Airframe Log #I Open: 12/9/2005 · FAR 91 .207d. Inspected and serviced landing gear, tires,...

Airframe Log # I

Open: 12/9/2005

AIRFRAME MAINTENANCE

RECORDS

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AIRFRAME MAINTENANCE RECORDS

Aircraft Information

"'~'·" ~· R•att•tion Humbtt: N'l45US

MOdel :

SIN

Date or Monr:

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1~- .. I ·t:~~--~!-Y ' NU!.US TACH: 491.1 1V1S/Oe I

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TACH OR RECORDING

METER TIME

DESCRIPTION OF WORK PERFORMEDSIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK

TOTAL brought forward from previous page -

-C A NJ.tS lJS TACII 7H7.5 4/14/1011

Accoanplishcd pre-purchase mspcct ion pea O\\ nca • s 1 equcst Accotnpll . hcd contprcssion check 70/HO (> 1/RO o 7/HO (, 1/RO ()9/RO <)5 RO Rcnto\ ~d otl filter and cut open to inspect 1nedia. no abnonllalittcs noted. RentO\ ed spark plugs and tested gapped and cleaned. Accoanplishcd 13orcscopcd inspection of all 6 cylinders. no da tllagc noted. Glenn t\ 1acDcnnod J053~27AP

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-CA CITY AVI ATlON N 345US TACH 833.7 9/7/2011

Accomplished Vacuum and complete service of aircraft air conditioning system IA W Mooney supplement. Measured temps at the TXVs and found that they were 5 deg off from each other. Perfo1 rned steps in Mooney M20R MM Ch 2 1. Ops checks oood at this ti1ne. o

Thomas Shane Dyar ~J 1

_ 3523005AP ""1./v ~~~~,~ ~~

SUB-'

-£~ N345US TACH: 843.3 TTAF: 843.3 11n12011

Accomplished Annual inspection lAW Mooney service instructions and 1 OOhr check list Opened all access panels. Cleaned, inspected, and lubricated all push pull tubes and rod ends. Replaced LH wing tip strobe pn 02-0250276-00. Stop drilled crack in LH nav light lens cover. EL T batteries dated 03/2015. Functionally checked EL T lAW FAR 91 .207d. Inspected and serviced landing gear, tires, wheels, and brakes. Replaced NLG bearings and races pn 08125-20629 and 08231-20629. Relined brakes with 066-10500. Accomplished gear swing, both normal and emergency, no faults noted. Checked all ADs through ATP as of 1/1/11.1 certify this airframe has been inspected lAW an Annual inspection and was found to be in airworthy condition at this time.

EL T exp date 03/2015, PitotlStatic Due 04130/2012, Annual due 11/30/2012

Glenn MacDermod 30534271A

N345US "'VI AT I 0 N , 1 H 0 ,

Hobbs:878.2 4/13/2012

CIW AD 2012-05-09 and Service Bulletin No. M20-313A for the tail trimno defects noted.

Thomas S. Dyar 3523005AP

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:\irfra ml' l .ug f/ 1

O pt•n: 121'>/2()115

No.

DESCRIPTION OF WORK PERFORMED-TACH OR TOTAL

CERTIFICATE NO. OF PERSON PERFORMING WORK RECORDING TIME

SIGNATURE & >ATE IN METER

I SERVICE TIME

d Carthage NC 28327 Sandhills Avionics ~~3~0~~rle :~: 1023/1 sAL BPS

CRS #J31<RS47X

LOG ID# 355 20-Apn - MOONEY M20R 5US S/N 29-0403 N34 Pg 1/1

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N345US TACH:888.3 7/2/12

Replaced inoperative A/C condenser fan relay with serviceable unit p/n 26.72.03. A/C system ops checked good.

Thomas S Dyar 3523005AP

A N34SUS TACH: 895.3 7/27/2012

Replaced# 1 battery with Concorde RG24-15; SN 40511213

Thomas S Dyar ,., .. 3523005AP

' 000 f ee t .

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" ,.. AYI.lno" N345US Hobbs: 902.4 8/29/2012

Found all three tires were beyond !he service limits. Replaced nose gear tube wilh pin 302-013-400 and tire with pin 072-3 1 2-0. Reassembled !he wheel and tire and reinstalled on !he acft wilh a new cotter pin. Installed two new tubes p/n Gl.r6020 and two new tires pin 072-314-0. Reassembled wheels and tires and reinstalled assemblies on the act\ with new cotter pins. ReinstaJied both brake calipers and both outboard speed fairings. Thomas S Dyar ").k;,- ~ ~ vt---- ' 3523005AP

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Twin Lakes Avionics . --- ----· Ollie: I 0-15-1:? Model: Mooney S/N: '4 7R0509J N# 345US W/0# 8483Tach: 9 I 3.0

Removed Garmin GDC. PN:O 11-008882-00 SN:47805093; Performed field calibration lA \\' service adorrsory 0"120 Revo A and reinstalled

. Th c a i rc raft, a i rl~mnc, ll pp li an ce . i d ~Ill i fi ed '' bO\ c was repaired 11 n d ins pee red' i 0

a ceo rdance with ~" rrent J,umcnancc 1 u le~ olthc Federal A vmt10n Regulat IIlli s and ~ ~ appro\ ed for r~turn

10 service. Peninem details of

!he: rc.!pCJ ir at\· on fi lc a1 th i' repair sLm ion - f:"'i!) _La!es A\'ion~s._q~~ ,JU4_1!_2?_§1M __ iu~J!'~c'!d '£':!?.""";?'~ ~

SUB-TOTAL this page

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DATE

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Page No. TOTAL TACH OR TIME RECORDING DESCRIPTION OF WORK PERFORMED-IN METER

SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK SERVICE TIME

TOTAL brought forward from previous page

N345US SN 29-0403 TACH: 926.9 TTAF: 926.9 12114/2012

Accomplished A~nual inspection lAW FAR 43 (d). Opened all access panels Cleaned, inspected. and lubricated all push pull tubes and rod ends. EL T batte~1es dated 0312015. Functionally checked ELT lAW FAR 91 .207d. Replaced inducbon filter elsnent vi new Donaldson pin ED04028 & saft1~d clasps: Due replacement 3 years or 500 hr. Jacked NC, Inspected and serviced landing gear, tires, wheels. and brakes Torqued & resart1~ bolts m yoke atop strut & linkage attached to yoke. Removed and serviced speed brakes wrth lubnplate AccompliShed 6 fa~lt free gear SWing, both nonnal and emergency. Replaced both 0-rings MS28513-338 and ~10 on LH & RH fuel caps & adJusted tension. Ren:'oved AVOX bottle & regulator assy. p/n 895-08015, service port & fill line assy. Along with bottle mount brackets Equ1pment removed we1ghs 20.21bs, Re-computed weight and balance for 02 equipment removed. Checked all ADs through ATP as of 12/12n012 AD 2012~5-06C was PCW lAW M20-313. I certify this airframe has been inspected lAW an Annual inspection and was found to be m a1rworthy condition at this time.

EL T exp date 03/2015,

Abner Tisdale 35621551A

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Pi tot/Static Due 04130/201¥: Annual due 12131/2013

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Twin Lakes Avionics -

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_j Date: 3-19-13 Model: M20R S/N: 29·07403 N# N345US \V/0 # 8673 Tach: 950.0 Hobs: 948.1

Re loaded GTX software and GTX configuration 'iettings I.A. Vi. Garmin Manual PN: 190·00907-00. Ground check satisfactOI)

The a ircraft, airframe, engine, or appliance identified above was repaired and inspected in accordanc~ '" ith current ntaintenance rules of the Federal Aviation Regulations a.!l! is approved for ret · to !:len ' ice.

Paul R. Greer Jr. A&P: 3254795 Ins ected · ??..d ~ ~e..~ • • •

N345U~SN: 29-0403 TT AF: 1005.0 01/10/2014

Accomplished a 100hr inspection in accordance with Mooney service instructions and FAR 43(d). Opened all access panels, cleaned, inspected, and lubricated all push/pull tubes and rod ends. Functionally checked ELT lAW (FAR 91.207d): ELT batteries dated 03/2015. Jacked aircraft, inspected and serviced landing gear, t i res, wheels, and brakes. Accomplished 6 fault free gear swing, both normal and emergency. Removed and serviced speed brakes with lubriplate. Installed new battery (PN:RG24-15, SN:40626534), in accordance with (Concord 0/0 Manual, Pg.10). Installed overhauled oxygen bottle (with regulator attached and b,vdrostatic test complete) from AVOX systems and safetied in accordance with (Mooney Service Manual 35-00·02). Operational check satisfactory at this time. Checked all ADs through ATP as of (01/10/2014). I certify this airfram~ has been inspected in accordance with a 100-hour Inspection and was found to be in airworthy condition at this

timet:::

James Caudle 359734SAJt/

ELT exp date 03/2015 Pitot/Statlc Due 04/30/2014 Annual due 01/31/2015

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Inspected aircraft in accordance with (FAR 43, Appendix D)/ Annual Inspection. Performed (6} fault-free

extension and retraction tests (Both emergency and normal}. Inspected ELT in accordance with (FAR 91.207, D).

Inspected/Lubricated all controls, cables, pulleys, and befl·cranks. I certify this aircraft was inspected within the

scope and detail of (FAR 43, Appendix D)/Annual Inspection, and is returned to service at this time.

Glenn MacDermod

30534271A

IL-----~ 1 u 1 AL-varry rurwe1ru LV llt7M tJa~o

Page No. __ _

TOTAL TIME

IN SERVICE

TACH OR RECORDING

METER TIME



'-.1~~E MoonP.. \1u0EL ~.X.P. ~ ~o "'4~"· ~ ~ I • u. ~E- 'll"' '!., J • -::

'.'"'RK "'ROEF :u51 \:.3 :01J

Airframe Entnes

Don Maxwell Aviation Services, Inc.

' 1) Rep<l1red left fuel t.mk leak

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- .1-E ., ... 01"'"1 J - ~- _ .... ~ C TSII

TlCI-'/0~.1

\ DATE 320~0~1~4------------------~S~IG~N~~~-~~~~~~~t~~~~~-----------------------------W_o_rk_O_rd_e_r_2_05_1_-0_3_-2_01_4

Printed by EBis 3 cdarcomed1a.com)

Twin Lakes Avionics Date: 04/1 1/20 14 Model: Mooney M20R SIN: 29-07403 N# 345US W/0# 9195Tach: 1029.0

Adjusted Garnlin GDC 74 lAW Garmin flight line maintenance manual. Performed the Altimeter. Transponder and static system tests required By FAR 91.411 and 91.413

Transponder Make: Gannin. Model : GTX 33, SN: 448393 Pilots PFD Make: United Instruments , SN: 448393 tested to 20,000 ft. on 04 I 11 I 2014.

Pilots altimeter Make: Garmin G 61000. SN: 47805093 tested to 20,000 ft. on 04 I 11 I 2014.

1 Static system. and altitude reporting tested on 04 I 11 I 20 14 to 20,000 ft.

1 The aircraft, airframe. appliance identified above was repaired and inspected in accordance with current ~ I maintenance rules of the Federal Aviation Regulations and is approved for return to seiVice. Pertinent details of

the repair arc on file at tilis repair station • Twin Lakes Avionics, CRS: JB4R278M Ins ected ·

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Twin Lakes Avionics Date: 0-1-/1 1/2014 Model: l\.1ooney M20R SIN: 29-07403 N# 345US W/0# 9216 Tach: 1029.0

)Ved Pitch sen ro. thoroughly cleaned clutch and connectors. checked clutch torque, reinstalled seiVo, and re-tensioned idle cable. Re-flowed solder joints on pitch trim switch. Re-racked autopilot computer. Ground check satisfactory. lle aircraft. airframe. engine. or appliance identified above was repaired and inspected in accordance with current

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• I I maintenance mles of the Federal Aviation Ref,'lllations and is approved for return to se · .

PauiR. ~reerJr.A~P: 3254795~Ir~Is~ec~t~ed~~~~~~-~~~~~~~~~~~~~ -- -

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Thumbs Up Services, LLC

DATE: 7109114 REGISTRATION: N345US TACH TIME: 1047.5 AFIT: 1047.5

Service oxygen syst:m to detennine source of leak per owner's request. System was installed by another party dulUlg the last annual and has been leaking since. First leak was noted at the service line t-fitling in the connection from the "T" to the bottle. Removed line and found th end of the J/8" line was not.properly sea~g dne to damage at the end of the line. Repair~ tube and cleaned compress10n seal. Re-mstalled and re-service system to 1300 · d

r. ed I ak d . . th . psl an per1~nn ~ elect mspecbon on at line and valve, no leaks noted. Next day revealed a 50p~t drop m pressure. Re~oved b.ottle ~d connected pressure to system and fotmd the servtce con~ector reducer fitting Ieakmg behind 02 bottle. Fitting was not properly torqued. Torqued .fittmg and perfonned leak detect check, no further leaks noted. Re-installed bottle and ~omtored pressure for two days, noting no change in pressure reading. Found fastener bad m le~t rem: fuselage access pan.el. Installed a serviceable fastener.

I certtfy tlus System has been ln~'})ected in respect to the abov t ' d k d d . . . . . e men tone wor an was

etennmed to be m auworthy condtlton and is approved for return t ·

?JZ ~125 Michael A. St:tickland

A&P 3544968

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TOTAL-Carry forward to next page

TOTAL TIME

IN SERVICE

TACH OR RECORDING

METER TIME



THUMBS UP SERVICES, LLC

DATE: 210112015 REGISTRATION: N345US TACH TIME: 1090.0 AFTI: I 090.0

Perfonned i)NNUAL inspection using the Mooney Service Manual and FAR 43 Appendix D. Checked all lights for operation. Lubcd aircraft. Complied with Flap discrete check. Charged batteries, owner declined capacity checks, per note 2 in CMM. Perfonned speed brake lubrication and function check. Checked placards. Replaced worn fuel cap, speed brake, and static port placards. Replaced fuel cap 0-rings part numbers MS29513-0 10 and MS29513-338. Inspected fuel strainer installed new 0-ring on part no. MS29512-05. Reinstalled knob on horizon. Removed interior side panels inspected frame tubes, wing bolt torque, and fuel quantity transmitter for leaks, no defects noted at this time. Installed new RT-Al200 fire extinguisher due to current bottle failed weight check (empty). Replaced copilots overhead light GE400. Found AMSAFE EMA life limit expired in 3/2012. Owner notified, system must be function checked by a certified AMSafe technician annually per ICA. Bottles due life limit change 7/2015. Per ICA disarmed system and stowed connectors. Airb~te, System is INOP until units can be replaced and function checks complied with. Placard on instrument panel installed. Inspected brakes, owner notified that disc are right at limits per Parker CMM and to expect change at next lining change. Installed 8 ea. 66-105 brake linings. Removed, Cleaned and installed new MS28775-222 0-rings in left brake caliper, back filled with 5606 and re-installed. Serviced brake reservoir .

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Date: 2/01/2015 Registration: N345US Tach 1090.0 AFTT: 1090.0

Removed, inspected and repacked all wheel bearings. Found all gear shock mounts worn beyond limits. Installed 11 each owner provided J-11968-14 (530021-000) shock mounts and cleaned inspected shock mount tubs, tubes in serviceable condition at the time of this inspection. Work was complied with per Mooney MM 32-81-00. Due to unknown history, performed hard landing inspection per procedures in section 32-82-00, no defects noted at this time. Performed airspeed function check on gear found setting at 60 knots. Checked all preloads: Left gear 270 in!lbs; Right gear 260 in/lbs; nose both measured .063. Performed normal and emergency gear retraction checks adjusted right outboard gear door. Ran 8 complete cycles, all checks satisfactory at this time. Found slight leak in left tank, owner just had repaired 70 hours ago (3/14) and if needed will fly back for further sealing. Perfonned ELT battery replacement and function check per FAR 91.207(d) BaEery Exp. 12/23. _ AD 14-15-18 (SBM20-318) N/A per aircraft SIN. All AD's checked through Bi-weekly

2015-02

1 certify this AIRCRAFT has been inspected in accordance with an ANNUAL inspection and was determined to be in airworthy condition and is approved for m · _ 7 .111 c <~~

Michael A. Strickland A&P3544968IA

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T ___ sUP SERVICES, LLC DATE: 4110/2015 REGIS1RATTON: N345US TACH TIME: 1100.7

AFTT: 1100.7

Removed defective landing lamp from righl wing and installed new GE-4596 250W landing lamp. All operational checks found salisfacloty.

I certify this AIRCRAFT has been inspected in accordance wiU1 U1e above mentioned work detai~ ?nlY. Th~ listed .repairs are dclenuined to be in compliance ain 'Ot1hy

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cond1llons the mrcrafl1s approved for relum to service. r.J.~+.--?'~-,~ \

Michael A. Strickland A&P3544968

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tTAL brought forward from previous page

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DTAL-Carr

Thumbs Up Services, LLC

DATE: 1211212015 REGISTRATION: N345US TACHTIME: 1166.6 AFIT: 1166.6

Removed right main tire part no. 072-314-0 serial no. 1251 S00352 and tube due wear. Installed new tire of same part no. serial no. 5152800056 and new Goodyear tube G 15/6.00-6 TR20 Product identification no. 302-246-4001. Service to 42 psi per manual. Removed cleaned, inspected and repacked wheel bearings. Inspected brake linings and fotmd worn but within limits. Atumal due in February and linings should lost tmtil then. Owner was notified last rumual to expect both main brake linings to be changed next annual, and, further notified with photo of lining wear at this maintenance event. Right broke disc thickness checked and fowtd to be .330, these will need replaced in the near future. Notified owner of lower right brake puck leaking (probably due to lining and disc wear), suggest rebuild at annual or prior is fluid is foWld leaking on ground Perfonned gear retraction checks to ensure tire and inner gear door panel fit and clearances, no rubbing or defects noted at this time. Owner should watch tire as they may stretch until a few cycles are put on the new tire and tube.

I certify this Component has been inspected in respect to the above mentioned work and was determined to be in airworthy condition and is approved 'ce.

Michael A. Strickland A&P 3544968

Thumbs UJ> Services, LLC

DATE: 1213112015 REGISTRATION: N345US TACHTIME: 1168.9 AFTT: 1168.9

Removed right main tire part no. 072-314-0 serial no. 5152S00056 and removed new Goodyear tube G 15/6.00-6 TR20 Product identification no. 302-246-4001 due to pinched tube. Installed owners original tube dated year2012 after inspection and it was determined to be without creases or any other signs of damage and in serviceable condition. Re-installed new tire and service to 42 psi per manual. Checked air pressure after 20 min and no air had been lost.

I certify this Component has been inspected in respect to the above mentioned work and was determined to be in airw01thy condition and is approved for un to service.

Perfonn

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Michael A. St:Iickland A&P 3544968


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DATE: 310112016 REGISTRATION: N345US TACH TIME: 1177.4 AFTT: 1177.4

ed ANNUAL inspection using the Mooney Service Manual PIN I 61 and FAR 43 Appendi x D. Checked all lights for operation. Lubed aircraft. Complied with Flap discrete

otentiometer required adjustment to indicate flaps T/0 position. Charged batteries, eclined capacity checks, per note 2 in CMM. Replaced fuel cap 0 -rings part numbers 3-010 and MS29513-33 8. Inspected fuel strainer installed new 0 -ring on part no. 2-05 and MS9388137. Installed new Compass mount bracket Part no. CF24-727F.

check,p owner d MS2951 MS2951 Remove transmi

d interior side panels inspected frame tubes, wing bolt torque, and fuel quantity tter for leaks, no defects noted at this time. Airbae System is INOP until units can be

and function checks complied with, Plncurd on instrument mmel installed. Inspected replnccd brakes, owner notified that disc are right at limits per Parker CMM and to expect change at next lini . ng change. Installed 4 ea. 66-105 brake linings right side. Removed, Cleaned and mst~lled new MS28775-222 0-rings in Right brake caliper back filled with 5606 and re-installed. Serv1ced brake reservoir. ,

1U ' · · · · · · · · · · · · · · · · · · · · · · · · · · · · · ······· .. Page 1 of2 Continued on next page ....... . . ~t.. ?.~ . .(l(.~~.f ......... .

TOTAL TIME

IN SERVICE

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METER TIM(

DESCRIPTION OF WORK PERFORMEDSIGNATURE & CERTIFICATE NO OF PERSON PERFORMING WOnK

TOTAL brought forward from previous pogo

.. ............. · ... .. .................. Pngc 2 of2 Continued from prcvlnuq pngc ................................. .

Dote: 3/01 /20 16 Rcgistrntion: N345US Tnch 1177A AI· J"l': 11 77.4

Perf~nncd nirspced function check. Checked nil pre-londs: I .en gear 265 in/ lbs; Right gcur 260 m/lbs: nose both mensurcd .065. Performed nonnnl nnd emergency gear rctrnction checks, rnn 8 nil checks sntistbctory nt this time. Serviced nose tire to 49 psi und rnoln tires to 42 psi. \\'heel bearings checked. Found slight leok in len tunk still present but the sumc u~ lost. ~nnunl, ~wner stnted he planned to return to facility that seoled tanks two years prior. nottltcd and 1fnceded will fly back for further senling ot foci!' Performed ELT buttery ~epln~ement and function check per FAR 91 .207(d otter :xp. 12/23 . /'f/ SB M20-32_0 by msertmg pages in POH section 3. C/\V ~0 84-26-02 by rep occment of airfilter (Note Donaldson filter is synthetic material not poper so AD really does not apply. All AD's checked through Bi-weekly 2016-03

'\01F· 1TRP1101 ~1 \riClR\"'~PONDIRt'lllt' f....SDt r.t2016. NOll 02 BOlll I Dt E llYDRO 1 \ llC 'JI \.I 'I \R D NOTI:.. 11\IGI'\lr \lR I IL TI R Dt 1: Cl t\NGI' 1677.-t OR 3 2019.

I certify this AIRCRAFT has been inspected in accordance with an ANNUAL inspection and was detcnnincd to be in airworthy condition and is approved for retu to se v'ce. ., /

~ut4d/Y Michael A. Strickland

A&P3544968IA

Pogo No

---------------------------------------------------- -------Twin Lakes Avionics

Date: 4/8/2016 Model: Moonev M20R SIN~ 29-0403 N#345 US W IO# I 0 I 07 Tach: 1180.5 ~

AD 08-02-06 Not applicable: GSM 85 not installed in £his aircraft. Completed I OOOhr Electrical Bonding lest iA'W' Gnrmin G i vOO ma;nt~~~rtCC ;~ar.~a! !:ection 1L3.1 Performed the Altimeter, Transponder and static sysrem tests re0.u1red By FAR 91 .4 1 1 and 91.413

Transponder ivtake: Garmin Model: GTX 33. SN:8470 1492 Pilots PFD Make: GDC 74a, SN : 86502729 tested ro 20,000 ft. on 4/8/2016.

Pilots standby a ltimeter Make: United. SN:448393 tested to 20.000 tl. on 4 '8/ 20 16. Static system, and altitude reporting testtd on 1l/8/20 16 to 20,000 ft.

I

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The aircraft, a irframe, appliance identified above was rcpaired·and inspected in accordance with current maintenance rules of the Federal Aviation Regulations and is 1.1pproved for return to service. Pertinent details of

the repair arc on fil e at this rcpatr stati

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-b=:J1Q"w~·~·n~L~a~k~es~A~v~io~n~ic~s~,~C~R~S~:~J~B~4~R2~7~8~iV1~1~ns~p~e~.c.t~c~'d~~&l~~:::.::~~~~==c.::: .. ::'::~--_]_


DATE: -111212017 REGISTRATION: N345US TACH TIME: 1240.3 AFTT: 1240.3

Performed ANNUAL inspection using the Mooney Service Manual PIN 161 and FAR43 Appendix D. Checked all lights for operntion, found afi strobe inoperative. Researched nnd checked wiring. Removed rechecked all wiring, re-installed and system found to \\ork nt this time. Lubed aircrafi. Complied with Flap discrete check. Replaced fuel cap 0-rings part numbers MS29513-010 and MS29513-338. Inspected fuel strainer installed new 0-ring on part no. MS29512-05 and MS9388I37. Instnllcd new throttle cable Port no. 660226-027 \\ith new bearing Part no. I-IF-3M, ground rigged genr warning call out. Removed interior side panels inspected frame tubes, wing bolt torque, nnd fuel qunntity trnnsmi tter Lor Jenks, no defects noted at this time. fnslnlled new brnke disc purt no 164-02300 both sides due to w~or. Installed 4 ea. 66-105 brake linings len mnin. lnstnlled new Goodyenr Flight Custom 116.00 X 6 6 ply tire port no. 301-027-420 on lefi mnin. Removed 02 bottle for 3 yenr hydrostatic

51 check. Re-installed and serviced to 1100 psi and no leaks noted nt this time. Peribrmed airspeed function check. Checked all pre-loads: Lcfi gear 264 inllbs; Right genr 26..J in lbs~

Tt nose both measured .063. Perfom1ed normal and emergency gear retraction checks. Found ten main tire rubbing mud shield . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .... Page 1 of2 Cosltitt\aed 011 1\CXt pngc .. ..... ......... ... · .. · · · · · · · · · · · · · · · · · · · · · ·

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DATE TOTAL TIM I:

IN SERVICE

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Dnlc ·I 12 2017 Rcg1s1rn11on NJ45US Tach 1240.3 AFTT: 1240.3

Vurwu~ checks round u1sc sci v1ccnhlc. assuc ~vns rcsolvc.d with instnllalion of n~w Qu?lity _tire JlCI ·~commcndnllon of SCI\ ICC ccntea tcchll1Cil\11S. Old tare hnd o.nt SfOl. Afier mstnllmg tare,

0' ., H n.:llnct1011 test nntl round uthourd genr doors needed udjustmg. Cycled gear

Jill\ C I • ' d ' ' ndd1r1onnl 8 tunes. nil chccl..s snt asfnctoJ V nt tha s tunc. Service nose tare to 49 psa and main

111 ~s to 42 ps1 Wheel beatings acmovcd, !n~!>cc t cd, and repacked. Installed. new #I battery RG-15 Scnnlno.40H•II •I4 0. Performed J·.L I bntlcry replnccmcnt nnd function check per FAR 91.207(d) Battery Exp. 12 23. All AD's checked through Bi-weekly 2017-07

~n 11 p\~ Nl R NU IIIII J) lilA I Sl'l I D HRAKI·S UYI l<l>l JJ RJ CnMMT NDJ I>

0\ 1 Rll \ lll 1 O il 0~ HOI III Jill llt-.111 I XPIRI '\IN Mn' 2020 NOTJ \lRH \(i ~'"II M Rl t-.1/\ INS INOPI•RA IIVF PrR OWNl RS Rl QlJF I )I \ C \ RDS s 1111 11\1 PI \ Cl IN COCK PI I ON PANNI L

I ccrtilY this AIRCRAFT hns been inspected in accordance with an ANNUA~ inspection and wns determined to be in nirworthy condi tion and is approved n rvt e

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TI IUMBS UP SERVICES, LLC

DATE: 9116120 17 REGISTRATION: N345US TACHTIME: 1264.3 AFTT: 1264.3

Inspected landing gear per owners request for tar sealant that was picked up from ramp crack sealing program. Noted large amounts of tar on all three wheels; no tar noted in wheel brakes or rim assemblies. Attempted to remove while tires installed, found access difficult. Jacked aircraft and removed main tires and cleaned tar off tires. Washed tires with soap and water after process. Inspected and repacked main wheel bearings, inspected brake disc and linings (no issues noted with plenty of wear left on linings). Cleaned nose tire while installed but jacked and spun tire to note any bearing noise, none noted at U1i s time. Main tires found 5 lbs low, serviced to 42 p~i per maintenance manual.

I certify the ~omponen~s li~ted above wh~~e inspe~tcd and re-installed after cleaning and have been deterrmncd to be m (llrworthy cond1hon and IS approved for re ight.

~~:z:~ Michael A. Strickland

A&P3544968


DATE: 511912018 REGISTRATION: N345US TACH TIME· 1296.8 AFIT: 1296.8 . ..:...::.::~

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Performed ANNUAL inspection usin the M . -Appendix D. Checked all lights foro gpe t' oofiney Servtce Manual PIN 161 and FAR 43 new GE4596 L b · ra ton, ound Left Land' 1 · · _ · u ed a1rcrafi. Complied with Fl . mg amp moperatlve, installed Inspected fuel strainer installed new O-rin ap dtscrete check. Inspected fuel cap 0-rings G~ound rigged gear warning call out Rer:o~~ P~ n~. M~29512-05 and MS9388137. wmg bolt torque, and fuel quantity t · . d mtenor stde panels inspected frame tubes, Installed 4 ea. 66-105 brake linings :~mttte: for leaks, no defects noted at this time. function check. Inspected static m g t mam. Jacked aircraft and perfonned airspeed a 10 ll easurement ofland' pprox. ga ons lower Right checks at 395 mg gear collars with full right tank left -all pre-loads: Left gear 270 in/lbs· Ri ht. and ~eft at .300; Nose had no gap. Checked Performed 10 normal and 4 en1e ' g gear 265 tn/lbs; nose both measured 045 · rgency gear retr · • ·

lime. Owner made aware that a new tire w' ll l'ku~hon checks. With no defects noted at this change. Current collar is u -005 ~vould 1 1 e Y cause the left main to require a collar .. • ... ................. • .. · · .... · ..... Pnge 1 of2 c~~~~n~~~~dn:x~OO 1 eas installed on the right main.

png 0. ••••• I. t II I ••••• • • • I t • 0. • •• e • ••• f ••• 1 • t • ••• t

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TOTAL TIME

IN SERVICC ...... ...................... Pngc 2 of2 Continued from previous pngc .... .. ...................... .. .... .

Dntc: 5/19/2018 Rcgistrntion: N345US l'nch .1226.8 AFrr: 1296,8

Serviced nose tire to 49 psi nnd mnin tires to 42 psi. \Vhccl bcnrings removed, inspected, und repnckcd. Grensc speed brakes gcnr per mnnunl. lnstollcd one len elcvnlor stotic wick pnrt no. 10-900-60/ I . Serviced brnkc reservoir with 5606. Performed EL r function check per FAR 91.207(d) 13nucry Exp. 12123. All AIYs checked through Bi-weekly 20 18-lO

01 r 0\\ Nl R NOrtrtl DIll,\ 1 SPrt D BRAhl ~ OVI RDlJI RH'O~I~II NDr l> OVHHIA IJI. NOI r · 02 BOI 11 F llFl I lt-.11 r l· \PlRrS IN Mn) 2020 'JOl r \lRH.\G S\ Sll M Rl MAINS INOPI·R \ IIVL PI'R OWN! RS R£ (.)lJJ '\I PI ACARDS ~ 111 l IN Pl \Cl IN COCI,Pl rON P \NNrt

l certify this AIRCRAFT hns been inspected in accordance with an ANNUAL inspection ru1d was detennined to be in airworthy condition and is approved for return to service .

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SUB-TOTAL this page

TOTAL-Carry forward to next page

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Page No.

AJrcreft Record G&nerallnformahon

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llanufacluror (!Jr.f_[J1Jf;IH/1L Model

Manufacturer Model _____ _

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llonufoctu,., H/bt~Z £-• .:J..I$, tft)E" Model

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SICNATUREc9c , l '--D !/'....-© DATE Jli!.LI.ILIGl!I09!1!8!.-______ _

WORKORDERN~4~0~2S~----------

Airframe Log #I Open: 12/9/2005 · FAR 91 .207d. Inspected and serviced landing gear, tires,...

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Transcript of Airframe Log #I Open: 12/9/2005 · FAR 91 .207d. Inspected and serviced landing gear, tires,...