800XP

1124, 1124A

, -----------------------------------------------------·------------------------------End of~isting--------------------------------------------------------------------------------

Page 1 of2

) ) )


HIGHER PLANES 15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART PART NAME NUMBER

APPROVED REPLACEMENT FOR


PMA No. PQ880SW Supplement No. 7

Revision No. DateJUL 2 1 1999

INSTALLATION INSTALLATION ELIGIBILITY ELIGIBILITY (MAKE) _(M_O_D_EL_) ____ _

NOTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original F AA-PMA.

Ed Cuevas Project Engineer, Special Certification Office, ASW-190

(;,/30/99 • I

Date Robert A. Robina, Manager, Manufacturing Inspec I

SW-MID0-43

This Supplement is an attachment to your FAA-PMA approval letter dated 06/10/98.

Page 2 of2

1-,.,-99 Date

,.,._--..,

Page 1 of 13

FEDERAL A VIA TI ON ADMINISTRATION - PARTS MANUFACTURING APPROVAL

Higher Planes 15001 Walden Road, Suite 214B Montgomery, Texas 77356

APPROVED REPLACEMENT

PART NUMBER

FOR PART APPROVAL BASIS AND APPROVED PART NAME

Valve-Seat

NUMBER DESIGN DATA

867905-lHP 867905-1 Test & Computation . per 14 CFR §21.303, DWG No: 867905-lHP REV: A Date: 7 /15/99 or later FAA approved revisions

PMA NO. PQ880SW SUPPLEMENT NO: 8

DATE: DEC 1 7 \999

MAKE ELEGIBILITY

AlliedSignal (Garrett)

MODEL ELEGIBILITY

TPE 331-1-lOOF/-l-lOIB/l-l O 1E/-1-101 F/-1-1 OlZ/-1-15 lA/-1-151 G/-1-1 S lK/-2-20 IA/-2-201 C/-2UA-203D/-3U-303G/-3 UW-303G/-3 U-303V/-3U-304G/-5-25 l K/-5-251 C/-5-252M/-5-252K/-5-254K/-5-252C/-5-255KJ-5-252D/-5B-252D/-5A-252D/-5AB-252D/-6-251M/-6-252M/-6A-252M/-6-252B/-6-253B/-6A-25 lM/-8-40 l S/-8-402S/-8-403S/-8-422S/-8-423S/l0N-511S/-10N-512S/-10N-514S/-10N-515S/-10N-531S/-l0N-532S/-10N-534S/-l ON-535S/-l OUF-50 lH/-l OUF-5 l lH/-l OUF-512H/-IOUF-513H/-10UR-513H/-10UG-513H/-l OUGR-513H/-l OUG-514H/-l OUGR-514H/-l OUF-514H/-l OUF-515H/l OUF-5 l 6H/-l OUG-515H/l OUGR-515H/-l OUG-516H/-l OUGR-516H/-10U-50 lG/-1 OU-502G/-l OU-5 l l G/-l OU-512G/-l OUR-5 l 6H/-l OUR-5 l 4H/-l 0-50 lM/-10-511 M/-l OT-Sl lM/-10-SOIC/-lOR-501 C/-1 OR-502C/-l 0-511 C/-l OR-5 l l C/-l OR-512C/-l OR-513C/-l 0-501KJ-10-5 l 1KJ-10U-503G/-l OU-513G/-l OUA-5 l l G/-l OT-51 lD/-l OP-511D/-10GT-511D/-10GP-51 ID/-10A V-511 B/-l lU-60 l G/-11 U-602G/-l l U-6l l G/-l lU-612G/-12B-701A/-l 2B-702A/-l2UAR-701H/-l 2UAR-702H/-12UAR-703H/-12UAR-704H/-l 2UAR-705H/-12UAR-706H/-12UAR-707H/-l 2UAR-708H/-12UHR-701H/-12UHR-702H/-12UHR-703H/l2UHR-704H/-12UHR-705H/-l 2UHR-6H/-12 UHR-707H/-l 2-UHR-708H/I2UHR-701G/-12UA-701G/-12UAR-701G/-12JR-701C TSE-33 l-3U-303N

of 13

FEDERAL AVIATION ADMINISTRATION -PARTS MANUFACTURING APPROVAL

-~ Higher Planes PMA NO. PQ880SW 15001 Walden Road, Suite 214B SUPPLEMENT NO: 8 Montgomery, Texas 77356 DATE: DEC 1 7 1999


PART FOR PART APPROVAL BASIS AND APPROVED MAKE PART NAME NUMBER NUMBER DESIGN DATA ELEGIBILITY MODEL ELEGIBILITY

Bushing 3101703-lHP 3101703-1 Test and Computation AlliedSignal TPE 331-l lU-60lG/-l lU-

per 14 CFR §21.303, (Garrett) 6020/-I I U-61 IG/-l I U-612G/-l2B-701A/-l2B-

DWG No: 3101703 702A/-l 2UAR-70 I HI-REV: lR 12UAR-702H/-12UAR-

Date: 2/17 /99 703H/-12UAR-704H/-

or later FAA approved revisions l 2UAR-705H/-12UAR-706H/-12UAR-707H/-l 2UAR-708H/-l 2UHR-70 I H/-12UHR-702HI-12UHR-703H/-12UHR-704H/-12UA-70 l GI-I 2UAR-701G/-12JR-701 C

Bushing 3101703-2HP 3101703-2 Test and Computation AlliedSignal TPE 331-l lU-60IG/-l lU-

per 14 CFR §21.303, (Garrett) 602G/-l l U-61 lG/-l l U-6 l2G/-l2B-701A/-12B-

DWGNo: 3101703 702A/-l 2UAR-70 I HI-REV: lR 12UAR-702H/-12UAR-

Date: 2/17 /99 703H/-12UAR-704H/-

or later FAA approved revisions l 2UAR-705H/-12UAR-706H/-12UAR-707H/-

'~ I 2UAR-708H/-l 2UHR-701 H/-l 2UHR-702H/-12UHR-703H/-12UHR-704H/-12UA-701G/-I 2UAR-70lG/-12JR-701 C

BUSHING 31 O 1703-3HP 3101703-3 Test and Computation AlliedSignal TPE 331-l lU-601G/-l lU-

per 14 CFR §21.303, (Garrett) 602G/-l 1 U-61 lG/-l l U-612G/-12B-701A/-12B-

DWG No: 3101703 702A/-l 2UAR-70 I H/-REV: lR l 2UAR-702H/-12UAR-

Date: 2/17 /99 703HI-I2UAR-704HI-

or later FAA approved revisions l 2UAR-705H/-12UAR-706H/-l 2UAR-707H/-12UAR-708H/-l 2UHR-701 H/-12UHR-702H/-I 2UHR-703H/-l2UHR-704H/-12UA-701G/-12UAR-70 I G/-12JR-70 IC

13USJ-IING 310 l 703-4IIP 3101703-4 Test and Computation AlliedSignal TPE 331-1-lOOf./-l-!OlB/-

per 14 CFR §21.303, (Garrett) l-10 lE/-1-10 lF/-1-1 OIZ/-1-15 IA/-1-151 G/-1-l SlK/-2-

DWG No: 3101703 20 I A/-2-201 C/-2UA-203D/-REV: lR 3U-303G/-3UW-303G/-3U-

Date: 2/17/99 303V/-3U-304G/-6-25 l Ml-

or later FAA approved revisions 6-252M/-6A-252M/-6-252B/-6-253B/-6A-251M/-lOAV-51 lB TSE-33 l-3U-303N

of 13

FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURING APPROVAL

--~ Higher Planes 15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART NAME

BUSHING

BUSHING

~ BUSHING

_____ ,/

PART NUMBER

3101703-SHP

310 l 703-6HP

3101703-7HP

APPROVED REPLACEMENT FOR PART APPROVAL BASIS AND APPROVED NUMBER DESIGN DATA

3101703-5 Test and Computation per 14 CFR §21.303, DWGNo: 3101703 REV: IR Date: 2/ 17 /99 or later FAA approved revisions

31 O 1703-6 Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: ·2/17/99 or later FAA approved revisions

31 O 1703-7 Test and Computation per 14 CFR §21.303, DWGNo: 3101703 REV: IR Date: 2/17/99 or later FAA approved revisions


DATE: OEC 1 7 \999

MAKE ELEGIBILITY



A lliedS ignal (Garrett)

MODEL ELEGIBILITY

TPE 331-1-lOOF/-l-lOlB/l-lO lE/-1-10 l F/-1-1 OlZ/-1-151 A/-1-151 G/-l-l 5 lK/-2-20 lA/-2-201 C/-2UA-203D/-3 U-303G/-3UW-303G/-3 U-303V/-3U-304G/-6-25 l M/-6-252M/-6A-252M/-6-252B/-6-253B/-6A-251M/lOAV-51 lB TSE-33 l-3U-303N

TPE 331-1-lOOF/-l-lOlB/l-lO l E/-1-10 lF/-1-1 OlZ/-l-15 lA/-l-151 G/-1-15 lK/-2-201N-2-201 C/-2UA-203D/-3U-303G/-3UW-303G/-3U-303V/-3U-304G/-6-25 lM/-6-252M/-6A-252l'vU-6-252B/-6-253B/-6A-25 l M/-l OA V-51 lB TSE-33 l-3U-303N

TPE 331-8-40 l S/-8-402S/l OUF-50 lH/-l OUF-5 l lH/lOUF-512H/-l OUF-5 l3H/-10UR-513H/-l OUG-513H/lOUGR-513H/-lOUG-5 l 4H/-l OUGR-5 l 4H/-l OUF-514H/-l OUF-515H/l OUF-5161--I/-l OUG-5 l 5H/l OUGR-515H/- l OUG-5161--I/-l OUGR-5 l 6H/-l OUSO 1 G/-1 OU-5020/-1 OU-5 l l G/- l OU-512G/-l0-501M/-10-5 l lM/-lOT-5l lM/-10-501C/-10R-50 l C/-1 OR-502C/-l 0-511 C/-l OR-511 C/- l OR-5 l 2C/- l OR-5 I 3C/-l 0-501 K/-I 0-511 K/- l OU-503G/-l OU-513G/-IOUA-5 l l G/-l OUR-5.l 6H

,---.,._\

Page 4 of 13



PART NAME

BUSHING

PART NUMBER

3101703-8HP


31 o 1703-8 Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/1 7 /99 ~r later FAA approved revisions


DATE: DEC 1 7 1999

MAKE ELEGIBILITY


MODEL ELEGIBILITY

TPE 331-8-401 S/-8-402S/-10UF-501H/-10UF-511H/-10UF-512H/-l OUF-513H/-10UR-513H/-10UG-513H/-10UGR-513H/-10UG-514H/-10UGR-514H/-1 OUF-~ l 4H/- l OUF-51 SH/l OUF-5 l 6H/- l OUG-515H/l OUGR-S l SH/-l OUG-5 l 6H/-l OUGR-5 l 6H/-l OUSO 1 G/-1 OU-5020/-1 OU-5 l l G/-l OU-512G/-10-SOlM/-10-Sl lM/-lOT-Sl lM/-10-SOlC/-lOR-501 C/-1 OR-502C/-l 0-511 C/- l OR-511 C/-l OR-512C/-10R-513C/-10-501K/-10-511K/-10U-5030/-1 OU-513G/-10UA-511G/-l OUR-516H

,,.,.--.,,,

1

BUSHING 3101703-9HP 31 o 1 703-9 Test and Computation per 14 CFR §21.303, DWGNo: 3101703 REV: IR


TPE 331-8-401 S/-8-402S/l OUF-501H/-l OUF-5 l l H/-1 OUF-5 l 2H/-l OUF-513H/-10UR-513H/-10UG-513H/-10UGR-513H/-I0UG-514H/-10UGR-514H/-10UF-514H/-l OUF-5 l SH/-10UF-516H/-1 OUG-515H/l OUGR-S l SH/-l OUG-516H/-10UGR-516H/-10U-501 G/-1 OU-5020/-1 OU-511 G/-1 OU-512G/-10-

BUSHING 3101703-lOHP 3101703-10

Date: 2/17/99 or later FAA approved revisions

I

Test and Cornputation·--per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/17/99 or later FAA approved revisions

A I liedSignal (Garrett)

50 l M/-10-511 M/-l OT-Sl lM/-10-SOlC/-lOR-501 C/-1 OR-502C/-l 0-511 C/- lOR-511 C/-lOR-512C/-10R-513C/-10-501 K/-10-S l 1K/-10U-5030/-1 OU-5130/-1 OUA-5 l l G/-l OUR-5 l 6H

TPE 331-1-lOOF/-l-lOlB/l-l O I E/-1-101F/-1-101 Z/-1-151 A/- l - l 5 l G/-l-15 lK/-2-20lA/-2-201 C/-2UA-203D/-3U-303G/-3UW-303G/-3U-303V /-3 U-304G/-S-252D/-5B-252D/-5A-252D/-5AB-

. 252D/-6-251M/-6-252M/-6A-252M/-6-252B/-6-2.53B/-6A-251 M/-1 OT-S l lD/-l OP-5110/-l OGT-S l lD/-lOGP-5110/-lOAVS l lB/ TSE-33 l-3U-303N

of 13


,~ Higher Planes 15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART NAME

BUSHING

BUSHING

BUSHING

BUSHING

BUSHING

PART NUMBER

3101703-1 IHP

3101703-12HP

3 IOI 703-l3HP

3 IOI 703-14HP

3101703-ISHP

APPROVED REPLACEMENT FOR PART APPROVAL BASIS AND APPROVED NUMBER DESIGN DATA ,

31 o 1703-11 Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: lR

3101703-12

3101703-13

3101703-14

3101703-15

Date: 2/17 /99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/17 /99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: lR Date: 2/17/99

· or later FAA approved revisions

Test and Computation per 14 CFR §21.3Q3, DWGNo: 3I017el3 REV: lR Date: 2/17/99 or later FAA approved revisions

Testand Computation per 14 CFR §21.303, DWGNo: 3101703 REV: IR Date: 2/17 /99 or later FAA approved revisions


DATE: DEC 1 7 1999

MAKE ELEGIBILITY






MODEL ELEGIBILITY

TPE 331-1-IOOF/-1-lOIB/l-l O 1 E/-1-10 I F/-1-1 OIZ/-l-15 IN-l-151 G/-1-151 K/-2-20 I N-2-20 I C/-2UA-203D/-3U-303G/-3UW-303G/-3U-303V /-3 U-304G/-5-252D/-5B-252D/-5A-252D/-5AB-252D/-6-25 I M/-6-252M/-6A-252M/-6-252B/-6-253B/-6A-25 I M/-1 OT-51 ID/-1 OP-51 ID/-l OGT-5 l lD/-l OGP-51 lD/- l OA V-51 lB/ TSE-33 l-3U-303N

TPE 331-1-IOOF/-1-lOlB/l-l 01E/-1-101 F/-1-10 lZ/-l-15 lN-1-151 G/-l-15 lK/-2-20lN-2-201 C/-2UA-203D/-3 U-303G/-3UW-303G/-3 U-303V/-3U-304G/-5-252D/-5B-252D/-5A-252D/-5AB-252D/-6-25 l M/-6-252M/-6A-252M/-6-252B/-6-253B/-6A-25 l M/-1 OT-51 ID/-l OP-5 l lD/-IOGT-5 l lD/-l OGP-511D/-l OA V-51 lB/ TSE-33 l-3U-303N

TPE 331-1-lOOF/-l-lOIB/l-l O 1E/-1-101F/-1-101Z/-l-151N-l-151 G/-l-l 51 K/-2-20lA/-2-201 C/-2UA-203D/-5-252D/-5B-252D/-5A-2520/-5AB-252D/-l OT-51 lD/-l OP-5 l lD/-l OGT-5 l lD/-lOGP-51 lD

TPE 331-1-lOOF/-l-lOIB/l-l O 1 E/-1-10 I F/-1-101Z/-ll 51N-l-l 51 G/-l-l51K/-2-20 I A/-2-201 C/-2UA-203D/-5-252D/~5B-252D/-5A-252D/-5AB-252D/-l OT-5 l lD/-l OP-5110/-IOGT-51 ID/- l OGP-51 lD

TPE 331-1-IOOF/-l-lOIB/l-l O I E/-1-10 I F/-l-1 OIZ/-ll 51A/-l-l 51 G/-l-151K/-2-20 I N-2-20 I C/-2UA-203D/-5-252D/-5B-252D/-5A-252D/-SAB-252D/- I OT-5 l lD/-I OP-51 lD/-l OGT-5110/-1 OGP-51 lD

of 13


/--..,, Higher Planes 15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART NAME

BUSHING

BUSHING

BUSHING


PART FOR PART APPROVAL BASIS AND APPROVED NUMBER NUMBER DESIGN DATA

31 o l 703- l 6HP 31 o 1703-16 Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/17 /99 or later FAA approved revisions

3101703-17HP 3101703-17 Test and Computation per 14 CFR §21.303, DWGNo: 3101703 REV: IR Date: 2/17/99 or later FAA approved revisions

3101703-18HP 3101703-18HP Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/ 1 7 /99 or later FAA approved r~visions


DATE: DEC l 7 1999

MAKE ELEGIBILITY


A lliedS ignal (Garrett)


MODEL ELEGIBILITY

TPE 33l-l lU-601G/-l lU-602G/-l 1U-611G/-11 U-612G/-l2B-701A/-l2B-702A/-12UAR-701H/-12UAR-702H/-12UAR-703H/-l 2UAR-704H/-12UAR-705H/-12UAR-706H/-l 2UAR-707H/-12UAR-708H/-12UHR-701 H/-l 2UHR-702H/-12UHR-703H/-12UHR-704H/-12UA-701G/I2UAR-701G/-12JR-701C

TPE 331-1 IU-601 G/-1 IU-602G/-1 l U-6110/-11 U-612G/-12B-701A/-l2B-702A/-l 2UAR-70 l H/-12UAR-702I:I/-12UAR-703H/-12UAR-704H/-12UAR-705H/-l2UAR-706H/-12UAR-707H/-l 2UAR-708H/-12UHR-701 H/- l 2UHR-702H/-l 2UHR-703H/-12UHR-704H/-l 2UA-70 l G/-12UAR-70 lG/-12JR-70lC

TPE 331-8-401S/-8-402S/-8-403 S/-8-404S/-8-406S/-8-422S/-8-423 S/-8-426S/ION-511S/-10N-512S/-l0N-5l4S/-10N-515S/~10N-531S/-10N-532S/-10N-534S/-1 ON-535S/-10UF-50 l H/-l OUF-5 l l H/-l OUF-5 l2H/-10UF-513H/-10UR-5 l3H/-l OUG-513H/-l OUGR-513H/-lOUG-514H/-l OUGR-5 l4H/-l OUF-514H/-l OUF-5 l 5H/l OUF-5 l6H/-l OUG-5 l5H/lOUGR-5l 5H/-lOUG-516H/-lOUGR-516H/-lOU-50 l G/-1 OU-502G/-l OU-511G/-10U-512G/-10-501M/-10-5 l lM/-lOT-51 tM/-10-501C/-lOR-501 C/-lOR-502C/-10-51 lC/-lOR-5 l l C/-lOR-512C/-10R-513C/-l0-501K/-10-511K/-10US03G/-l OU-513G/-lOUA-5.l l G/-l OUR-516H

of 13


,.~ Higher Planes · 15001 Walden Road, Suite 214B Montgomery, Texas 77356


PART NUMBER


BUSHING

BUSHING

310170J.19HP

3101703-20HP

NUMBER DESIGN DATA

3101703-19

3101703-20

Test and Computation per 14 CFR §21.303, DWGNo: 3101703 REV: IR Date: 2/17/99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/17199 or later FAA approved revisions


DATE: DEC 1 7 1999

MAKE ELEGIBILITY


AlliedSignal {Garrett)

MODEL ELEGIBILITY

TPE 33l-8-40IS/-8-402S/-8-403S/-8-404S/-8-406S/-8-422S/-8-423S/-8-426S/l0N-511S/-I ON-512S/-l 0N-514S/-ION-515S/-ION-531 S/-1 ON-532S/-I ON-534S/- ION-535S/-l OUF-501 H/-I OUF-51 IH/-I OUF-512H/-IOUF-513H/-1 OUR-513H/-10UG-513H/-1 OUGR-513H/-I OUG-514H/-l OUGR-5 I 4H/-1 OUF-5 I 4H/-I OUF-51 SH/I OUF-516H/-I OUG-51 SH/IOUGR-515H/-IOUG-516H/-I OUGR-516H/-lOU-501G/-I OU-502GI-IOU-5 I lG/-lOU-5 l2G/-IO-501M/-10-51 IM/-IOT-SI IM/-10-501C/-IOR-50 I C/-IOR-502C/-l 0-5 l l C/- l OR-5 l l C/-l OR-512C/-1 OR-513C/-10-50 IK/-10-511K/-IOU-5030/-1 OU-5130/-1 OUA-5 l l G/-10UR-5 l 6H

TPE 331-8-40 l S/-8-402S/-8-40 3 S/-8-404S/ -8-406S/-8-422S/-8-423S/-8-426S/ION-511S/-ION-5 l2S/-l0N-514S/-l ON-51 SS/-l ON-53 IS/-l ON-532S/-l ON-534S/-l ON-53 5S/-l OUF-501H/-10UF-S l 1H/-IOUF-512H/-10UF-513H/-10UR-513H/-l OUG-:513H/-I OUGR-5 l3H/-l OUG-5 l 4H/-1 OUGR-5 l 4H/-1 OUF-5 l 4H/-l OUF-51 SH/l OUF-516H/-IOUG-51 SH/-10UGR-515H/-10UG-5 l 6H/-1 OUGR-5 I 6H/-1 OU-50 l G/-1 OU-502G/-IOU-511 G/- l OU-512G/- l O-50IM/-l0-5 l 1M/-l OT-5 l lM/-10-50lC/-lOR-50 I C/-IOR-502C/-l 0-5 l l C/-l OR-51 I C/-l OR-5 l2C/-l OR-513C/-I0-501K/-I0-511 K/-10U-5030/-1 OU-5130/-1 OUA-511G/-IOUR-5I6H

of 13



PARTNAME

BUSHING

BUSHING

BUSHING

BUSHING

PART NUMBER

3101703-24HP

310 l 703-25HP

310 l 703-26HP

3101703-27HP

APPROVED REPLACEMENT FOR PART APPROVAL BASIS AND APPROVED NUMBER

3101703-24 Test and C.omputation per 14 CFR §21.303, DWGNo: 3101703 REV: IR Date: 2/17/99 or later· FAA approved revisions

3101703-25 Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR

3101703-26

3101703-27

Date: 2/17 /99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV:· IR Date: 2/17 /99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: IR Date: 2/17 /99 or later FAA approved revisions


DATE: DEC 1 7 1999

IVIAKE ELEGIBILITY


AlliedSig_nal (Garrett)



MODEL ELEGIBILITY

TPE 331-1-lOOF/-l-lOlB/l-l O lE/-l-10 lF/-1-1 O lZ/-1-15 lA/-l-l 5 l G/-l-l 5 lK/-2-20 lA/-2-20 l C/-2UA-203D/-5-2S2D/-5B-252D/-5A-252D/-5AB-252D/-l OT-5 l lD/-1 OP-5 l lD/-lOGT-51 lD/-l OGP-51 lD

TPE 331-1-1 OOF/-1-10 lB/-1-1 O 1 E/-1-10 lF/-l-l01Z/-ll5 lA/-l-l 5 lG/-l-l 5 lK/-2-20lA/-2-201 C/-2UA-203D/-5-252D/-5B-252D/-5A-252D/-5AB-252D/-l OT-5 l lD/-l OP-5llD/-10GT-51 lD/-lOGP-5 l lD

TPE 331-l-lOOF/-l-lOlB/l-10 I E/-l-10 lF/-1-10 lZ/-ll 5 lA/-l-15 l G/-l-15 lK/-2-20 l A/-2-20 l C/-2UA-203D/-5-252D/-5B-252D/-5A-252D/-5AB-252D/-l OT-511 D/-l OP-5 l lD/-l OGT-5 ll D/-l OGP-5 l lD

TPE 33 l-8-401S/-8-402S/· 8-40 3S/-8-404S/-8-406S/-8-422S/-8-423 S/-8-426S/l0N-511S/-ION-512S/-10N-5l4S/-l ON-51 SS/- l ON-53 l S/-10N-532S/-lON· 534S/-l ON-535S/-l0UF-50 l H/-10UF-511 H/-l0UF-512H/-IOUF-513H/-lOUR-513H/-lOUG-513H/IOUGR-513H/-l0UG-514H/-10UGR-514H/lOUF-514H/-lOUF-5 l5H/lOUF-516H/-l OUG-515H/-10UGR-515H/-10UG-5 I 6H/-l OUGR-5 l 6H/- l OU-50 lG/-lOU-502G/-lOU-5 l lG/-lOU-5 l2G/-10-501M/-10.Sl 1M/-lOT-511M/-10-50lC/-lOR-501 C/-1 OR-502C/-l 0-511 C/-l OR-511 C/-lOR-512C/-lOR-513C/-l0-501 K/-l 0-5 I lK/-IOU-· 503G/-10U-513G/-lOUA-5 l lG/-lOUR-516H

of 13


~ , Higher Planes. PMA NO. PQ880SW

SUPPLEMENT NO: 8

,~

15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART NAME

BUSHING

BUSHING


PART FOR PART APPROVAL BASIS AND APPROVED. NUMBER NUMBER DESIGN DATA

3101703-28HP 3101703-28 Test and Computation per 14 CFR §21.303, DWG No: 3101703 REV: lR Date: 2/17/99 or later FAA approved revisions

3101703-29HP 3101703-29 Test and Computation per 14 CFR §21.303, DWGNo: 3101703 REV: lR Date: 2/17 /99 or later FAA approved revisions

DATE: DEC 1 7 1999

MAKE ELEGIBILITY



MODEL ELEGIBILITY

TPE 331-8-40 l S/-8-402S/-8-403S/-8-404S/-8-406S/-8-422S/-8-423S/-8-426S/-l ON-5 l l S/-l ON-512S/-l ON-514S/-10N-515S/-10N-531S/-10N-532S/-10N-534S/-l ON-535S/-l OUF-501 H/-l OUF-5 l l H/-l OUF-512H/-10UF-513H/-10UR-513H/-l OUG-513H/lOUGR-513H/-lOUG-5 l4H/-lOUGR-5 l4H/-1 OUF-5 l 4H/- l OUF-515H/l OUF-5 l 6H/-l OUG-515H/-10UGR-5 l 5H/-10UG-516H/-l OUGR-5 l 6H/-l OUSO 1 G/-1 OU-5020/-1 OU-5 l l G/-l OU-512G/-10-501M/-10-5 l lM/-lOT-511M/-10-50lC/-lOR-501 C/-1 OR-502C/- l 0-511 C/- l OR-5 l l C/-l OR-512C/-10R-513C/-10-501K/-10-511K/-10U-5030/-1 OU-513G/-10UA-5 l l G/-l OUR-516H

TPE 331-8-401S/-8-402S/-8-403S/-8-404S/-8-406S/-8-422S/-8-423S/-8-426S/-l ON-511S/-l ON-5 l2S/- l ON-514S/-10N-515S/-10N-531S/-10N-532S/-10N-534S/-l ON-535S/-l OUF-501 H/- l OUF-5 l l H/-l OUF-512H/-10UF-513H/~10UR-513H/-10UG-513H/-10UGR-5 l3H/-10UG-514H/-l OUGR-5 l 4H/-l OUF-5 l 4H/-l OUF-51 SH/~ 10UF-516H/-10UG-515H/-10UGR-515H/-10UG-516H/-1 OUGR-516H/- l OU-501 G/-1 OU-502G/-1 OU-5 l l G/-l OU-512G/-10-501M/-10-511M/-10T-511M/-10-501C/-10R-501 C/-1 OR-502C/-l 0-511 C/- l OR-5 l l C/-l OR-512C/-10R-513C/-10-501 K/-l0-511K/-10U-5030/-1 OU-5130/-1 OUA-5 l l G/-l OUR-5 l 6H

~\

Page 10 of 13




PART NUMBER


BUSHING

BUSHING

3101759-lHP

3 I01759-2HP

NUMBER DESIGN DATA

3101759-1

3101759-2

Test and Computation per 14 CFR §21.303, DWGNo: 3101759 REV: A Date: 7 /15/99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101759 REV: A Date: 7/15/99 or later FAA approved revisions


DATE: DEC l 7 1999

MAKE ELEGIBILITY



MODEL ELEGIBILITY

TPE 331-1-1OOF/-1-10 IB/-1-101E/-1-10 l F/-1-1 OlZ/-1-15 lN-l-lS 1 G/-1-151 K/-2-20 lN-2-201 C/-2UA-203D/S-252D/-SB-252D/-SA-2S2D/-5AB-2S2D/-8-40 l S/-8-402S/-8-403S/-8-422S/-8-423S/-l0N-Sl lS/-10N-512S/-10N-514S/-l0N-S lSS/-1 ON-S31S/-10NS32S/-1 ON-534S/-l ON-535S/-1 OU-SO 1 G/-1 OU-502G/-10U-51 I G/-10USl2G/-10-501M/-10-SI lM/lOT-Sl IM/-10-SOlC/-lOR-501 C/-1OR-502C/-10-S I l C/-l OR-SI l C/-l OR-512C/-10R-S 13C/-10-SO IK/-10-S l l K/-I OU-503G/- I OU-5 I 3G/-I OUA-511 G/- I OT-5 l lD/- IOP-Sl 1D/-10GT-511D/-10GP-511D

TPE 331-1-lOOF/-l-IOlB/l-l O IE/-1-10lF/-1-1012/-1-15 lN-l-lS IG/-1-151 K/-2-20 l N-2-20 l C/-2UA-203 D/S-252D/-5B-252D/-5A-252D/-5AB-252D/-8-401 S/-8-402S/-8-403S/-8-422S/-8-423S/-10N-Sl 1S/-10NSl2S/-10N-514S/-l0N-51 SS/-l ON-531 S/-ION-532S/-l ON-534S/-l ON-535S/-l OU-SO l G/-1 OU-502G/-l OU-511 G/-1 OU-S l 2G/-l O-SO l M/-10-511 M/lOT-Sl lM/-10:-SOlC/-IOR-501C/-IOR-502C/-IO-S I lC/-lOR-SrIC/-lOR-512C/-l OR-5 l3C/-10-501 K/-l 0-5 l 1K/-IOU-503G/-l OU-5 l 3G/- l OUA-511 G/-l OT-S l lD/-l OP-S l lD/-IOGT-51 lD/-lOGPS l lD/-lOUF-SOlH/-IOUF-511H/-IOUF-512H/-10UF-513H/-l OUR-5 I3H/-l OUG-513H/-l OUGR-S I3H/-l OUG-5 I 4H/-l OUGR-514H/-l OUF-S 14H/-10UF-51 SH/-1 OUF-5 l 6H/-l OUG-51 SH/-1OUGR-515H/-I OUG-516H/-10UGR-516H/-IOUR-516H

---......

Page 11 of 13


, Higher Planes 15001 Walden Road, Suite 214B Montgomery, Texas 77356

PART NAME

BUSHING

PART NUMBER

3101759-3HP


3101759-3 Test and Computation per 14 CFR §21.303, DWG No: 3101759 REV: A . Date: 7/15/99 or later FAA approved revisions


DATE: DEC 1 7 1999

MAKE ELEGIBILITY


MODEL ELEGIBILITY

TPE 331-1-1 OOF/-1-1018/-1-10 l E/-1-1 OIF/-1-1 OIZ/-1-151N-l-151G/-l-ISIK/-2-20 I N-2-20 I C/-2UA-203 D/-5-252D/-5B-252D/-5A-252D/-5AB-252D/-8-40 l S/-8-402S/-8-403S/-8-422S/-8-423S/-ION-511S/-10N-512S/-l0N-514S/-l0N-5 l 5S/-l ON-531 S/-1 ON-532S/-1 ON-534S/-l ON-535S/-l OU-50 I G/-1 OU-502G/-1 OU-511 G/-IOU-512G/-10-501M/-10-5 l 1M/lOT-5 l lM/-10-501C/-lOR-50 l C/-1OR-502C/-10-511 C/-lOR-51 l C/-lOR-512C/-IOR-513C/-10-50 I K/-10-511 K/-10U-503G/-l OU-513G/-l OUA-511G/-lOT-511P/-lOP-51 ID/-IOGT-511D/-IOGP-51 ID/- l OUF-50 I H/-1 OUF-5 l l H/-l OUF-512H/-lOUF-513H/-10UR-513H/-IOUG-513H/-IOUGR-513H/-10UG-514H/-10UGR-514H/-l OUF-5 l 4H/-l OUF-51 SH/-1 OUF-516H/-10UG-515H/-10UGR-515H/lOUG-516H/-lOUGR-516H/-lOUR-516H

of 13

FEDERAL AVIATION ADMINISTRATION -PARTS MANUFACTURING APPROVAL


PART NAME

BUSHING

BUSHING

BUSHING

PART NUMBER

3101759-4HP

310 l 759-5HP

310 l 759-6HP

APPROVED REPLACEMENT FOR PART NUMBER

3101759-4

3101759-S

3101759-6


Test and Computation per 14 CFR §21.303, DWG No: 3101759 REV: A Date: 7 /15/99 or later FAA approved revisions

Test and Computation per 14 CFR §21.303, DWG No: 3101759 REV: A Date: 7 /l 5/99 -,

or later FAA approved revisions

Test and Computation-· per 14 CFR §21.303, DWG No: 3101759 REV: A Date: 7/15/99 or later FAA approved revisions


DATE: DEC l 7 1999

MAKE ELEGIBILITY




MODEL ELEGIBILITY

TPE 331-1-lOOF/-I-lOlB/l-l O IE/..:1-10 IF/-l-101Z/-ll51A/-l-l51 G/-1-151 K/-2-201 A/-2-20 l C/-2UA-203 D/-5-252D/-5B-252D/-5A-252D/-5AB-252D/-8-401 S/-8-402S/-8-403S/-8-422S/-8-423S/-10N-51 IS/-l0N-512S/-l0N-514S/-10N-5 l5S/-10N-S31S/-ION:. 532S/-l ON-534S/-l ON-535S/-l OU-501 G/-IOU-502G/-IOU-5 l l G/-10U-512G/-l0-501M/-I0-5l Uv1/-10T-511M/-l0-501C/-IOR-50 l C/-1 OR-502C/-l 0-51 l C/-l OR-5 l l C/-l OR-512C/-IOR-513C/-10-501 K/-l0-511K/-lOU-5030/-1 OU-5 l 3G/-l OUA-511 G/-l OT-5 l lD/- l OP-511D/-lOGT-51 lD/-IOGP-51 lD/-lOUF-501H/-lOUF-5 l 1H/-10UF-512H/-l OUF-513H/-lOUR-513H/-lOUG-513H/-IOUGR-513H/IOUG-514H/-1 OUGR-514H/-lOUF-514H/-lOUF-51 SH/-1 OUF-5 l 6H/-l OUG-5 l 5H/-l OUGR-515H/-10UG-516H/-I0UGR-516H/-10UR-516H

TPE 331-1-lOOF/-1-lOIB/l-101 E/-1-10 l F/-1-1 OlZ/-l-15 IA/-1-151 G/-1-151 K/-2-20lA/-2-201 C/-2UA-203D/-5-252D/-5B-252D/-5A-252D/-5AB-252D/- l OT-51 lD/-l OP-511D/- IOGT-511D/- l OGP-5 ll D

TPE 331-1-1 OOF/-HOIB/-1-10 lE/-l-10 I F/-1-1 OlZ/-l-15 lA/-1-151 G/-l-15 IK/-2-20lA/-2-201 C/-2UA-203D/· 5-252D/-5B-252D/-5A-252D/-5AB-252D/-l OT-5 l 1D/-l OP-511D/-IOGT-51 lD/-lOGP-5 I ID

,·~

Page 13 of13





DATE: DEC 1 7 1999

PART NUMBER

FOR PART APPROVAL BASIS AND APPROVED MAKE ELEGIBILITY PART NAME

BUSHING 3l0l 759-7HP

NUMBER DESIGN DATA

3101759-7 Test and Computation per 14 CFR §21.303, DWGNo: 3101759 REV: A Date: 7/15/99


MODEL ELEGIBILITY

TPE 331-l-lOOF/-l-lOIB/l-l O l E/-1-10 lF/-1-10 lZ/-l-15 lAf-1-151 G/-l-15 l K/-2-20 lA/-2-20 l C/-2UA-203D/-5-252D/-5B-252D/-5A-2520/-5AB-252D//-l OT-

or later FAA approved revisions 51 lD/- l OP-5 l lD/-l OGT-51 lD/-lOGP-51 lD

----------- .--------------------------------------------------End of Listing-------------------------------------------------------4----------------------

Note: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major Design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

artier na r, Propulsion Branch

Los ngeles Aircraft Certification Office Manager, Manufactuming Inspection District Office SW-MID0-43

) ) )

FAA- PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT

Higher Planes 15001 Walden Road. Suite 214B Montgomery, TX 77356

PART NAME Exhaust Duct

PART NUMBER 035A-42401HP

PMA No. P0880SW Supplement No. _9 ________ _

Revision No. None ----------AC O PMA Project Number: PM1849AC-A

APPROVED APPROVAL BASIS . REPLACEMENT· AND APPROVED FOR DESIGN DATA 035A-42401 Test and computations per

14 CFR Section 21.303 Dwg. No. 035A-42401HP Rev. A Dtd. 10-25-00 or later FAA approved revisions ..

INSTALLATION ELIGIBILITY (MAKE) Mitsubishi Heavy Industries, Ltd.


MU-2B-25, MU-2B-26, MU-2B-35, MU-2B-36, MU-2B-26A modified per STC SA09565SC, MU-2B-36A modified per STC SA09565SC, and MU-2B-40 & MU-2B-60 modified per STC SA094668SC

Note: Minor design changes (reference 14CFR part 21 §§21.93 and 21.95) must be approved and submitted in a manner as determined by the ACO. Major Design changes (reference 14CFR part 21 §§21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

Michele M. Owsley 7 Manager, · Airplane Certification Office, ASW-150

J./ I. ·01 ~

Manager, Manufacturing Inspection District Office, SW-MID0-43

This Supplement is an attachment to your FAA-PMA approval letter dated: June 10, 1998.

) ) )

FAA- PARTS MANUFACTURER APPROVAL {PMA) SUPPLEMENT

Higher Planes 15001 Walden Road. Suite 214B Montgomery, TX 77356

PART NAME Exhaust Duct

PART NUMBER 035A-42401HP

PMA No. PQ880SW Supplement No. ____ 9 ______ _

Revision No. 1 ----------AC O PMA Project Number: PM1849AC-A

APPROVED APPROVAL BASIS REPLACEMENT .AND APPROVED FOR DESIGN DATA 035A-42401 Test and computations per

14 CFR Section 21.303 Dwg. No. 035A-42401HP Rev. A Dtd. 10-25-00 or later FAA approved revisions.

INSTALLATION ELIGIBILITY (MAKE) Mitsubishi Heavy Industries, Ltd.


MU-2B-25, MU-2B-26, MU-2B-35, MU-2B-36; modified per STC SA09565SC; MU-2B-26A and MU-2B-36A modified per STC SA09468SC; and MU-2B-40 & MU-2B-60

Note: Minor design changes (reference 14CFR part 21 §§21.93 and 21.95) must be approved and submitted in a manner as determined by the ACO. Major Design changes (reference 14CFR part 21 §§21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original F AA-PMA.

#zL Date

Manager, ·,

Manufacturing Inspection District Office, SW-MID0-43

) ) Federal Aviation Administration - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT (SAMPLE)

Higher Planes 513 Bryant Road Conroe, TX 77303

PART Part NAME Number

Thrust 207218HP Washer

Approved APPROVAL BASIS ReRlacement AND APPROVED For DESIGN DATA

Raytheon Test and computations per 207218 14 CFR Section 21.303

Dwg. No. 20721 SHP Rev. IR DTD: 5-14-01 or later FAA approved revisions.

PMA No. P0880SW Supplement No. _!Q__ Revision No. ----ACO PMA Project Number: PM6768SC-E

INSTALLATION INSTALLATION ELIGIBILITY <MODEL}

ELIGIBILITY {MAKE)

Raytheon Aircraft

Israel Aircraft Industries ltd.

BH. 125 Series 600A HS. 125 Series 600A HS. 125 Series 600B HS. 125 Series 600B/l HS. 125 Series 600B/2 HS. 125 Series 600B/3 HS. 125 Series 700A HS. 125 Series 700B Bae. 125 Series 800A (C-29A, U-125) Bae. 125 Series 800B Bae. 125 Series 1000A Bae. 125 Series I OOOB Hawker 800, Hawker 800 (U-125A) Hawker 1000 Hawker 800XP

1124, 1124A

------------------------------------------------------------------------------En d of Listing---------------------------------------------------------------------------------------

Note: Minor design changes (reference 14CFR part 21§§21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major Design changes (reference 14CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

~·~.~ Jurgen E. Priester Project Engineer Special Certification Office, ASW-190

Manager Manufacturing Inspection Dis nc Office SW-MID0-43

)

Page 1 of I

) ) ) Federal Aviation Administration- PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT


PART NAME

Key Washer

Part Number

5006492HP


Pratt & Whitney Canada Inc. 5006492


Test and computations per 14 CFR Section 21.303 Dwg. No. 50()6492HP Rev. IRDTD: 4-17-01 or later FAA approved revisions.

PMA No. P0880SW Supplement No. -=-'~

Revision No. ___ _ ACO PMA Project Number: PM6769SC-E


Pratt & Whitney Canada Inc.


PVV118,PVV118A,PVV118B,PVV1198, PVV119C,PVV120,PVV120A,PVV121,PVV121A, PVV123,PVV123AF,PVV123B,PVV123C, PVV123D, PVV123E, PVV124B, PVV1.25B, PVV126A,PVV127,PVV127E,PVV127F, PVV127G

---------------------------------------------------------------------------En d of Listing-----------------------------------------------------------------------------------

Note: Minor design changes (reference l 4CFR part 21 §§21.93 and 21.95) must be submitted in a manner as detennined by the ACO. Major Design changes (reference 14CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

Jurgen E. Priester Project Engineer Special Certification Office, ASW-190

Manager Manufacturing Inspectt...__=--.H SW-MID0-43

Page 1 of 1

) ) Federal Aviation Administration - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT


PART Part NAME Number

Lock Plate 3101373-IHP


3101373-1


Test and computations per 14 CFR Section 21.303 Dwg. No. 3101373 Rev. IR DTD. 5-29-01 or later FAA approved revisions.

PMA No. P0880SW Supplement No. -=l=-2 _ Revision No. __ ACO PMA Project Number: PM6770SC-E

INSTALLATION ELIGIBILITY {MAKE}

Allied Signal (GARRETT)

INSTALLATION ELIGIBILITY {MODEL)

TPE.331-3 SERIES/-5 SERIES/-6 SERIES/-8 SERIES/-10 SERIES TSE331-3 SERIES

------------------------------------------------------------------------------------En d of Listing---------------------·------------------------------------------------------------------------

Note: Minor design changes (reference 14CFR part 21§§21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major Design changes (reference l 4CFR part 21 § § 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

~£.~ Ju~ Project Engineer Special Certification Office, ASW-190

anager Manufacturing Inspection SW-MID0-43

)

Page I of 1

)

Higher Planes 513 Bryant Road Conroe, Texas 77303

PART NAME

Spring Washer

Spring Washer

Vespel Bearing

Part Number

D6-1HP

D6-4HP

3233190-2HP

) Federal Aviation Administration- PARTS MANUFACTUK.BR APPROVAL (PMA) SUPPLEMENT (SAMPLE)

PMA No. PQ880SW


D6-1

D6-4

3233190-2


Test & Computation Per 14 CFR § 21.303 In Accordance With Dwg.D6 Rev. B, DTD: 10/30/01 Or Later FAA-Approved Revision

Test & Computation Per 14 CFR § 21.303 In Accordance With Dwg.D6 Rev. B, DTD: 10/30/01 Or Later FAA-Approved Revision

Test & Computation Per 14 CFR § 21.303 In Accordance With Dwg. 3233190-2HP Rev. B, DTD: 06/09/03 Or Later FAA-Approved Revision

Supplement No. _Ll_ Revision No. 1, AUGUST 31, 2006 ACO PMA Project Number: PM6767SC-T


Learjet

Dassault Aviation

Sabreliner Corp.

Raytheon Aircraft Co.

Learjet

Dassault Aviation

SabreJiner Corp.

Raytheon Aircraft Co.

Learjet

Dassault Aviation

Sabreliner Corp


35, 35A (C-21), 36, 36A, 55, 55B, 55C

Fan Jet Falcon, Fan Jet Falcon Series C, D, E, F Modified per STC: SA2568WE

NA-265-80

HS.125 Series 700A, HS.125 Series 700B

35, 35A (C-21), 36, 36A, 55, 55B, 55C


NA-265-80

HS.125 Series 700A, HS.125 Series 700B

35, 35A (C-21), 36, 36A, 55, 55B, 55C


NA-265-80

Raytheon Aircraft Co HS.125 Series 700A, HS.125 Series 700B

J

-----------------------------------------------------------------------------------End of Listing------------------------- .. -------------------------------------------------------------------Note: Minor design changes (reference l4CFR part 21§§21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major Design changes (reference 14CFR part 21 §§ 21.93 · and 21.97) to drawings and specifications are to be handled in the same J,nanner as that for an original

FAA-PMA. . --:7_ / J. -' Q . 7 t/0/(_ ~.---

'""' S. Frances Cox Manager, Special Certifica ion Office ASW-190

) )

Ford Lauer Manager, Manufacturing Inspection District Office

SW-MID0-43

Pagel of 1

)

) --Higher Planes 513 Bryant Road Conroe, Texas 77303

PART NAME

Bushing

Part Number

893579-lHP

) Federal Aviation Administration - PARTS MANUFACTURER APPROVAL (PMA) SUPPLEMENT (SAMPLE)

PMA No. P0880SW

)


Allied Signal 893579-1


Test and computations per 14 CFR Section 21.303 Dwg. No. 893579-lHP Rev. B, DTD: 09/04/02 or later FAA approved revisions.

Supplement No. _H Revision No. 1, AUGUST 31, 2006 ACO PMA Project Number: PM7034SC-E


Allied Signal (Honeywell)

INSTALLATION ELIGIBILITY (MODEL}

TPE 331-1, TPE331-2, TPE331-2U, TPE331-2UA, TPE331-3U, TPE331-3UW, TPE331-5, TPE331-5A, TPE33I-6, TPE331-6A, TPE331-10, TPE331-10U, TPE331-10UA, TPE331-10UF, TPE331-10UG,, TPE331-10UGR, TPE331-IOUR, TPE331-l 1U, TPE331-12UA, TPE331-12UAR TSE331-3U

---------------------------------------------------------------------------------End of Listing---------------------------------------------------------------------------------------------Note: Minor design changes (reference 14CFR part 21§§21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major Design changes (reference I4CFR part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original

FAA~~ . fend~ S. Frances Cox Ford Lauer Manager, Special Certification Office Manager, Manufacturing Inspection District Office ASW-190 SW-MID0-43

Page 1 of 1

)


PART NAME

Cable Assembly

Cable AssemblyAft

Cable AssemblyAft

Cable Assembly

Cable Assembly

PART NUMBER

54 l 5530-5HP

5415542-16HP

54 I 5542-23HP

5415542-26HP

6015 550-002HP

) \ FAA- PARTS MANUFACTURER APPROVAL <PMA) SUPPLEMENT

,/

REPLACEMENT FOR

5415530-5

5415542-16

5415542-23

5415542-26

6015550-002


Test and computations per 14 CFR Section 21.303 Dwg. No. 5415530 Rev. IR Dtd. 10/17/02 or later FAA approved revisions.

Test and computations per 14 CFR Section 21.303 Dwg.No.5415542 Rev. IR Dtd. 10/10/02 or later FAA approved revisions.

Test and computations per 14 CFR Section 21.303 Dwg. No. 5415542 Rev. IR Dtd. 10/10/02 or later FAA approved revisions.

Test and computations per 14 CFR Section 21.303 Dwg. No. 5415542 Rev. IR Dtd. 10/ 10/02 or later FAA approved revisions.

:rest and computations per 14 CFR Section 21.303 Dwg. No. 6015550 Rev. IR Dtd. 10/19/02 or later FAA approved revisions.

Page 1 of2

PMA No. PQ880SW Supplement No. 15

Revision No. Project No. PM7343SC-T

ELIGIBILITY (MAKE)

Learje_t Inc.

Learjet Inc.

Learjet Inc.

Learjet Inc.

Learjet Inc.

ELIGIBILITY (MODEL)

55, 55B, 55C, 60

55

55, 55B, 55C

55, 55B, SSC

60

) ) PMA No. PQ880SW Supplement No. 15 Revision No.

PART NAME Cable Assembly

PART NUMBER 6015550-003HP

REPLACEMENT FOR 6015550-003

APPROVAL BASIS AND APPROVED DESIGN DATA Test and computations per 14 CFR Section 21.303 Dwg. No. 6015550 Rev. IR Dtd. 10/19/02 or later FAA approved revisions.

ELIGIBILITY . ELIGIBILITY (MAKE) _(M __ O_DE_L_) ______ _ Learjet Inc. 60

------------------------------------------------------------------------------------End of~isting---------------------------------------------------------------------------


James Aero ace Engineer, Special Certification Office, AS -190

I I /nt)tZ D3 . Date

Manager, Manufacturing Inspection District Office SWMID0-43

This Supplement is an attachment to your FAA-PMA approval letter dated: June 10, 1998

Page 2 of2

t1AR 2 6 2003

Date

FEDERAL AVIATION ADMINISTRATION -PARTS MANUFACTURER APPROVAL


Part Name

As Identified on Master Drawing List


Part Number



PMANo. Supplement No. Revision No. Project No.

PQ0880SW 16 A

Approved Replacement for Part


Make Eligibility

Model Eligibility

Modification Identicality per 14 CFR § 21.303, licensing agreement between Higher Planes, Inc. and Flight Test Associates, Inc. dated August 7, 2003, Dwg. No: West Star Aviation, Inc. Master Drawing List 3 OA2 l 0002 Rev: C Date: May 08, 2003, or later FAA approved revisions as approved on STC STO l 525LA issued August 1, 2003.

Learjet

Modification Identicality per 14 CFR § Learjet 21.303, licensing agreement between Higher Planes, Inc. and Flight Test Associates, Inc. dated August 7, 2003, Dwg. No: West Star Aviation, Inc. Master Drawing List 30A210001 Rev: F Date: May 08, 2002, or later FAA approved revisions as approved on STC STO l 524LA issued: August 1, 2003.

35,35A, 36, 36A

35,35A, 36, 36A

-------------------------------------------------------------End of Listing---------------------------------------------------N OTE: Minor design changes (reference 14 CFR part 21 §§ 21.93 and 21.95) must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR part 21 §§ 21.93 and 21.97) to drawings and specification are to be h 'n the same manner as that for an original F AA-PMA.

Robert A. Robino, Jr. Manager, Manufacturing Insp

District Office, SW MID0-43

~ -;2 ,5-0 ~ Date

This Supplement is an attachment to your F AA-PMA approval letter dated: October 2, 200 I Page 1 of 1

f.

) ) h·dl.'ral A,·i.&1iu11 i\d111i11is1ration_ P,\RTS MANlJFA<.. vRER APPRO\'Al. WMAtSUPPLEMENT <SAMJ_1J:1

11 iglu.·r Phuws 11.' H1·~1ant Roud ('unrot•, Tt•x;1s 77357

Part N.mtL'

s~·al ;\:S.'.'IL' llihl Y

Part Nmnb(•r

31-llJ2IOO-l:'illP

31-JU.2 IOO · IHIIP

Sea! FWD J 1-1 U:! I 00-J tJll p

\t·al ,\Fl J 1-IU2 I00--

20I IP

Approved Rcpluccnwnt For Part Numbers

3 l-1-U2 IOO-l 5

3l4lJ2100-18

.'\ I -H l 2 I 00- I lJ

JI 4U2 I00-20

A11provnl Rusis and Approved Design Data

Test and compurntions per 14 CFR Section 2 I .303, Dwg. No. 314U2 IOO, Rev. B. Dated 11/22/02, or Later FAA approved revisions.

Test and l:omputations per 14 CFR Section 21.303. Dwg. No. 3 l4U2JOO, Rev. B. Dated 11/22/02, or Lacer FAA approved revisions .

Make Eligibility

Boeing Company

Boeing Company

Test and computations per, 14 CFR Boeing Company Section 21.303, Dwg. No. Jl4U2100, Rev. B, Dated 11/22/02, or I •• lier FAA approved revisions.

Test and complllalions per 14 CFR Boeing Compnny Scc1ion 21.303, Dwg. No. 3I4U2IOO Rev. B. Dated, 11/22/02. or Later FAA approved revisions.

PMA No.: Su1)1>lcment No.:

Rt•,,ision No.:

Projec:t No.:

Model Eligibility

PQOM80SW 17

PM7229SC-T

747-200B. 747-300, 747-400, 747-4001), 747-400F. 767-::?oo. 767-Joo. 767-JOOF, 767-400ER

747-2000, 747-300. 747-400, 747-400D, 747-40or. 761-200, 767-300. 767-:mor. 767-400ER

747-2008, 747-]00, 747-400. 747-4001), 747°400F, 767-200. 767-300, 767-)00F, 767-400ER

747<!008, 747-300. 747-400, 747-4001), 747-4flOF, 767-200, 767-300, 767-JOOF. 767-400ER

Noll·: f\linor (ksign chauges (reference 14CFR p.1rt 21 §§:! I .93 und 21.95) must be submiued in a manner as determined by the ACO. Major Dcsi~n chan!!cs , 1cfnt·11n.- 1.H 'Fl{ p;u-l ::? I §§ 21.CJJ :md 2 I .97) to drawings :rnd spccificutions arc to he handled in the same mmllll'r :is th:11 for an rn·i!!in:11 FAA-PM A.

u~ l·u·d S1dl:11 Supl·n 1-..01 ~- h1gim.:l'L Sp\.'dal ( 'l"rlilkation Ollkc.

:\SW 11m

:L:t s.1: I'_ c:J .3 ·- -·· l>ah:

Mmmgcr. Manufacturing In. SW-MID0-43 .,,.

I hi.!- S11ppk111t·111 is an alladuncnt 10 your F/\A-PMA l,:th:r tlalcd: ~ IC) IJB 10/02/01.

I o//rlf-Jo 'l __ I >all'

Higher ts S 13 Hryant Road Conroe, Texas 77303

Part Name

Carbon Ring, Guide

Part Approved Number Replacement For

77E76-1 HP 77E76- I

Carbon Ring 78EI5-1HP 78El5-l

Ring Assy. 78E 16-lHP 78E 16-l Piston

Spherical Seal l 6J58-l HP l 6J58-l Assembly (Carbon)

Spherical Seal I 6J61-l HP 16J6l-l Assembly (Carbon)

) PMA No. P()O:--;XOS\V

Supplement No. 18 Revision No.

ACO Project Number PM7632SC-T

AJ>proval Basis And Approved Design Data

Test and computations per 14 CFR Section 21.303, Dwg. No. 77E76, Rev. A, Dated 8/6/03, or later FAA approved revisions.

Installation Eligibility Make

Boeing Company

Test and computations per, 14 CFR Section 21.303, Dwg. Boeing Company No. 78E 15, Rev. A, Dated 8/6/03, or later FAA approved revisions.

Test and computations per l 4 CFR Section 21.303, Dwg. Boeing Company No. 78E16, Rev. A, Dated 8/6/03, or later FAA approved revisions.

Test and computations per 14 CFR Section 21.303, Dwg. Boeing Company No. l 6J58, Rev. A, Dated 8/6/03, or later FAA approved revisions.

Test and computations per l4 CFR Section 21.303, Dwg. Boeing Company No. 1616 l, Rev. A, Dated 8/6/03, or later FAA approved revisions.

Installation Eligibility Model

757-200, 757-200PF, 757-200CB, 757-300

757-200, 757-200PF, 757-200C8, 757-300

757-200, 757-200PF, 757-200CB, 757-300

757-200, 757-200PF, 757-200CB, 757-300

757-200, 757-200PF, 757-200CB, 757-300

)

--------------------------------------------------------------------------------------End of Listing---------------------------------------------------------------- ------------ --------- -

Note: Minor design changes (reference J 4CFR part 21 §§21. 93 and 21.95) must be submitted in a manner as determined by the ACO. Major Design changes (reference 14CFR part 21 §§ 2 J .93 and 21.97) to drawings and specifications are to be handled in the same manner as that for an original FAA-PMA.

Z~JJ)lw~L·'~ S. Frances Cox Manager, Special Ce11ification Office. ASW-190

Manager, Manufacturing Inspection District Office, SW-MID0-43

, This Supplement is an attachment lo your FAA-PMA approval letter dated: October 2, 2001.

MAR 1 2 2004 Date

Page I of I


,,~ Higher Planes PMANo.: PQ0880SW S13 Bryant Road Supplement No.: 19 Conroe, Texas 77303 Revision No.:

Project No.:

Approved Approval Basis and

Part Replacement Make Part Name

Number for Part Approved Design

Eligibility Model Eligibility

Number Data

Angle, 52-1012-1 Modification Identicality per 14 CFR Boeing 737-200 Support § 21.303, licensing 737-200C

agreeinentbetvveen 737-300 Higher Planes, Inc. and 737-400 AeroTech Services, Inc. 737-500 Series Deceinber 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: N oveinber 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued Noveinber 17, 2004, ainended July 12, 2005, or later FAA approved revision.

Skin 52-1012-3 Modification Identicality per 14 CFR Boeing 737-200 § 21.303, licensing 737-200C agreeinentbetvveen 737-300 Higher Planes, Inc. and 737-400 AeroTech Services, Inc. 737-500 Series Deceinber 4, 2006, per Airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Part Name Part Number Approved Approval Basis and Make Model Eligibility -...., Replacement for Approved Design Data Eligibility

Part Number

Angle, 52-1012-5 Modification Identicality per 14 CFR Boeing 737-200 Retainer § 21.303, licensing 737-200C

agreement between 737-300 Higher Planes, Inc. and 737-400 AeroTech Services, Inc. 737-500 Series December 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Clip, 52-1012-7 Modification Identicality per 14 CFR Boeing 737-200 Vertical § 21.303, licensing 737-200C

agreement between 737-300 ~ Higher Planes, Inc. and 737-400

AeroTech Services, Inc. 737-500 Series December 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Part Name Part Number Approved Approval Basis and Make Model Eligibility

·~. Replacement for Approved Design Data Eligibility Part Number

Clip, 52-1012-13 Modification Identicality per 14 CFR Boeing 737-200 Vertical § 21.303, licensing 737-200C

agreement between 737-300 Higher Planes, Inc. and 737-400 AeroTech Services, Inc. 737-500 Series December 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev: F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November i7, 2004, amended July 12, 2005, or later FAA approved revision.

Spacer, 52-1030-1 Modification Identicality per 14 CFR Boeing 737-200 Inboard § 21.303, licensing 737-200C

agreement between 737-300 ~. Higher Planes, Inc. and 737-400

AeroTech Services, Inc. 737-500 Series December 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Approved Approval Basis and Make

~ Part Name Part Number Replacement for

Approved Design Data Eligibility Model Eligibility

\ Part Number

Spacer, 52-1030-3 Modification Identicality per 14 Boeing 737-200 Outboard CFR § 21.303, 737-200C

licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Plate, 52-1040-1 Modification Identicality per 14 Boeing 737-200

~ Aileron CFR § 21.303, 737-200C Index licensing agreement 737-300

between Higher 737-400 Planes, Inc. and 737-500 Series Aero Tech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.


~- Part Name Part Number Replacement for Approved Design Data Eligibility

Model Eligibility Part Number

Placard 52-1051-1 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Placard 52-1051-5 Modification Identicality per 14 Boeing 737-200 "~ CFR § 21.303, 737-200C


0 PartName Part Number Approved Approval Basis and Make Model Eligibility Replacement Approved Design Data Eligibility for Part Number

Extension, 52-1120-11 Modification Identicality per 14 Boeing 737-200 Inboard, CFR § 21.303, 737-200C Forward licensing agreement 737-300

between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Extension, 52-1120-13 Modification Identicality per 14 Boeing 737-200 Outboard, CFR § 21.303, 737-200C Aft licensing agreement 737-300



-~, Part Name Part Number Replacement Approved Design Data ~ligibility

Model Eligibility for Part Number

Extension, 52-1120-15 Modification Identicality per 14 Boeing 737-200 Inboard, Aft CFR § 21.303, 737-200C

licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services; Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

-~ Stop, Lower 52-1130-3 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737~400 Planes, Inc. and 737-500 Series Aero Tech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Part Name Part Number Approved Approval Basis and Make Model Eligibility .,.........,.', Replacement for Approved Design Data Eligibility

Part Number

Extension, 52-1120-17 Modification Identicality per 14 CFR Boeing 737-200 Outboard,· § 21.303, licensing 737-200C Forward agreement between 737-300

Higher Planes, Inc. and 737-400 AeroTech Services, Inc. 737-500 Series December 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC STO l 625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Stop, Upper 52-1130-1 Modification Identicality per 14 CFR Boeing 737-200 § 21.303, licensing 737-200C agreement between 737-300

~\ Higher Planes, Inc. and 737-400 AeroTech Services, Inc. 737-500 Series December 4, 2006, per airplanes AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

--


-~ ..... , Part Name Part Number Replacement Approved Design Data Eligibility

Model Eligibility for Part Number

Stop, Inner 52-1130-5 Modification ldenticality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005; or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Seal 52-1140-1 Modification Identicality per 14 Boeing 737-200

~ CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes,Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12,. 2005, or later FAA approved revision.


~ Part Name Part Number Replacement Approved Design Data Eligibility

Model Eligibility . for Part Number

Seal 52-1140-3 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC STO l 625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Extension, 52-1220-11 Modification Identicality per 14 Boeing 737-200 /~ Inboard, CFR § 21.303, 737-200C

Forward licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.


-~ Replacement Approved Design Data Eligibility for Part Number

Extension, 52-1220-13 Modification Identicality per 14 Boeing 737-200 Outboard, CPR§ 21.303, 737-200C Aft licensing agreement 737-300

between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, · 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: ·52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Extension, 52-1220-15 Modification Identicality per 14 Boeing 737-200 Inboard, Aft CFR § 21.303, 737-200C


Part Name Part Number Approved Approval Basis and Make Model Eligibility ~ Replacement Approved Design Data Eligibility

for Part Number

Extension, 52-1220-17 Modification Identicality per 14 Boeing 737-200 Outboard, CFR § 21.303, 737-200C Forward licensing agreement 737;.JOO


Angle, 52-1300-25 Modification Identicality per 14 Boeing 737-200 ~ Support CFR § 21.303, 737-200C


Part Name Part Number Approved Approval Basis and Make Model Eligibility Replacement for Approved Design Data Eligibility Part Number

Angle, 52-1300-27 Modification Identicality per 14 Boeing 737-200 Support CFR § 21.303, 737-200C


Angle, 52-1300-29 Modification ldenticality per 14 Boeing 37-200 /~ Support CFR § 21.303, 737-200C

licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev: F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004,

. amended July 12, 2005, or later FAA approved revision.


Angle, 52-1300-31 Modification Identicality per 14 Boeing 737-200 Support CFR § 21.303, 737-200C·


Angle, 52-1300-33 Modification Identicality per 14 Boeing 737-200 Support CFR § 21.303, 737-200C



Retainer 52-1300-35 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Retainer 52-1300-37 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series Aero Tech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC STO 1625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.


~ Replacement for Approved Design Data Eligib!lity Part Number

Retainer 52-1300-39 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg .. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Retainer 52-1300-41 Modification Identicality per 14 Boeing 737-200 ~. CFR § 21.303, 737-200C


,,.-...__,

Part Name Part Number Approved Approval Basis and Make Model Eligibility ,,...-.....,,_ Replacement Approved Design Data Eligibility

for Part Number

Retainer 52-1300-43 Modification Identicality per 14 Boeing 737-200 CFR § 21.303, 737-200C licensing agreement 737-300 between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

~\

Doubler, 52-1310-1 Modification Identicality per 14 Boeing 737-200 Outboard CFR § 21.303, 737-200C Saddle licensing agreement 737-300

between Higher 737-400 Planes, Inc. and 737-500 Series AeroTech Services, airplanes Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC STOI625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Part Name

Extension, Inboard Saddle

Part Number

52-1310-3

Approved Replacement for Part Number

Modification


Identicality per 14 CFR § 21.303, licensing agreement between Higher Planes, Inc. and AeroTech Services, Inc. December 4, 2006, per AeroTech Services, Inc. Dwg. No.: Master Drawing List: 52-0001 Rev:F Date: November 17, 2005, or later FAA approved revisions as approved on STC ST01625LA April 15, 2004, reissued November 17, 2004, amended July 12, 2005, or later FAA approved revision.

Make Eligibility

Boeing

Model Eligibility

737-200 737-200C 737-300 737.-400 737-500 Series airplanes

-------------------------------------------------------------------End of Listing----------------------------------------------------

NOTE: The procedures that have been accepted by the supplemental type certificate holder and their cognizant FAA Aircraft Certification Office, for minor changes to original parts used on type certificated products, are Also acceptable for incorporating the same minor changes on identical F AA-PMA replacement parts. The F AA-PMA holder shall be able to show traceably relating to the STC holder on all minor changes incorporated By this procedure. When these procedures are no longer applicable because of completion of the production contract, or termination of licensing agreement or Business relationship, all subsequent minor design changes to the PMA parts must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR Part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for the original F AA-PMA.

) _.--;, ~

-~· .b .:t~ c~ -/;,.;" ~{ ,, (._, z. _ _...-(. l,' "-£'1, !,-

Ford J. Lauer III Manager, San Antonio Manufacturing Inspection

District Office SW-MID0-43

This Supplement is an attachment to your F AA-PMA letter dated: 10-02-01

Date !/z7'c 7

Corporate Aircraft Components Inc. 513 Bryant Road Conroe, Texas 77303

Part Name' Part Number

Scissor CA9535


Modification

Scissor UpperMLG

CAES 11059- Modification 3

PMA No.: PQ0880SW

Supplement No.: 20 Revision No.:


Identicality per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc. and Central Airlines, Inc. dated June 20, 2007, per Central Airlines, Inc. Dwg. No.: CA9535 Date: March 26, 1993, or later FAA approved revisions as approved on STC SAOOOS l WI dated March 26, 1993.

Identicality per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc. and Central Airlines, Inc. dated June 20, 2007, per Central Airlines, Inc. Dwg.No: CAES 11059-3, per drawing list CAES11059 Date: October 28, 1993, or later FAA approved revisions as approved on STC SAOO 111 WI dated October 28, 1993.

Project No.:

Make Eligibility

Model Eligibility

Twin 500B, 500U, SOOS, Commander 690, 690A, and

690B.

Twin 500B, 500U, SOOS, Commander 690, 690A, and

690B

Part Name

Scissor LowerMLG

Part Number


CABS 11059- Modification 4


Identicality per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc. and Central Airlines, Inc. dated June 20, 2007, per Central Airlines, Inc. Dwg.No: CABS 11059-4, per drawing list CAES11059 Date: October 28, 1993, or later FAA approved revisions as approved on STC SAOO 111 WI dated October 28, 1993.

Make Eligibility

Model Eligibility

Twin 500B, SOOU, SOOS, Commander 690, 690A, and

690B

------------------------------------------------------------End of Listing---------------------------------------------

NOTE: The procedures that have been accepted by the supplemental type certificate holder and their cognizant FAA Aircraft Certification Office, for minor changes to original parts used on type certificated products, are also acceptable for incorporating the same minor changes on identical F AA-PMA replacement parts. The F AA-PMA holder shall be able to show traceably relating to the STC holder on all minor changes incorporated by this procedure. When these procedures are no longer applicable because of completion of the production contract, or termination of licensing agreement or business relationship, all subsequent minor design changes to the PMA parts must be submitted in a manner as determined by the ACO. Major design changes (reference14 CFR Part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner'as that for the original F AA-PMA.

~;/:;;-J. Lauer III

ager, San Antonio Manufacturing Inspection District Office

This Supplement is an attachment to your FAA-PMA letter dated: 10-02-01

Date 1 /18/CJ 7

Corporate Aircraft Components Inc. 513 Bryant Road Conroe, Texas 77303

Part Approved

Name • Part Number Replacement for

Axle ED12909-4 Replacement Part MLG IAI ED12909-4

Box A01WW5823641- Replacement Part assembly 513 AOIWW5823641-

513

PMA No.: PQ0880SW Supplement No.: 21

Revision No.:

Projec~~~~~ NOV O 5 2007

Approval Basis and Make Model Approved Design Data Eligibility Eligibility

Identically per 14 CFR § IAI 1124,1124A 21.303, licensing agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated August30,2007,per Israel Aerospace Industries LTD., TC A2SWrev. 13 Dwg. No: ED12909 Rev:G Date: 4/2/1985.

Identically per 14 CFR § IAI 1123, 1124, 21.303, licensing 1124A agreement between Corporate Aircraft Components, Inc, and Israel Aerospace Industries LTD. dated August 30, 2007, per

. Israel Aerospace Industries LTD., Inc., TC A2SWrev. 13

DDA01WW582364I, Rev:IR Date: 7/4/2004.

Part Approved

Approval Basis and Make Model Name

Part Number Replacement for Approved Design Data Eligibility Eligibility

Part Number

Window 343010-501 Replacement Part Identically per 14 CFR § IAI 1124, Fitting 343010~501 21.303, licensing 1124A

agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated August30,2007,per Israel Aerospace Industries LTD., Inc., TC A2SW rev. 13 Dwg.No: DDWW 43430-10 Rev: J Date: 7/11/1999.

Box A01WW5823641- Replacement Part Identically per 14 CFR § IAI 1123, 1124, assembly 511 A01WW5823641 21.303, licensing 1124A

-511 agreement between Corporate Aircraft Components, Inc., and Israel Aerospace Industries LTD. dated August 30, 2007, per Israel Aerospace Industries LTD., Inc., TC A2SWrev. 13 Dwg. No: DDA01WW5823641, Rev: IR dated 7/4/2004.

Box A01WW5823641- Replacement Part Identically per 14 CFR § IAI 1123, 1124, assembly 517 A01WW5823641 21.303, licensing 1124A

-517 agreement bet,veen Corporate Aircraft Components, Inc., and Israel Aerospace Industries LTD. dated August30,2007,per Israel Aerospace Industries LTD., Inc., TC A2SWrev. 13 Dwg.No: DDA01WW5823641 Rev: IR dated 7/4/2004.

Part Name

Bus Bar

Part Number

823641-007

Approved Replacement for Part "1111,.....hr.,,. ....

Replacement Part 823641-007


Identically per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc., and Israel Aerospace Industries LTD. dated August 30, 2007, per Israel Aerospace Industries LTD., Inc., TC A2SW rev. 13 and Dwg. No: DDA01WW5823641 Rev: IR dated 7/4/2004.

Make Eligibility

IAI

Model Eligibility

1123, 1124, 1124A

------------------------------------------------------------End of Listing---------------------------------------------

NOTE: The procedures that have been accepted bY- the supplemental type certificate holder and their cognizant FAA Aircraft Certification Office, for minor changes to original parts used on type certificated products, are also acceptable for incorporating the same minor changes on identical F AA-PMA replacement parts. The F AA-PMA holder shall be able to show traceably relating to the STC holder on all

~, minor changes incorporated by this procedure. When these procedures are no longer applicable because of completion of the production contract, or tennination of licensing agreement or business relationship, all subsequent minor design changes to the PMA parts must be submitted in a manner as determined by the ACO. Major design changes (reference14 CFR Part 21 §§ 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for the original F AA-PMA.

Ford J. Lauer III Manager, San Antonio Manufacturing Inspection

District Office

This Supplement is an attachment to your FAA-PMA letter dated: 10-02-01

Corporate Aircraft Components, Inc. 513 Bryant Road


Conroe, Texas 77303 Revision No.: Project No.:

Date: February 26, 2008

Part Name

Trunnion Pin, AFT

Part Number

ED13098-2

Approved Replacement for Part Number Replacement Part ED13098-2


Identically per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc, and Israe 1 Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TC A2SWRev. 13 Dwg. No: ED13098 Rev:B Date: 5/15/1963, or later FAA approved revisions.

Make Eligibility

IAl

Model Eligibility

1123, 124, 1124A

Flap Bolt 193502-3 Replacement Part Identically per 14 CFR § IAI 1123, 1124, 1124A 193502-3 21.303, licensing

agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TC A2SWRev. 13 Dwg. No: 193502 Rev:M Date: 11/20/1983, or later FAA approved revisions.

---------------------------------------------------------------------End of Listing-------------------------------------------------------N OTE: The procedures that have been accepted by the supplemental type certificate holder and their cognizant FAA Aircraft Certification Office, for minor changes to original parts used on type certificated products, are also acceptable for incorporating the same minor changes on identical F AA-PMA replacement parts. The FAAPMA holder shall be able to show traceably relating to the STC holder on all minor changes incorporated by this procedure. When these procedures are no longer applicable because of completion of the production contract, or termination of licensing agreement or business relationship, all subsequent minor design changes to the PMA parts must be submitted in a manner as determined by the ACO. Major design changes (reference 14 CFR Part 21 § § 21.93 and 21.97) to drawings and specifications are to be handled in the same manner as that for the original FM,-P~ ..

f~>tz~--Ford J. Lauer ID Date 2/26/08 Manager, San Antonio Manufacturing Inspection District Office This Supplement is an attachment to your FAA-PMA letter dated: 10/02/01

FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL

Corporate Aircraft Components, Inc. 513 Bryant Road Conroe, Texas 77303

Part Name

Grommet

Bushing Trunnion

Part Number

ED12902-1

ED12905-2


Replacement Part IAI ED12902-1

Replacement Part ED12905-2


Revision No.: Project No.:

Date: February 26, 2008


Identically per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TC A2SWRev. 13 Dwg. No: ED12902 Rev:A Date: 3/21/1962, or later FAA approved revisions.

Identically per 14 CFR § 21.303, licensing agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TC A2SW Rev. 13 Dwg. No: ED12905, Rev:B Date: 7/10/1962, or later FAA approved revisions.

Make Eligibility

w

w

Model Eligibility

1123, 1124, 1124A

1123, 1124, 1124A

Corporate Aircraft Components, Inc. PMANo.: PQ0880SW 513 Bryant Road Supplement No.: 22 Conroe, Texas 77303 Revision No.:

·--~ Project No.:

Date: February 26, 2008 ~

Approved Approval Basis and Make Model

Part Name Part Number Replacement for Approved Design Data Eligibility Eligibility

Part Number Pin EDI3102-2 Replacement Part Identically per 14 CFR § w 1123, 1124, Retract ED13102-2 21.303, licensing 1124A

agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TC A2SWRev. 13 Dwg. No: ED 13102, Rev:A Date: 4/29/1963, or later FAA approved revisions.

Pin ED13103-2 Replacement Part Identically per 14 CFR § w 1123, 1124, Retract ED13103-2 21.303, licensing 1124A

agreement between ~ Corporate Aircraft

Components, Inc. and Israel Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TC A2~W Rev. 13 Dwg. No: ED13103, Rev:A Date: 4/30/1963, or later FAA approved revisions.

Trunnion ED13097-2 Replacement Part Identically per 14 CFR § w 1123, 1124, Pin, Fwd ED13097-2 21.303, licensing 1124A

agreement between Corporate Aircraft Components, Inc. and Israel Aerospace Industries LTD. dated February 5, 2008, per Israel Aerospace Industries LTD., TCA2SWRev. 13 Dwg. No: ED13097

,,,--.._ Rev:B ',

Date: 4/29/1963, or later FAA approved revisions.

FEDERAL AVL .. \ TlON ADl\UNISTRA TION - PARTS MANL'F ACTURER APPROVAL

Corporate Aircraft Components. Inc. 513 Bryant Road

P\ti\ No. PQ0880SW Supplement !\o. 23

Conroe Texas 77303 Date: I 0114/20 I 0

Approved Replacement fr,r Part

Part Name Part Number Number

Seal 5:!-l 140-5 5 :;-1 140-5

ApproYal Ba.;;is and Approved Design Data

\fake Efo.dhilit, ... .

ldcntical1,- per l 4 CTR ~ Boeing ::! 1.303. lkensing agreement hetwccn Corporate Aircraft ComfX)ncnts. Inc. and :\croTech Ser,·ices. Inc .. dated July 2. 2007. DWG No: 5]-1140

Q~tc: July 23. 2010. or later FAA appro\ed revisions a._;. appm\'ed on STC Sl01625LA amended July J 2_ 2005. or lat~r FAA apprO\,Cd TC\ isi{ltl.

Model Elii!ibilitv :r: :·

7H-200 737-200(' 737-300 737-400 7J7-500 Series Airplanes

----------------------------------------------- End t)f l~isting --------------------------------------------------

NOTE: The procedures that haw been accepted by the t} pe certificate or TSO .authorization hoidcr and their co,.,:::!nizam FAA Aircraft Certification Office~ l<Jr minor changes to original parts used on typecertificated products. are also acceptable t(Jf' incorporating. the same minor changes on identical PMA replacement parts. The P\·tA holder must be able to show tract.YJ.bility relating to the TC. STC. or TSO authorization holder on all minor chang<.."S incorporated by this J)foccdure. When these procedures arc no longer applicable because of completion of the production contract. 0t tcm1ination of the licensing agreement or business relationship, all subsequent minor design changes to the PMA pans must be submitted in a manner as detem1ined by the ACO. Major design changes (reference t 4 Cl-'R ** :! 1.93 and 21. 97; to drawine.s and specifications are to be handled in the same manner as that for an ori2inal PM A.

'JRIGiNAL S\GNEO BY ... :=-ORD .J LAUER

Ford J. I .• mer \fanagcr. San Antonio Manufacturing

Inspection District Office. ASW-MID0-43

rhis Supplement is an attachment to your FAA-P\iA approval lcncr dated: 6/ l 0/Q& ():\ I 83\4JSHARE0\43 Facilities\PQ0880 Corporate Aircraft Components lnc\Production Apprornl\PQ0880 PMA02J.doc

FEDERAL A VIATI01\ ADMINISTRATION - PARTS \11Al\l.iFACTURER APPROVAL

Corporal~ Aircraft Component~. lrn.:. 51 3 Br} ant Road Conroe. T~xas 77'303

Part Name

Pm1~ as listc<l on MDL

,\ppn.1,cd Replact:mcnt fr,r Part

Part Number Numhcr

Parts as listed Mndifo.:ation on MDL pat1s

PMA No. Supph=ment No.

Date:

PQ0880SW 2-i 10/12/2011

Approval Basis and ivfakc \1odcl EligihiJity Appnm:d Design Data Eliuihilit)

ldcnticalit~ pt:r 1-l CFR * Bodng 21.303. licensing. agrccmcnl hcl\,ccn (\xporatc Aircraft Components. Inc. and ALRA. LLC dba A\!roTcch Sen ices. 1 nc ., <lated September t. ~01 L D\VG_ No: 52-000 I l{c,.: H [)JlJ~: July 23. '.!O I 0. or later h\A appnwed revisions.

737-200 737-200(' 737-300 737.400 7~7-500 Series Airplanes

-----------------------------------------------~ End of L.i s.ti ng -------------·-------------------------------------

NOTE: The procedures that have been accepted by the t}JJC certificate or TSO authorization holder and their cogni;:ant FA;\ Aircraft Certification Office_ frlr minor changes to original parts used on t)pe..:c11ifo.::..itcd products. arc also acceptable for incorporating the same minor changes on identical PMA replacement pa11s. The PMA holder must he ahlc to show rraci..-ability relating. to the TC STC. or TSO authorization holder on an minor changes im.:orpnratcd by this procedure. \Vhen these procedures arc m.1 longer applicable bc~ausc of comp Jct ion of the prodm.:tion l'.ontracL or tcnnination i)f the licensing agreement Qf business relationship. all subsequent mim)r design chang.:s lo the PMA parts must be -;ubmitte<l in a manner as dch:m1incd b:v the ACO. :\:1,~ior de:-.ign changes (reference 14 CFR *~ 21 .93 and 1 l .97} to drm.\ ings and spccifo:ati<ms are to he handled in the same manner as that lc.>r an original Pl\1/\.

Ford J. I .aucr Ill ~fanagcr. San Antonio Manufacturing

Inspection District Office. AS\\'-Ml00-43

Date

U.S. Department of Transportation

Federal Aviation Administration

June 14, 2013

Mr. Barry Cain Higher Planes, Inc. 513 Bryant Road Conroe, TX 773 03

Rotorcraft Directorate San Antonio Manufacturing Inspection District Office

10100 Reunion Place, Suite 650 San Antonio, Texas 78216 Phone: (210) 308-3360 Fax: (210) 308-3370


Dear Mr. Cain:

In accordance with the provisions of Title 14, Code of Federal Regulations (14 CFR), part 21, Certification Procedures for Products, Articles, and Parts, subpart K, the Federal Aviation Administration has found that the design data, based on Test and Computation submitted by Higher Planes, Inc. with your letter dated February 28, 2013, meets the airworthiness requirements of the regulations applicable to the products on which the articles are to be installed. Additionally, the FAA has determined that Higher Planes, Inc. has established the quality system required by§ 21.307 at 513 Bryant Road, Conroe, Texas 77303. Accordingly, Parts Manufacturer Approval (PMA) is hereby granted for production of the replacement articles listed in the enclosed Supplement No. : 25.

You are reminded that the provisions of 14 CFR, parts 21 and 45 noted in our PMA letter of approval dated February 5, 2013, also apply to the enclosed PMA Listing-Supplement No. 25. The enclosed supplement should be retained with the PMA letter as evidence of approval to produce the articles concerned.

Sincerely,

~fff:J 1~~";'!!a~e?ifi ey- r;;v-Manager, San Antonio Manufacturing Inspection District Office

Enclosure

cc: AIR-140



FEDERAL A VIA Tl ON ADMINISTRATION - PARTS MANUF ACTURER~PPRQ\{!\Lt,·:~,~:;..~;;,,;~ii1.~\

HIGHER PLANES, INC 513 BRYANT ROAD CONROE, TX 77303

Article Name Part Number

Plunger 291005-01

Seat- 291005-02 Unloading

Poppet 291005-03

Screen 291005-04

Poppet 291005-05


Part Number

ED12267

ED12268

Sub-Component of A7844

Sub-Component of ES12491

A6668


Test and Computations per 14 CFR § 21.303, DWG No: 291005

Rev: Bl Date: 05/01 /13

or later FAA-approved revisions


Rev: Bl Date: 05/01 /13



Rev: Bl Date: 05/01 /13



Rev: Bl Date: 05/01/13



Rev: Bl Date : 05/01/13


PMA. No.: PQ0880SW SUPPLEMENT No.: 25 DATE: i.JHN 1 4Zuu

Mak~, . \WJ'>#;.· M Oc9tli1t. Eligibility ·"' Eligibility .

500-A, 500-8, 500-U, 500-S, 560-F, 681, 690, 685, 680F,

Twin 690A, 6908 , 680FL, Commander 690C, 680FL(P),

690D, 680T, 695, 680V, 695A, 680W,

6958

500-A, 500-8, 500-U, 500-S, 560-F, 681, 690, 685, 680F,


6900, 680T, 695, 680V, 695A, 680W,

6958

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685, 680F,


6900, 680T, 695, 680V, 695A, 680W,

6958

:iOO-A, 500-B, 500-U, 500-S, 560-F, 681 , 690, 685, 680F,

Twin 690A, 6908, 680FL, Commander 690C, 680FL(P),

6900, 680T, 695, 680V, 695A, 680W,

6958

500-A, 500-8 , 500-U, 500-S, 560-F, 681 , 690, 685, 680F,


6900, 680T, 695, 680V, 695A, 680W,

6958


HIGHER PLANES, INC PMA. No.: PQ0880SW 513 BRYANT ROAD SUPPLE~N~ ~oi ~ . CONROE, TX 77303 DATE: ~ - .1 ' • ; "

Approved Replacement For Approval Basis and Make Model

Article Name Part Number Part Number Approved Design Data Eligibility Eligibility

Test and Computations per 500-A, 500-B, 500-U, 14 CFR § 21.303, 500-S, 560-F, 68 1, DWG No: 291005 690, 685, 680F,

Data Tag 291005-06 No OEM PN Rev: Bl Twin 690A, 690B, 680FL,

Indicated Date: 05/01/13 Commander 690C, 680FL{P),

or later FAA-approved 690D, 680T, 695,

revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-8, 500-U, 14 CFR § 21.303, 500-S, 560-F, 68 1, DWG No: 291005 690, 685, 680F,

Transfer Seat 291005-07 ES12491 Rev: B l Twin 690A, 690B, 680FL,

Assembly Date: 05/01/13 Commander 690C, 680FL(P),


revisions 680V, 695A, 680W, 695B


Warning Tag 291005-08 No OEM PN Rev: Bl Twin 690A, 690B, 680FL,

Indicated Date: 05/01/13 Commander 690C, 680FL(P),


revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-B, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681, DWG No: 291005 690, 685, 680F,

Ball 291005-09 ELA-16-18 Rev: Bl Twin 690A, 690B, 680FL, Date: 05/01/13 Commander 690C, 680FL(P),


revisions 68QV, 695A, 680W, 695B


Seat & Guide 291005-12 A6670 Rev: B l Twin 690A, 690B, 680FL, Date: 05/01/1 3 Commander 690C, 680FL(P),




Ball 291005-13 ELA16-7 Rev: Bl Twin 690A, 690B, 680FL,

Date: 05/01/13 Commander 690C, 680FL(P),



... ~


HIGHER PLANES, INC PMA. No.: PQ0880SW 513 BRYANT ROAD SUPPLEff ri: 25 CONROE, TX 77303 DATE: 2U13




Seat (OB) 291005-14 ED12161 Rev: Bl Twin 690A, 690B, 680FL,


or later FAA-approved 6900 , 680T, 695,



Seat (IB) 291005-15 ED12492 Rev: Bl Twin 690A, 690B, 680FL, Date: 05/01/13 Commander 690C, 680FL(P),




Placard 291005-16 No OEM PN Rev: BJ Twin 690A, 6908, 680FL, Indicated Date: 05/01/13 Commander 690C, 680FL(P),


revisions , 680V, 695A, 680W, 695B

Test and Computations per 500-A, 500-8, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681, DWG No: 291005 690, 685, 680F,

Cap- 291005-18 ED12270 Rev: Bl Twin 690A, 690B, 680FL, Unloading Date: 05/01/13 Commander 690C, 680FL(P),

or later FAA-approved 6900, 680T, 695,


Test and Computations per 500-A, 500-8, 5oo~u. 14 CFR § 21.303, 500-S, 560-F, 681, DWG No: 291005 690, 685, 680F,

Screen- 291005-19 ED12156 Rev: Bl Twin 690A, 690B, 680FL, Transfer Date: 05/01/13 Commander 690C, 680FL(P),




Spring 291005-20 A7968 Rev: Bl Twin 690A, 690B, 680FL,




3/5

FEDERAL AVIATION ADMINISTRATION -PARTS MANUFACTURERAPPROVAL

HIGHER PLANES, INC PMA. No.: PQ0880SW 513 BRYANT ROAD SUPPLEMENT No.: 25 CONROE, TX 77303 DATE: •<4 « ~ i -.-: ., .... ,...,,I'-, ,, ' ft . ,i"




Spacer 291005-21 ED12160 Rev: Bl Twin 690A, 6908, 680FL,

Date: 05/01/13 Commander 690C, 680FL(P), or later FAA-approved 690D, 680T, 695,

revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-8,500-U, 14 CFR § 2 1.303, 500-S, 560-F, 681, DWG No: 291005 690, 685, 680F,

Seat 291005-22 Sub-Component of Rev: Bl Twin 690A, 6908, 680FL,

A7844 Date: 05/01/13 Commander 690C, 680FL(P), or later FAA-approved 690D, 680T, 695,

revisions 680V, 695A, 680W, 6958


Nut-Lock 291005-24 A6473 Rev: Bl Twin 690A, 690B, 680FL, Date: 05/01/13 Commander 690C, 680FL(P),


revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-8, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681 , DWG No: 291005 690, 685, 680F,

Guide-291005-25 ED12269

Rev: Bl Twin 690A, 690B, 680FL, Unloading Date: 05/01/13 Commander 690C, 680FL(P),


revisions 680V, 695A, 680W, 6958


Spacer 291005-26 ED12160 Rev: Bl Twin 690A, 6908, 680FL, Date: 05/01/13 Commander 690C, 680FL(P),


revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-8, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681 , DWG No: 291005 690, 685, 680F,

Plug 291005-27 Sub-Component of Rev: Bl Twin 690A, 6908 , 680FL,

A7844 Date: 05/01 /13 Commander 690C, 680FL(P), or later FAA-approved 690D, 680T, 695,


FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACT'MRER APPR0V AL h

HIGHER PLANES, INC PMA. No.: PQ0880SW 513 BRYANT ROAD SUPPLEMENT No.: 25 CONROE, TX 77303 DATE:

JUN i iJ .3


Article Name Part Number Part Number Approved Design Data ,jligibility Eligibility

Test and Computations per 500-A, 500-8 , 500-U, 14 CFR § 21.303, 500-S, 560-F, 681, DWG No: 291005 690, 685, 680F,

Screw-Plug 291005-28 ED12494 Rev: Bl Twin 690A, 6908 , 680FL, Date: 05/01/13 Commander 690C, 680FL(P),


revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-B, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681 , DWG No: 291005 690, 685, 680F,

Spring 291005-29 A57 16 Rev: Bl Twin 690A, 690B, 680FL,


revisions 680V, 695A, 680W, 6958

Test and Computations per 500-A, 500-B, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681 , DWG No: 291005 690, 685, 680F,

Spring 291005-30 A6590 Rev: Bl Twin 690A, 690B, 680FL,



Test and Computations per 500-A, 500-B, 500-U, 14 CFR § 21.303, 500-S, 560-F, 681,

Poppet & DWG No: 291005 690, 685, 680F,

Seat 291005-31 A7844 Rev: Bl Twin 690A, 6908 , 680FL,

Assembly Date: 05/01/13 Commander 690C, 680FL(P),



--------------------End of Listing-------------------NOTE:

I) Provide minor design changes in a manner as determined by the ACO. Handle major design changes to drawings and specifications in the same manner as that for an original FAA-PMA.

2) The FAA approved ICA for the above articles with their designs. These ICA may refer to those of the respective articles from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement articles.

ke referral statements or supplemental ICA readily available per 14 CFR 21.50.

4t::llib~~ Ford J. Lauer III Manager, Manufacturing Inspection District Office





Article Name Part Number Approved Replacement For Part Number

Channel 4950008-71HP 4950008-71


PMA NO. P00880SW SUPPLEMENTNO. 26 DATE 11/19/2013

Make Eligibility

Model Eligibility

Test and Computation Learjet 31,31A,35,35A (C-21A), Per 14 CFR § 21.303,

With HP DWG: 4950008, Rev. B, OTO: 9/11 /13 or Later FAAApproved Revision

36,36A

-------------------End of Listing--------------------

NOTE:

1) Provide minor design changes in a manner as determined by the ACO. Handle major design changes to drawings and specifications in the same manner as that for an original FAA-PMA.

2) The FAA approved ICA for the above articles with their designs. These ICA may refer to those of the respective articles from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement articles. Make referral statements or supplemental ICA readily available per 14 CFR 21.50.

~~-~ \ ._,/ S. Frances Cox, Manager

Special Certification Office, Aircraft Certification Service

1/2

~:2-~ /Jr.ln1t1 L. ~ vie v Pov Ford J. Lauer III, ~mager San Antonio Manufacturing

Inspection District Office, MID0-43

·.___.

U.S. Depa1ment of Transportation Fede1al Avlaflon Administration



Article Name Part Number Approved Replacement for Part Number

Drum AssemblyDrive Mechanism, Inboard Aft Flap

Drum AssemblyDrive Mechanism. Inboard Aft Flap

65C30824-tHP 65C30824-1

65C30824-2HP 65C30824 -2

PMA NO: ; ·•· POOS80SW SUPPLEMEN1 NO: 27 ------DATE: 2~2014


Test and Computation per 14 CFR § 21.303 DWG No: 65C30824 _&aA Date: 06/06/2013 or later FAA Approved revisions

Make Eligibility

Boeing

Test and Computation Boeing per 14 CFR § 21.303 DWG N2: 65C30824 Rev:A Date: 06/06/2013 or later FAA Approved revisions

Model Eligibility

737-300 Series 73 7-400 Series 737-500 Series

737-300 Series 737-400 Series 737-500 Series

End of Listing------------------------------------------------------------

NOTE:

1. Provide minor design changes in a manner as determined by the ACO. Handle major design changes to drawings and specifications in the same manner as that for an original F AA-PMA.

2. The FAA approved ICA for the above parts with their designs. These ICA may refer to those of the respective parts from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement parts. Make referra1 statements or supplemental ICA readily available per 14 CFR 21 .50.

. Frances Cox, Mana Special Certification Office, Aircraft Certification Service

Ford Lauer, Manager Manufacturing Inspection District Office, SW MID0-43



FEDERAL A VIA TI ON ADMINISTRATION - PARTS MANUFACTURER APPROVAL

Higher Planes, Inc dba Central Texas Aircraft Parts

1216D Sidney Baker South

Kerrville, TX 78028

Article Name

Article Number

Approved Replacement For Article Number

Switch Plate 45-12370-lHP 45-12370-1 Assy.

Actuator Assy.

Plug & Switch Assy.

45-12449-3HP 45-12449-3

45-0008-07HP 45-0008-7

Pivot Arm 45-12368-9HP 45-1 2368-9


Test and Computations per 14 CFR 21.303 , DWG No: 45-12370, Rev: IR, Date: 11/25/1 3 or later FAA-approved revisions

Test and Computations per 14 CFR 21.303 , DWG No: 45-12449, Rev: IR, Date: 11/25/1 3 or later FAA-approved revisions

Test and Computations per 14 CFR 21.303 , DWG No: 45-0008, Rev: IR, Date: 11 /25/ 13 or later FAA-approved revisions

Test and Computations per 14 CFR21.303 , DWG No: 45-12368, Rev: IR, Date: 11/25/1 3 or later FAA-approved revisions

PMA NO. PQ0880SW

SUPPLEMENT NO. 28

REVISION IR

DATE~~~---=6~/~30=/~1=6~

MakeffCH Model/Series Eligibility Eligibility

Learjet

Learjet

Learjet

Learjet

35 , 35A (C-21A), 36, 36A, 55, 55B, 55C

35, 35A (C-21A), 36, 36A, 55, 55B, 55C

35, 35A (C-21A), 36, 36A, 55, 55B, 55C

35, 35A (C-21A), 36, 36A, 55, 55B, 55C

Pg. I of2


Higher Planes, Inc dba Central Texas Aircraft Parts

1216D Sidney Baker South

PMA NO. PQ0880SW

SUPPLEMENT NO. 28 Kerrville, TX 78028

Article Name

Spring

Bumper Plate

Article Number

Approved Replacement For Article Number

45-12356-IHP 45-12356-1

45-12256-3HP 45-12256-3


Test and Computations per 14 CFR 21.303, DWG No: 45-12356, Rev: IR, Date: 11/25/13 or later FAA-approved revisions

Test and Computations per 14 CFR 21.303 , DWG No: 45-12256, Rev: IR!, Date: 4/08/16 or later FAA-approved revisions

REVISION IR DATE 6/30/16

Make/TCH Model/Series Eligibility Eligibility

Learjet

Learjet

35, 35A (C-21A), 36, 36A, 55, 55B, 55C

35, 35A (C-21A), 36, 36A, 55, 55B, 55C

----------------------------------------------------------------END OF DAT A-------------------------------------------------------------

0 ENERAL NOTES:

Provide minor design changes in a manner as determined by the ACO. Process major design changes to drawings and specifications in the same manner as that for an original FAA-PMA.

The FAA accepted the I CA approach for the above articles with their designs. These I CA may refer to those of the respective articles from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement articles. Make referral statements or supplemental ICA readily available per 14 CFR 21 .50.

V Acting Manager, Fort Worth Aircraft Certification Office

Ford Lauer, Manager San Antonio Manufacturing Inspection District Office

Pg. 2 of2



Rotorcraft Directorate 10100 Reunion Place, Suite 650 San Antonio Manufacturing Inspection District Office Sari Antonio, Texas 78216

Phone: (21 0) 308-3360 Fax: (21 0) 308-3370

June 14,2013

Mr. Barry Cain Higher Planes, Inc. 5 13 Bryant Road Conroe, TX 77303


Dear Mr. Cain:

In accordance with the provisions of Title 14, Code of Federal Regulations (14 CFR), part 21, Certification Procedures for Products, Articles, and Parts, subpart K, the Federal Aviation Administration has found that the design data, based on Test and Computation submitted by Higher Planes, Inc. with your letter dated February 28, 2013, meets the airworthiness requirements of the regulations applicable to the products on which the articles are to be installed. Additionally, the FAA has determined that Higher Planes, Inc. has established the quality system required by 5 21.307 at 513 Bryant Road, Conroe, Texas 77303. Accordingly, Parts Manufacturer Approval (PMA) is hereby granted for production of the replacement articles listed in the enclosed Supplement No.: 25.

You are reminded that the provisions of 14 CFR, parts 2 1 and 45 noted in our PMA letter of approval dated February 5,2013, also apply to the enclosed PMA Listing-Supplement No. 25. The enclosed supplement should be retained with the PMA letter as evidence of approval to produce the articles concerned.

Sincerely,

Manager, San Antonio Manufacturing Inspection District Office

Enclosure

cc: AIR- 140



FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURERAPPR,Q,Y4,pI;.i:2;2;r8ai.* , .. .


Approved Replacement For Approval Basis and

Article Name Part Number Part Number Approved Design Data

Plunger

Seat- Unloading

Poppet

Screen

Poppet

291 005-03 Sub-component of A7844

291 005-04 Sub-component of ES12491

Test and Computations per 14 CFR 4 21.303, DWG No: 291005

Rev: B1 Date: 05/01 / I 3



Rev: B1 Date: 05/01 / I 3



Rev: B1 Date: 05/01/13



Rev: B1 Date: 0510 1 / I 3



Rev: B1 Date: 05/01 11 3


PMA. No.: PQ0880SW SUPPLEMENT No.: 25 DATE: :iB@t! 1 A :.;: _ . , ;:

Make #+-,* M~gQpp~.. Eligibility " Eligibility

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,

Twin 690A, 690B, 680FL, Commander 690C, 680FL(P),

690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V. 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B



PMA. No.: PQ0880SW SUPPLEyyf i NPJ: 3, DATE:


Article Name Part Number Part Number Approved Design Data Make Model

Eligibility Eligibility

Test and Computations per 14 CFR 5 21.303, DWG No: 29 1005

Rev: B1 Date: 0510 111 3


No OEM PN lndicated

Twin Commander Data Tag 291 005-06

Test and Computations per 14 CFR 8 2 1.303, DWG No: 29 1005

Rev: B1 Date: 05/01/13


Transfer Seat 291 005-07 Assembly

Twin Commander


Rev: B1 Date: 05/01/13


No OEM PN lndicated

Twin Commander Warning Tag 291 005-08


Rev: B1 Date: 05101 I1 3


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,

Twin 690A, 690B, 680FL, Commander 690C,680FL(P),

690D, 680T, 695, 680V, 695A, 680W,

695B

Ball

Test and Computations per 14 CFR $ 21.303, DWG No: 291005

Rev: B1 Date: 05/01 / I 3


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

Seat & Guide 291 005-12

Test and Computations per 14 CFR $21.303, DWG No: 291005

Rev: B1 Date: 05/01/13


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,

Twin 690A, 690B, 680FL, Commander 690c, 680FL(P),

690D, 680T, 695, 680V, 695A, 680W,

695B

Ball


HIGHER PLANES, INC PMA. No.: PQ0880SW 513 BRYANT ROAD S U P P L E V H flo.: 25 CONROE, TX 77303 DATE: 4 2m3


Article Name Part Number Part Number Approved Design Data

Seat (OB) 291 005-14

Seat (IB) 291 005-1 5

Placard 291005-16

Cap- Unloading 291 005-1 8

Screen- 291 005-1 9 Transfer

Spring

No OEM PN Indicated

Test and Computations per 14CFR$ 21.303, DWG No: 291005

Rev: B1 Date: 05/01/13



Rev: B1 Date: 05/01/13


Test and Computations per 14 CFR § 21.303, DWG No: 291 005

Rev: B1 Date: 05/01/13



Rev: B1 Date: 05/01/13


Test and Computations per 14 CFR $21.303, DWG No: 291005

Rev: B1 Date: 05/01 /I 3



Rev: B1 Date: 05/01/13


Make Model Eligibility Eligibility

Twin Commander

500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


6908,68OT, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B



PMA. No.: PQ0880SW SUPPLEMENT No.: 25 DATE:

' 4 " ' 5 4 l : *& , 1 '


Article Name Part Number Part Number Approved Design Data Make Model

Eligibility Eligibility


Rev: B1 Date: 05/01/13


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D,680T, 695, 680V, 695A, 680W,

695B

Spacer


Rev: B1 Date: 05/01/13


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,

Twin 690A, 690B, 680FL, Commander 690c, 680FL(P),

690D, 680T, 695, 680V, 695A, 680W,

695B

Sub-component of A7844 Seat


Rev: B1 Date: 05/01/13


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

Test and Computations per 14 CFR $21.303, DWG No: 29 1005

Rev: B1 Date: 05/01/13


500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

Guide- 291 005-25 Unloading


Rev: B1 Date: 0510 1 11 3


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

Spacer


Rev: B1 Date: 05/01 / I 3


500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

Sub-component of A7844 Plug

FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL i ,


PMA. No.: PQ0880SW SUPPLEMENT No.: 25 DATE:


Article Name Part Number Part Number Approved Design Data gligibility Eligibility -

Screw-Plug 291 005-28

Spring

Spring

Poppet & Seat 291 005-31

Assembly


Rev: B1 Date: 05/01/13



Rev: B1 Date: 05/01/13


Test and Computations per 14 CFR § 21.303, DWG No: 29 1005

Rev: B1 Date: 05/01/13



Rev: B1 Date: 05/01/13


Twin Commander

500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 68 1, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

500-A, 500-B, 500-U, 500-S, 560-F, 681, 690, 685,68OF,


690D, 680T, 695, 680V, 695A, 680W,

695B

.................... End of Listing -------------------- NOTE:


2) The FAA approved ICA for the above articles with their designs. These ICA may refer to those of the respective articles from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement articles.

e referral statements or supplemental ICA readily available per 14 CFR 21 -50.

Ford J. Lauer I11 Manager, Manufacturing Inspection District Office

U.S. Department of Transportation Federal Aviation Adminisfration

FEDERAL AVIATION ADMTNISTRATION - PARTS MANUFACTURER APPROVAL


PMA NO. P00880SW SUPPLEMENT NO. 2 6 DATE 1 1 / 1 9 / 2 0 1 3

Article Name Part Number Approved Approval Basis and Make Model Replacement For Approved Design Data Eligibility Eligibility Part Number

Channel 4950008-71 HP 4950008-71 Test and Computation Learjet 31,31 A, 35,35A Per 14 CFR 5 21.303, (C-2 1 A), With HP DWG: 4950008, Rev. 36,36A B, DTD: 911 111 3 or Later FAA- Approved Revision

------------------- End of Listing ---------- - ---------

NOTE:


2) The FAA approved ICA for the above articles with their designs. These ICA may refer to those of the respective articles from the holders of type certificates. Otherwise, provide supplemental ICA for differences in the replacement articles. Make referral statements or supplemental ICA readily available per 14 CFR 21 S O .

- = = -7- - S. Frances Cox, Manager Special Certification Office,

Aircraft Certification Service

Ford J. Lauer 111, ~ a n a g e r &Y

San Antonio ~ a n u f a c G i n g Inspection District Office, MIDO-43

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