Appromg A~1at1on 2. Form T rackmg No Authonty FAA/UNITED ... … · cmm 32-10-08 rev, 05 datbd nov...

JI

-.., .., .., _.., .. ... ..

.. ORI

1 Appromg National A~1at1on 2. 3 Form T rackmg No Authonty I Country

AUTHORIZED RELEASE CERTIFICATE FAA/UNITED STATES FAA 13/43826

FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

4. Orgamsation NamE and Address Messier Services Americas, S.A. de C.V. 5

Work Order Nurriler Av. La Noria 131, Parque Industrial llueretaro

711776.1.1 nuer6taro, Oro, M6xico, CP 76220 Telephone : + 52 (442) 192 5800 Fax : +52 1442) 192 5801 Contract/ Invoice Nurriler

Certificata No. MXVY496Y 9-77036

6 Item 7 Oescriptmn B Part Number 9. Ehg1b1hty . 10. Quantity : 11 Senal I Batch Number 12. Status/~rk

1 MLG Db.G STRUT ASSY 10200-553 N/A. 1 DCL3801/99 OVERHAULED

13 Remarks ·

THIS COMPONBN'l' WAS OVBRHAtrLBD IAW MBSSIU DOWTY INC. CMM 32-10-08

REV, 05 DATBD NOV 09/2010.

TSN: 24173.6 CSN: 26567 TSO: 00:00 CSO: 0

TOTAL TIMBS AND TOTAL CYCLES HAVl! BEEN PROVIDED BY THE CUSTOMER.

NON-INCIDENT LETTER PROVIDBD BY THE CUSTOMER

ALL DETAILS OF WOll CARRIED Otl'T PBR won ORDER 711776. l.1

AD'S, SB'S EMBODIED: NONE

CONCBSSIONS BMBODIBD: RO 13/036 AND RO 13/047

14. Certifies the item idenllfied above were manu~ 19. [FJ_14 CFR 43.9 Return to Service D OthBr regulation specified in Block 13

D Approved design data and are in condition for safe operation. Certifies that unless otherwise specified in block 13, the work identified in Block 12 and described in

D Non-approved design data specified in Block 13 Block 13 was accomplished in accordance with Title 14, Code Of Federal Regulations, part 43 and in respect to that work, the items are approved for ret1 n to service..

15 Authon2ed Signature :----------- 16 Approval I Author12at1on No 20 Authonzed S1gnat~ ) J tESSIER 21 Approval I Cert1f1cate No MXVY496Y - 212 . I I I I ,:-]' ; '\ MSMly

l~o,Printed) 18 Date 22- Name (Typed or PMtl!di ,. I. l. ,.

23 Date lm/d/yl MAR/26/2013 0 GARC A \

User / Installer ResponS1biliti ., 1 It 11 important to unaeratana tnat tne ex11tence ot tne aocument 11on1 aon not 1utomatii:111y conat1tute authority to IQltlU tne part I component I 1U11111bly - \ Z Wher1 thl user I u11t1ll1r pwform work IQ 1ccord1nc1 with the national regul1t1on1 of an 11rwarthi111111 authority d1Herant than thea1rwarth1n•• 1uthor1ty of thl country 1pec1f11d 1n block 1, 1111 aHntlal that the u• / IQ1t1llor IJIIIUrn that h11 I her airwarthlnna

authority accepts part, I cam,an•ts / as11111bhn from the a1rwartlunn1 authority of the country 1pec1f1ed ,n black 1. 3 Stltementl IQ Blach 14 and 19 d1 not can1t1tute 1nat1ll1t11n cert1f1catlon In all cHn, 11rcr1ft 1T111nt•ance record I must contllQ an 1Qltlll1hon cert1f1cat1on 111ued IQ 1ccardance with the nation.I regulatlan1 by the user/ 1nat1ller before the aircraft may be flown

FAA Form 8130 3 01 m I mStaner must cross cnecK a11g1uuny wnn appucau,a 1ecnmca1 oata NSN 0052 00 01Z 9005

• • • • • • • • • .ii .. ~

~ -~

• ii .. • • • • • • .I MSM• fonr OAF 151

R.,.. On1•~~1 20 Jan 09

P/N:

DRAG STRUT ASSY, MLG

10200-553 S/N: DCL3801/99

DATE MAR 19 1013

• • • • • • • • • • • • • • • • • • • • • • • • •

Equipment: ORAQ STRUT ASSY, MLQ

FAA FORM 8130-3

Identification Sheet:

Equipment historical data:

List of sub-assemblies:

List of LIFE LIMITED PARTS:

Modification Status

Airworthiness directives:

CONCESSIONS

SsAFRAN Messier-Bugatti-Dowty

S/Ns OCL3801/99

CONTENTS

PREVIOUS OPERATOR STATEMENTS(NON INCIDENT, LLP PARTS CHANGED IN SERVICE,CSN/TSN)

O.B.M. CERTS FOR NEW LLP / LRU ITEMS

MSMX Form QAF-1S8 R.v o,;,,nal 20 Jan 09

Page: 1

Front Cover

Pages 2

3 4

5

6

7

ATTACHMENT 1

2

3

DATE MAR lg ]013

• • • • • • • • • • • • • • • • • • • • • • • • •

~ 1 ~ ~ " '""I''~ • '< ' -,1 > ~ I!' ' t , - ' ~4'T • = 1 ! I , ', l 1

• ' ' > '

t - -~- ._..:a::,.. ___ - - - • - -u -----------·---'- --" ~· . . . .

Bquipment,

MSMltFormQAF-151 llev Orem.al 20 Jan 09

DRAG STRUT ASSY. IILQ

SsAFRAN Messler-Bugatti-Dowty

S/N1 DCL3801/99 .. ,. ... 2

CONMUTAIR

STAMP DATE MAR 19, 2013

• • • • • • Equipment, DRAG STRUT ASSY 1 MLG

II Equipment Historical Data

• • • • • • • • • • • • • • • • • •

/JalpaliDn



MSMX Form ClAF•lSI FIN Oncinal 20 11n 09


S/N, DCL3801/99

,, '1,11 --~ Ptlrt N- SerWN~kr

10200-553 OCL3801/99

10200-553 DCL3801/99

, ,,

Date

DEC 12, 2012

MAR 19, 2013

Pagei 3

"

i. '

~

, :-: 1-1r:; 't,~i. :r,,.· ' ,,,,

R.-u; CSN 24173 6

TSN 26~67

CSN: 24173 6 TSN: 26567 CSO: 0 TSO: 0000

STAMP \e) DATE MAR 19,2013

• • • • • • • • • • • .. .. • • • • • • • • • • •

Equipment: DRAG STRUT ASSY, MLG

Qty Description

, SHOCK STRUT ASSY

OYH ~ Overtiauled

MSMXkir"'UAI' I.Sa RN ~,nal 10 l•n 09

SsAFRAN Messier--Bugatti-Dowty

S/N: DCL3801/99 Pages •

List of Sub-assemblies/Line replacement units

Part number Sarlsl number STATUS CONCESSION

10200-553 L3801/99 OVH ----

MOD = Modified REP = Repaired INSP = Inspected TST =Tested NEW= Manufacture Component N/R Not Required

TSN/cSN a.re intcrmatioos rscord@d under rsspoo«abilitv ot thn custamsr

STM-1P DATf MAR 19 2013

• • • • • •

• • ·• ·• I

1. I

• • • • • • • • • •


Equipment: DRAQ STRUT ASSY, MLG S/N: DCL3801/99 Page: 5

List of Life Limit Parts

Qty DescrlptJon ,..,.,t Numve1 ,,.,-,.numDIK

Serial Number Machinlnn sub a·-· CSN cso TSN TSO STA1VS • CONCESSION

1 Drag Strut $/A 10204-13 10205-553 DCL 3839 26567 0 24173 6 00 00 OVH RO 13/036

1 Pin, Shock Strut ---- 10216-551 DCL 3869 26567 0 24173 6 00 00 OVH RO 13/047

1 Pm, Retraction Actuator -- 10212-551 DCL 3590 26567 0 24173 6 00 00 OVH --

OYH • Overhauled MOD :: Modified REP "Repaired INSP ::: Inspected TST :Tested NEW• Manufacture Component N/R Not Required

T$NICSN ara 1nformat1oos recorded under r««eonsabi,Htv et the cu«tame.r LIFE LIMIT PART LISTED ON BOMBARDIER Manufactures Approved Documents Raf. Part 2 Rev.17 of MPM Airworthiness Limitations dated MAR. 1612011.

MSMX Fo,m Q.AF-1!,1

Re-. Or,1inal 20 Ja~ 09 STAMP ®i DATE MAR 19,2013

• •• • • • • • • • • • •• • • • • • • • • • • • • •


Equipment, DRAG STRUT ASSY, MLG S/N, DCL3801/99

Modification Status

ALL SERVICE BULLETINS ANO SERVICE LETTERS APPLIED IN SHOP ARE AT THE LATEST REVISION IN USE

I Customa- ilequlI'mlCIII 2 NotAppbed

MSM.I( form QAF-151

Rev Ori&J~I 20 Jin 09

J Not Coneemcd ·-- !I Apphed tn Shop 6 f'mal status

Page: 6

7 AO 1w hem. apphcd

STAM® DATE MAR 19,2013

• • • • • • • • • • • • • • • • • • • • • • • • •

Bquipment1

AD

MSMX Fo..., QAf-lSI

A~ or111n,1 20 Jan 09


EfJecth,lty date

~SAFRAN ~ Messier-Bugatti-Dowty

S/N1 DCL3801/99 Pages 7

Airworthiness Directives

NOT APPLICABLE

STAMP® DATE MAR 19, 2013

• • • • • • • • • 1• • • • • • • • • • • • • • • •

Equipment:

MSMX Form QAF 15,11

Rn-Onc,n•I 20 ).on 09



S/N: DCt.3801/99 Attachment 1

CONCESSIONS

~TAMP® DATE MARJ9,2013

11111 • • • • • • a • a • 11 11. I. a, a • II II II a II • • •

BOMBARDIER REPAIR DRAWING (RD)

1 TITLE 2 RD NUMBER

REWORK TO MLG DRAG STRUT, PIN 1'0204-''' 8-32-3332 --

J 3 SECTION 4 SHEET

I I

5 PRIME DESIGN ACTIVITY 6 ADDITIONAL LIMITATIONS 7 SERIES 8 APPLICABILITY 11

BOMBARDIER INC., MLG Drag Strut DOWNSVIEW 71867 NONE DHC-8 PIN 10204-553

S/NDCL3839 9 DESCRIPTION

This document approves a repair for damage to the MLG Drag Strut, PIN 10204-553 as described in Messier Dowty Concession Letter RO 13/036 Rev. Nil.

Rework the MLG Drag Strut as per the instructions of Messier Dowty Concession Letter RO 13/036 Rev. Nil, dated January 22, 2013.

Ensure that all damage is removed after rework.

This approval is covered by RD 8-32-3332, Section 1: Sheet 1, Issue 1

...

10 ISSUE I I I - - -

11 DATE Jan. 25, '13 ' - --

12 PREPARED BY P B01s-Gross1a.nt

7A 7 ~ --

13 STRESS

17 /fl,/ --16 DESIGN AUTHORITY

14 , ~i'[,f -

15 11J..I. -

17 DAO AUTHORITY ?l!~';JJJ "- 2C"'1'1

THE TECHNICAL CONTENT OF THIS DOCUMENT JS APPROVED UNDER THf-

' "S!JQSITION "-OH APPqQVJ\ H" )P!_R/11 UR ,2" 18 Ix] DESIGN AUTHORITY OF TRANSPORT CANADA DESIGN APPROVAL

',[<.,<; Al ''lORf"Y ORGANIZATION DAO NO 93-0-02

-- --THE INfORMATIC/', ( NI( ,

Tl-11S REPAIR OAAWING HAS BEEN PREPARED ON THE BASIS OF INFORMATION SUPPLIED TO , , ,-.;, ,W,l l\l'iLU t1Ef<f:,N ARL THf f ,{ I US'\! ''<Ul-'E-.RI

BOMBARDIER INC 8Y THE OPERATOR OR HIS AGENT IT IS Tt£ RESPONSIBILITY OF THE OF BOMBARDIEfl IN( OH C~\ 1 , • I;' H, I r,7.v HIGHTS OF OTHLRS ANO Af.!L N01 !0 RE USlcl , f< '

OPeRATOR OR HIS AGENT TO VERIFY THAT TIE INFOFV,MTION SUPPUED IS cc:w.FLETE ANO OtSCLOSEO TO OTHU~S Wlll'(J ~ 11 l •!1 -rFN CONSENT OF BOMSAADIER INC THE RECIPIENT 0~ Tr>,<;

ACCUtATE 90M8ARD1ER INC. DOES NOT ACCEPT RESPONSIBILITY FOR AM' DOCUMENT BY 11S Ht 1ENTl8N AM; ~S' AGRELS TO I-IOU) IN CONFIDENCE THE TECHNICAL DATA ANO

CONSEOlENCE RESULTING FROM IHCOMPLETE OR INACCURATE REPORTING Of THE DESIGNS CONTAINED HLREIN THF I Of.!El,OING SHALL NOT APPLY TO PERSONS HAVING PROf'RIETARY RIGHTS TO SUCH INFORMATION TEC'HNICAL OATA OR SUCH DESIGNS TO THE EXTENT THAT SUCH DAMA.GE / DISCREPANCY RIGHTS EXIST 0 3303-27 REV 1999-07

BT0214·11 MW REV 2006-08 © Bombardier Inc.

._ • • • • • • • • II • I:: L L I. 11 II 11 • a. 11 11 11 11 •

Mns1•r~Dowty J11c. Tel +I 905 683 3100 ~~ Messier-Dowty 57" Monarclt Al'tttue, Ajax Fax. +1 905 683 69311

Ontario LIS 2GB, Ca11ada

I Messier~Dowty Concession Number I RO13/036 (To be marked 011 llle part)

From rENDER

I Cust, Ref No MX5877

Tel. No. ~ +(52) 442 192 58 00 Fax.No. +(52) 442 1 92 58 01

P.O. Number Job I Order No. 71177613

AICType I AICMSN I Operator AIC-TSN AJC-CSN rr:me Sillce New) 1C·""'ln Since Nrwl

DASH8 COMMUTAIR 2417336 26567

I CMM I 32-10-08 I I Rev I 5 I j Page No j I I Figure I I ~

Part No 10204-553 Assy No '')200 553 --Issue Juue

Serial No DCL3839 Serial No JC:..3801:99 --Description DRAG STRUT Assy-CSN 26567

I Part-T.S.N I I Part-C.S.N

I I Part-T.S.O I

I Part-C.S.O I 24173 36 26567 NIL I NIL

Pnv1011s Conct.mon(s) alnady ,:ranted on lltm refured to lun,n NONE

Rttuon for the Applu:at1on w1thfull dttailJ of dwerge11ce from Component Ma,nttMJtce Manual

Where upproprialc, a1tach dimcns1onrd sketch(es)

MX5877 DRAG STRUT PIN 1 0204-553 SIN DCL3839 COMMUTAI R

SPOTFACES MACHINED TO REMOVE CORROSION BOTH SIDES, SPOTFACFS Anc 2 l('<l ',( "'l':" orPTH LH AND 2 gga~ X 0 094" DEPTH RH, THE BORE IS 2.2300" BOTH SIDES

Name: ADRIANA BRAVO Signature : .................................

Tille : PRODUCT ENGINEER Date: • 0 0 0 I O O O O O O O O O O O O O O O O O I I I I O O O O O O O O O I O O O O O I e O O O O O o o o o • o O O I O , ,-, o o o o o I I I O O O I O O I I O O O O O O I <

To Be Completed By O.E.M. (Orlgmal Equipment Mmm(acturr, J

IS LIFE ADVERSELY A.FFECTED7 -.:.;. Lal7P.' "" """ IS STRENGTH ADVERSELY AFFECTED? N• IS FUNCTION ADVERSELY AFFECTED? I\.)• ' ~t:<..~,,~: .J IS INTERCHANOEABIUTY AFFECTED? N, ----ANTBRIORITE I ANTERIORTY IJl\Ji(') J <'""- .2/ ,2,-; f f

REPAIR CUSSIFICATION I IV\ 11'J<>C I Signature Dal,

IMmler-Dowty - O.ci110n

9,~ ~ I Cwtomtr Dtdgn Strtt11t1 Quality

I MD - Approval

I Strvica

Name § ~ A \::~o• ~.v- § d S1g11ature 7" c· <cs

J1y/ c 1 /z.:•1,;. I

Dal, <l<tn 2-\ / I~ '~ I ~

PS002 Rev D

••••••••••• II II • a a • 11 11 11 II • • •

Messier Services Americas S.A. de C.V.

Av La Nona No 131, Parque Industrial Ouer8taro Santa Rosa J8uregu1, 76220 Quer8taro, ORO Mexico

OGAC Repair StaHon No 346

NON CONFORMING MATERIAL REPORT

REPORTE DE MATERIAL NO CONFORME FAA Repair Sta\1or No ~..AXVY496Y EASA Re u1r St;i· o No_,_45~0 .. 3 .. 5 .. 6 _________ __,

Work Order· Orden de TrabaJo

NMRNo No de RMNC·

Sertal NUTJber No de Serie

CMM. 32-10-08

Item No ArtlculoNo,

R8H DEPIH Ill D

Llll llAIElBI 1111 I

SPOIFACE IMA!fl!R 11111.H

BORE llA (""' IMt(J Oil G

QW,f!RIIIH

SPO!FACE DEPIHOilllltl.H

OJ!OOT(lox)Oill

OOIOOT l'fl!H 0111 L

ConerRdo DIIM

lnapedor Stamp I Date·

711776.1.3

NMR-000!5·2013

DCL3839

Rev 5

Customer Chente COMMUTI\IR

Aircraft Registration I MSN Matrlcula de la Aeronave / MSN

Desctlptlon De,c,lpcl6n· DRAG STRUT

Previous Concession applied to this Part Ves Concesl6n Previa aplcada a esta Parte· •

No f.]

1"ogrc1r, , ogr 1 ''d DASH 8

Purl Number

No de Parle 10204-553

TSN. 24173.36 CSN:26567

Previous ConoesSIOn No· No Conce816n Pravla: NONE

Oellcrlptlon of Nonc:onformhy (lnch.Jde any sketches as neccesary)

Descrlpcl6n de la No Contomudad (Incl/ya pianos ad1clonalea como sea necesarlo)

SPOTFACES MACHINED TO REMOVE CORROSION BOTH SIDES, SPOTFACES ARE 2 999" X 0,093" DEPTH LH AND 2.918• X

O.OIM" DEPTH RH, THE BORE IS 2.2300"' BOTH SIDES

1Zll" 1.211·

1 000" 1.000"

ll24"11'

0.170"' o.rnr

5114" 5,114"

2.998" 20811"

O.<Kl4"

NIA

II/A .. '"' NIA

NIA HM

II/A

l!R

TrxD!n EnVLuc

MoJRldJ

Ro"1

Sj,ol

%(0., CNml

~hCu·

Dmlx -1>./

,,

,,, .... 7 '" ,1re --~

'

I

1 -r,>----J

,____J_t

Inspector Selo / Fecha: 15/JAN/13

MSMX Form: l.8200-15 NMR·0005-2013

Rev 06 · 27 Jan 11 Paga 1 ol 1

•

..

..

lJ ll Ii II II II ll R: It L L L L L L L I. L L L la II Ii II W

ATTACHMENT FOR RO 131036 Page I of5

Description : Drag Strut, MLG Part Number · 10204-553 Serial No : DCL-3839 Cycles : TSN - 24173; CSN - 26567; Operator : Commuta1r

DEFECT DESCRIPTION: 1. Apex Pin attachment lug faces were spotfaced to remove corrosion. Spotfaces are

02.999" by .093" LH and 02.998" by 094" RH. The bore is reported as 02.2300" (to drawing requirements).

See attached dimensional chart

COMMENTS/INSTRUCTIONS: Part is acceptable after the following rework is completed·

Item 1:

1. Ensure that chamfer 0.140"/0.160" x 45° is machined on both sides per CMM 32-10-08.

•

2. Ensure that a R.050 radius is machined at the intersection of the chamfers and the bore or alternatively machine a .040" x 22.5° chamfer at this location per CMM 32-10-08.

3 Ensure spotface has a minimum flat area of 02.900" mm for both sides of Apex lug.

4. Ensure a spotface corner radius of 030" minimum and th;it 1he reworked spotfaces are perpendicular to the bore within 002"

5. Break all sharp edges 010" I .015" .. 6. Ensure reworked area is smooth, continuous and free from dents, chips, scratches, pits

and tool marks. Ensure 63Ra micro-inch surface finish or smoother on main bore and a 125Ra micro-inch surface finish or smoother on all other reworked areas.

7. Locally liquid penetrant inspect reworked area per CMM 32-10-08.

8. Locally shoVrotary peen reworked areas per CMM 32-10-08 Mask as required prior to shoVrotary peening reworked area.

9. Locally chemical conversion coat reworked areas per CMM 32-10-08

10 Fabricate qty (2) repair sleeves as shown on the follm._,,,.,1 ,,,1<,es

11. Fabricate qty (2) repair bushings as shown on the fol Iv:."" . ,ges

12. Install bushings into sleeves per CMM 32-10-08 requirements

13. Install sleeve/bushing subassemblies into reworked lug per CMM 32-10-08 requirements.

14. After installation ensure a 3.384"/3.390" dimension across bushing flanges and 01.8560"/1.8570" per Figure 604 of CMM 32-10-08, with a symmetry to the centerline within .002". Locally brush cadmium plate reworked faces of bushings per CMM 32-10-08. Ensure lubrication passageways allow full greasing of joints (if applicable).

ENG t'.Z tJ {t.lC,d4t Date Lb / , I f ~ STRESS c ~ z Date JC ' --- ~[ ·:;; ..

M&P Date :;;;,....._ 7../ /2-fPf} I

••••••••••••••••••••••••• ATTACHMENT FOR RO 13/036 Page 2ofi

Identification and Completion:

1. Identify drag strut (10204-553) with "RO 13/036" close to ex1st1ng part mark per CMM

32-10-08 (vibro-peening). Locally Chemical Convers1n•· r::ic1t reworked 1dent1f1cat1on per

CMM 32-10-08 requirements.

2. Complete part and final assembly per CMM 32-10-08 requirements

..

..

I.J I.. L L 11. L L L L L L L L L L L L L L L L I.I a. t. U

ATTACHMENT FOR RO 13/036

DIMENSION "C RADIUS"D"

CHAMFER "J" .-----;~l;.!,-_______ r;: DIAMETER "F"

DIAMETER "A"

- DIAMETFR "H"

+ CHAMFER "G" CHAMFER "E"

DIMENSION "B"

FEATURE SIZE

DIMENSION "A" 0 1.980" / 1.981"

GEOMETRI C REQUIREMENTS

METER "F" TO WITHIN 002" CONCENTRIC TO DIA

DIMENSION "B" 1 375 / 1 385"

DIMENSION "C" 0 140" IO 160" X 45'

RADIUS"D" R O 020" / 0 040"

CHAMFER"E" 0.040" I 0.060" X 45'

DIAMETER "F" 0 2.2337/2.2342

CHAMFER "G" 0.020" I 0.030" X 15'

DIAMETER "H' 0 2 430/2 450"

CHAMFER "J" 0 020" I 0.030" X 45' --- -----

NOTES FOR APEX PIN LUG REPAIR SLEEVE

1. ALL DIMENSIONS ARE INCHES.

2 ALL ANGLE TOLERANCES ARE+/. 2 DEGREES

3 BREAK SHARP EDGES .005"/.015".

-~~

4. MA T'L : 17-4PH STAINLESS STEEL PER AMS5643, CONDITION A. PRECIPITATION HARDEN PER AMS2759/3 TO CONDITION H1025

5. LIQUID PENETRANT INSPECT PER CMM32-10-08.

6. HARDNESS TEST IN DESIGNATED AREA 34-42 Re

7. GLASS BEAD BLAST OR VAPOUR BLAST PER MIL-STD-1504, OR PASSIV ATE ALL OVER PER AMS-2700.

8. CADMIUM PLATE ALL OVER PER QQ-P-416, CLASS 2, TYPF ll

9. ALL DIMENSIONS TO BE MET AFTER PLATING

JO SURFACE FINISH TO BE63Ra MICRO-INCH OR SMOOl'Hlc.R l'l<llJ,< , cJ I' \ .1,l,

..

IJ ~ L I.. L L L L L L L L L L L L L L L L L LI ._. lJ U


DIMENSION "B" DIM. "A" -------===c=-='-'--'---=-----..

DIA "G"

CHAMFER "D"

RAD. "C" 7 DIA"H" CHAMFER "E"

CHAMFER "J"

/\ /

DIA "F"

Page 4 of5

_M SPIRAL GROOVE, 0.5 PITCH

FEATURE SIZE GEOMETRIC REQUIREMENTS

DIMENSION "A" 150"/ 155" BOTH SURFACES TO BE SQUARE TO DIAMETER "F" TO WITHIN 001"

DIMENSION "B" 1.375" / 1.385" RADIUS"C" R .020" / 040"

CHAMFER "D" .020"/.030" X 15° CHAMFER"E" .010"/.020" X 45° DIAMETER "F" 01 9830" / 1 9835" DIAMETER "G" 02 855" / 2.875"

DIAMETER "H" 01 8542" / 1 8552" 1 TO BE CONCI NI I,, , ,,M[TlR T' TO WITHIN/ 801

CHAMFER "J" 050" I 060" x 45° --------- -·"

NOTES FOR APEX PIN LUG REPAIR BUSHING

ffi DIMENSIONS TO BE MET AFTER BUSHING INSTALLATION INTO SLEEVE

2. ALL ANGLE TOLERANCES ARE +/- 2 DEGREES.

3. BREAK SHARP EDGES .005"/.0IS".

4. MAT'L: 17-4PH STAINLESS STEEL PER AMS5643, CONDITION A. PRECIPITATION HARDEN PER AMS2759/3 TO CONDITION HI 025

5. LIQUID PENETRANT INSPECT PER CMM32-10-08

6. HARDNESS TEST IN DESIGNATED AREA 34-42 Re

7. GLASSBEADBLASTORVAPOURBLASTPER MIL-STD-1504. 01( 1',\SSI\ \ 11 AI.I.OVf KI'! R AM,-27IJU

8 CADMIUM PLATE ALL OVER PER QQ-P-4I6, CLASS 2, TYPE II

9. ALL DIMENSIONS TO BE MET AFTER PLATING.

J.!l· SURFACE FINISH TO BE 63Ra MICRO-INCH OR SMOOTHER PRIOR TO PLATING.

&sPIRAL GROOVES ARE TO BE MACHINED IN THE BUSHINGS IF THE LUBE FITTING INSTALLATION .. PROCEDURE SHOWN IN CMM32-I0-08 REPAIR #1 HAS BEEN PERFORMED OR THE LUBE FITTING IS PRESENT lN THE DRAG STRUT. IF THE LUBE FITTING IS NOT INSTALLED IN THE DRAG STRUT DO NOT

••••••••••••••••••••••••• ATTACHMENT FOR RO 13/036

MACHINE SPIRAL GROOVES. NOTE: IT IS RECOMMENDLD, BL I ,, , \,,\ ,,JA I ORY, I HA r I HI, l.l,llf FITnNG BE INSTALLED PER CMM32-I0-08 REPAIR #1 AND THE UROOVI.D BUSHINGS BE USED.

... II Ii 81 II II II 111! L Ii LL a, a. II II II IIWll 111111 MM

BOMBARDIER f~EPAIR DRAWING (RDJ

1 TITLE 2 RD NUMBER

REWORK TO SHOCK STRUT TO DRAG STRUT PIN, PIN I 0216-551 8-32-3335

3 SECTION 4 SHEET

1 1 5 PRIME DESIGN ACTIVITY 6 ADDITIONAL LIMITATIONS 7 SERIES 8 APPLICABILITY

BOMBARDIER INC., Shock strut to drag strut DOWNSVIEW 71867 NONE DHC-N

pin P/N 10216-551 s;" ncr 1N6<J

9 DESCRIPTION i.

This document approves a repair for damage to the Shock strut to drag strut pin, P/N 10216-551 as described in Messier Dowty Concession Letter RO 13/047 Rev. Nil.

Rework the Shock strut to drag strut pin as per the instructions of Messier Dowty Concession Letter RO 13/047 Rev. Nil, dated January 23, 2013.

Ensure that all damage is removed after rework.

This approval is covered by RD 8-32-3335, Section 1: Sheet 1, Issue 1

(

•

10 ISSUE 1 - - - -- - --

11 DATE Jan. 28, '13 - -

12 PREPARED BY P Bo1s-Gross1ant

13 STRESS //-"'1/ , -

16 DESIGN AUTHORITY v7 _/ ' 14 ' ,',/,A :

15 11A4

---

17 DAO AUTHORITY '4?:~:1 C. ?~ ., '1

THE TECHNICAL CONTENT OF THIS DOCUMENT IS APPROVED UNDER THt-, I YO~ITION I OR A.PPROV<'\, 1'

I 18 Ii] DESIGN AUTHORITY Of TRANSPORT CANADA DESIGN APPROVAL [J

1,1 I!,: Jr1',

ORGANIZATION DAO NO 93-0-02 '.J,,\ ' ' r-i 'llN[SS AUTHORITY

THIS R2PAIR DRAWING HAS BEEN PREPARED ON Tl£ BASIS OF INFORMATION SUPl'UED TO T11E INFORMATION TECHNICAL DAT t, A Nil 11E;,1GNS DISCLOSED HEREIN ARE THE EXCLUSIVE PROPERTY 80M8AROIER INC. BY THI! OPERATOR OR HIS AGENT IT rs THE RESPONSIBILITY OF THE 01' BOMBARDIER INC OR CON f AIN PROf'RlrT ARY RIGHTS OF OTl11!!!RS ANO ARE NOT TO BE USl:O OR OPERATOR OR HIS AC3ENI' TO VERIFY THAT Tl1E INl"ORMATION SUPPLIED IS COMPLETE AND OISCI..OSEO TO OTHERS WITHOUT THE WRITTEN COliSENT OF BOMBARO!ER INC Tl£ RECIPIENT OF THIS ""'-"A,._ BOt.eAROIER INC. DOES NOT ACCEPT RESPONSISIUTY FOR ANY OOCUM:NT, BY ITS RETEffflON ANO USE AGREES TO HOlD IN COlflCENCe Tl-I! TECHNICAL DATA N«> CONSEQUENCE RESULTNG FROM INCOWLETE OR INACCURATc R!FORTlNG CF TIE DESIGNS CONT~EO 11ERE!N THE FOREGOING SHALL HOT APPLY TO PERSONS HAVNG PROPRIETARY OAMAGE I DISCREPANCY RIGHTS TO SUCH INFORMATION, TECHNICAL DATA OR SUCH DESIGNS TO THE EXTENT TW.T SUCH

RIGHTS EXIST D.3383-27 REV 11111M7

BT0214-11 MW REV 2006-08

1-r· © Bombardier Inc. '9 r-

ll • ll • • • II ll ll • II l;a l. l. II II II II • II II Ii It .. _.

Meniu-,.Dowt, /11c. Tel: +I 905 683 3100 K.~ Messier-Dowty 51' Mo1111rch APen11d, Ajax Fax: +I 905 683 6936 O11Utrlo US 208, Canada ~' \.l\~ANC,1""'1"

f Mes,ier-Dowty Co11ceasion Number I RO13/047 (To b, ma,k,4 on 1h, part) I RC-TO-0063831

From !"ENDER I C11st Ref No. MX5889

T•L No. ~+(62) 442 192 58 00 Fax.No. +(52) 442 1 92 58 01

P.O.NamW Job I Order No. 711776.1 5

~ I AICMSN 11 Operator I AJC-TSN A/C-CSN

rnme Since New\ rc .. des Si11ct New 1

COMMUTAIR l "' 7':. '1~ ?6567 8 -

I CMM I 32-10-08 I I Rev I 5 I j Page No I I I 11:ure I I Purl No 10216-551 A.ssyNo - 10?00-553

l1tu1 lnue

Serial No DCl3669 $,rial No DCL3801/99

Ducrlptio11 SHOCK STRUT PIN Au1-CSN 26567

I Pm - r:f,w · I I Part-C.S.N. I I Pa,t - T,S.<J I I Part-c.s.o I 24173:36 28567 NIL I NIL

PrevUJ11s Conuuion(s) already tramed on lton rde"'" to hereln: NONE

Rea30l1/01· the A.ppUcatlo,1 with fall d,taiU of dlw:rgencefrom Compone11t Malnteno.nce Man11.al

Whefe 1ppropriatc, 111ach dhnenalonal skctch(cs)

MX5889 SHOCK STRUT PIN PIN 10216-551 SIN DCL3669 COMMUTAIR

OD WAS MACHINED IN ORDER TO REMOVE CORROSION TO 1 8405"

Name: ADRIANA BRAVO Signature• ................................

Tille: PRODUCT ENGINEER Date • 0 • • 0 0 0 I I O I O I I I O O O I O I I I O I I I I I I O O O I O I O O O I I t O f O O O O O O o I I , , o • ' • • ' ~- .. ' ................. '

To Be Complel#d By O.B.M, (Orifrnnl Bqulp,ne11t Ma11u1«, 111•,,

rs LIFE ADVERSELY AFFECTED? f\. h Lnboro/u1y fJn1111J11

-

' IS STRE:NGTII A.DVBRSBLY A.PPBCTBD? .. \. IS FUNCTION ADVERSELY AFFECTED' ,-~

~-- --

.;p".--.<J"J~l IS INTBRCHl&NGBA.BIUTY AFFECTED'! ~~

ANTBR/ORITB I ANTBRIORTY '-1,L-->

REPAIR CUSSIPICA.TION I WI ' N<-(11.., I Signt1tur, Dale

r•nl"·Dowly -D,clllo,i s~ ~ I c...,..,, ,,..,,. s .... , Quality MIJ - Approval S,nka A

§ w ~ § ~----

Nam, ,, 1)

Signature I I

/r-

Dale L_- --- J~,11 ?1 2<J> > I I

PS002 Rev D

. . . . . . . . . . . . .. .. . . . . . . . . . . . Messler Services Americas S.A. de C.V.

I Av. La Noria No 131, Parque Industrial OJeretaro Santa Rosa Jauregw, 76220 Queretaro, ORO M6x1co

DGAC Rep,m St;it,"n Nr 'l46

NON CONFORMING MATERIAL REPORT FAA Rcp<W s•_, C ' ''Y ,v1195y

REPORTE DE MATERIAL NO CONFORME EASA ~CCd ;'<r.r

Work Omer Of'dan de Trabajo,

NMRNo. No, de AMNC:

Serial Number No de Sena

CMM 32-10-0S

11am No ArllctAoNo

,

[Thick.• 0.2415" after mach

Inspector Starr., I Dale. Inspector Selo / Fecha:

MSMXForm LS200-15 Rev 06-27Jan11

---CuSlomer µ,091dn

711778.1.5 criente COMMUTAIR Prograrna DASH B

Aircraft Reglstrallon / MSN Part Number

NMR--00&8-2013 Matrlcula de la Aeronave / MSN' No. de Parte 10216-551

Description· TSN: 24173:36

DCl.38fl Oescnpat,n: SHOCK STRUT PIN CSN 26567

Previous Conceulon applied to this Part y., No. Previous Concession No: Rev • Concesl6n Prevla aplcacla a esta Parte D No. Conceal6n Prevla. NONE

Oescrlpcton ol Nonconformity (lne.Jde any sketches as neccesary)

Desc,lpcl6n de la No Contormldad (lncklya pianos adlclonalcs como sea necesarlo)

OD WAS MACHINED IN ORDER TO REMOVE CORROSION TO 1 8405"

----

I & .,,, ','/<,~,'////j////._,-_ / k%(~!.~.w,:;_ ,_ l I /'c.

I

I !

I /OD. 1 8405" 'After rnachin1'1q

-:Z"";-r,,77,;; :·',',/;,,, /?'· :l_L • -- ---· - -

JAFB ... 17.JAN-2013

I _,

'

NMR-0058-2013

Page 1 of 1

..

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1111 • • • • • • II II II II • L l. • II Ii II II Ill • II 1111 • •


Part Number: 10216-551 Serial No. : DCL3869 Description : Pin, Shock Strut-Drag Strut, MLG Cycles : TSN - 24173; CSN - 26567; Operator : Commutair

DEFECT DESCRIPTION: The 01.846"/1.848" pre plating outside diameter was machined to 01.8405" to remove corrosion.

COMMENTS/INSTRUCTIONS: Part is acceptable after the following rework is completed.

..

Note: After this repair is completed, all future repairs must be approved by Messier-Dowty Inc. prior to part being used for service.

1. The 01.8405" dimension is acceptable. Ensure the Ti cad plate or IVD has been stripped per CMM32-10-08 requirements

2. Break all sharp edges .010"-.015" Ensure reworked c1rea Is smooth, continuous and free from dents, chips, scratches. pits and tool 11·,,·. ccsure a 32Ra m1cro-1nch surface finish or smoother on all reworked area, ..

3. Nital etch per AMS 2649 type 2.

4. MPI per CMM 32-10-08. Acceptance criteria per CMM 32-10-08.

5. Shot peen per CMM 32-10-08. Mask all surfaces not reworked by this concession. Do not mask cross bolt holes.

6. Re-chrome per CMM 32-10-08. 7. Identify pin with "RO 13/047" close to existing part mark per CMM32-10-08 pg. 602

(vibro-peen). 8. Mask as required and cadmium plate the remaining surfaces per CMM32-10-08

9. Complete part per CMM32-10-08

ENG ,J -(Ll vi, li*" l Date (~·l1[/ 7

')

STRESS ~- Date J(t '' /?ni3

M&P ft,,c-=::: Date J;,, a) I j,O(j

• • • • • • • • • • .. • • • • • • • • • • • • • •


Equipment: DRAG STRUT ASSY, MLG S/N: DCL3801/99 Attachment 2

PREVIOUS OPERATOR STATEMENTS(NON INCIDENT, LLP PARTS CHANGED IN SERVICE,CSN/TSN)

MSMX Form QAF 151

Rt• Ong,n1I 20 Jan 09 STAMP® DATE MA.1<19 2011

....................... ~~

NON INCIDENT ST ATEl\tlEJ\T

Please be advised that the best of our acknowledge; equipment mentioned below was not obtained from U.S Government or Military Source and have not been subject to severe stress or heat such a major engine failure, accident, fire(aircraft or storage) or submerged in salt water. Therefore this unit understood to be Non-Incident related.

We also confirm no life limited part was removed or changed while the equipment was in

Commutair Operation

~ - -- ~

Description: DRAG STRUT ASSY, MLG

Part Number: 10200-553

Serial Number: DCL3801/99

RO/PO: 9-77036 -

I TSN I I 24173 6

26567

Times operated with Commutair 24173 6

Cycles operated with Commuta1r 26567 --- - .

Removed from MSN N839CA -- - ..

Aircfract Type DHC-8 0300 --- ,--

Installation date 03/16/2000

---1 Removal date· 11/24/2012

SIGNED BY: TITLE, NAME & SIGNATURE

Michael DaS,lva. ~ate~als Ma~~ge/ommutair

l '

..

..

' •••• •••••••••••••••••••• --- - - - -- ---

' - - -... .. I . '

1 Oras Strut Assy, MLG 10200-553

2 Drag Strut S/ A 10205-553

3 Pin, Shock Strut 10216-551

4 Pin, Retraction Actuator 10212-551

-- ---,---~~~

-

<' - --- - ~-- ~

DCL3801/99 26567 24173.6

DCL3839 26567 24173.6

DCL 3869 2G567 24173 6

DCL 3590 ' ',0. 2J:73t, I l ..

:I

• • • • ill

• 1• • •• 1.

'

·., al

• • • ii

• .. • • ..

SsAFRAN Mess1er-Bugatt1-0owty

Equipment: DRAG STRUT ASSY, MLG S/N: DCL3801/99 Attachment

MSMX f<irm QAF-158

Rev On21nal 20 Jan 09

O.E.M CERTS FOR NEW LLP/LRU ITEMS

NOT APPLICABLE

3

DATE M.\R 19, 20!3

Appromg A~1at1on 2. Form T rackmg No Authonty FAA/UNITED ... … · cmm 32-10-08 rev, 05 datbd nov...

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Transcript of Appromg A~1at1on 2. Form T rackmg No Authonty FAA/UNITED ... … · cmm 32-10-08 rev, 05 datbd nov...