·rcraft Record General Information

·rcraft Record General Information

anulao~urer iJ; ~ Serial 3,)R&"1'd' OC\"2:> :late of Manufacture

Model PA- ·~- '30\ 'I ____ _ Registration Number ~~.~L\ ___ \-\ _______ _

e- gine(s) currently installed: 1

ufacturer l .... \JC.0'<Y)"oc{f Model \ ·io5L\.Gil..l\t)serial l ... J \ 0£:,- (o\ A nufacturer _________ Model Serial ____ _____ _

opeller(s) currently installed:

nufacturer \-\U. i'k2.0 \. \ _ Model :\-:\C.,~- \: 3~ (<.. - \ ~ F .. B Model £ 'l \.Ji\o 3 't.J_ ..... R'-"'----Serial Serial £'M_ \ 03 LJ> A

ade Model------- ---Serial _____ Serial _ ____ Serial _____ _

- de Model _____ _____ Serial . ____ Serial _____ Serial _____ _

.--.)1'.e I J~l'..'.'.01 4 /l•rc~'lft: N8'.::141-1 71ipe : PA-32R-20~T SIN: 32R ·80'.::3093 Tach· ) 438 50 YMI· J.:J 26 DJ

. "' .. !Ci'oJ '1' fC:f"'lft r•a \1-• ~ Df:l:-'€' -~s.:r Olf :lr.d '1')"Jr:.u ,II::: :J• • .;~·f '}<lt:K r~o;er, '.Jlf

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s:;,I - '11! pr " ' -:'/(;•. Sin. 30M , ."(•

=-r.•.:. ::. ; i ,, • :1· 1'1t:e•i right •lutno::iM -,er 11rig ,1111 with ov.:r''d•J1ed unit ptn . : ·· 40-0u::Ol-1 PS I 001,'.-1 l), ~1n

• : _:: ~ ,:; · ~ ne•v::: ~sKet Rc-111ovr:-·J an1J re,1mce-•: 1nr.lJariJ :11F:I ScP<l1ng\1rnt with c·1erh;:i1 rier1 • 1nit pm

- ' .: --~: ::) : v ' • .H~A • sin 1 4~.aog :..s1r.g new 1n~Ke!s Ren ,,ca!le<:l ·1gnt ' t .e1 tank. 1-<efut1e.j checK ' .. a11orat1on ; 1; • ,,,.: a~ "' vc;. :1·.:i;K<~· 1 90<..· 1. · Jo Jealts nom,j ( - l - : .~r· .:- •· -:i ··~"ar": un ncn1 ;nb· · ir•: '.1'"11eir" Jn,;ta1:.,,.'! ·:.'.) '1ew :11r. 'v1S~J6~4L5 s·:·ews and J_ "~"" n,,,., l _ .... ..:._ - .. ! ~C.t~i:,or; -

T~ s fh · raft i "r:irne i';'lg1ne or app11·anr'. · 1 ·f .. • . . _ . • · .e it t:ntl 1e1, was 1 o::paired and .nspecte•j in accordance o111tl1 current · fl~A;. ~·-~ '> ilLµrc,;e.-: ·01 re1l1rn r: service. 3t1cc 0rrJE·' ' :1.A-14-.2898

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===

TOTAL TIMEIN SERVICE

Current Weight and Balance Information

Empty Weight Empty CG Useful Load Remarks

y

2 D

Date: 5/1212015: Aircraft: N8214H' Type PA-32R-301T; S/N: 32R-8029093: Hobbs. 361 .30: Total Time· 3441 60 3!1op Order#: MA-15-3064. Closed· 6101/2015

~ , certify that th;s aircraft has been inspected in accordance with an ANNUAL INSPECTION and current FAA Regulations and was determined to be in an aiiworthy condibon. Time in service since last annual inspection= 1'5 1 hours. Pertinent details are on file at this facility under Shop Order# MA·15-3064

'.. Removed. cleaned. and inspect~d the en!,line fuel controller fuel inlet screen.

3 .nspected and ops tested EL T min ME406 sin 197-11356 per FAR 91 207(d). Battery replacement is due 3t31(L018. Reinstalled ELT in aircraft and armed. Ops checked good.

4 .nstalled new 83-5-1 vacuum regulator Otter.

'3 nspected and cleaned main fuel filter. Reinstalled using new MS29512-043 o-nng. No leaks noted

6 :..anding gear cleaned and lubed

7 '3er11r.ed tires 'Nllh air· N = 35 psi. M = 38 psi. Serviced brake reservoir.

a. The 1anding gear has nad 4 retractions and 1 emergency extension. ChecKed good.

'J installed new fire extinguisher m,~1 RT-A600 pin 13-0/655 sin y_49·1 132 in aircraft.

10. Installed new nose wheel ,·ace p/n: 082J1and beflring pin: 08 125. Greased bearing

' Alterations te Number of iecific entries.)

11 f)isconneded <ind inspected nose landing gear shimmy damper. Dampener checked good. Reconnected shimmy damper

' 2 Luoed nose landing g~ar and nght !anaing gear down lock. pivot points with LPS 2. Worked down lock ossembly and swung landing gear. Ops cheicked good on second emergency extension.

• 3 Removed battery G35 SN. G027618.44. charged and periormeo capacity test. Charged battery according to :1e Gill Ory-Charged lead acid battery manual document 0 01-1120 Rev G dated 9118114 Retested and battery passed wtth 90%+ capac:1ty Recharged battery. serviced with distillea water and reinstalled.

• 4 AD 93-05-06. Amendment .39-851 1. Issued 4/2911993. "Ger1es Ignition Switch Inspection". Next inspecilon s due attach 3929. 7

• 5 Note. AD 2013-02-13. Amendment 39-1/334. Issued 112212013. "Stab1lator Control System Inspection" due at acn 5403.09 or 5131/7020. Tach time left •s 196~.03 or by 5/31/2020 whichever occurs first.

•6 Comply with Instructions for Continued Airworthiness for the Aspen Avionics PFD in accordance with Aspen Document pin. ~00-00012-01 Revision T. Inspected Aspen Internal battery checked at 95%. Inspected Aspen for j amage. No damage noted.

· - Complied with instJ uctions for Continued Airworthiness for the Garmin GDL-69 XM Weather Receiver in aecorcmrice with Garmin Document p/n: 190-00355-00 Revision E dated ~/9'2011 . No defects noted.

3 Compli~d •Mth Instructions for Continued Airworthiness for Garmin GA37 XM/GPS antenna per document q0-0001.;..01 Rev F datea 812112007 No def1::cts noted.

' 3 Comolied with lpstn.ict1ons for ConlJ11ued >\Jrworth1ness for Garmin GNS-5::10W IAW garmin Document pin:

.neratlons Number of :ific entries.)

--YE. 20 DA'

20 Complied with Piper Service Bulletin 1244A. Aft Wing Attach Fitting Inspection. issued 41112013 .. Both checked good. No corrosion noted Treated areas with AV8 corrosion preventative spray compound.

21. Complied with Service Bulletin 1242. Date issued 1/3012015. "Rudder Pedal Assembly Inspection". No defects noted. Reinstalled and tightened four bolts in rudder bar support.

22. Complied with Service Bullebn 1216. Date issued 915/2012. "Aileron Rib Inspection". No defects noted.

23. Installed oxygen bottle pin 800112-21 sin 24080W16721 after hydrostatic testing. See FAA Form 8130-3 issued by Aerospace Turoine Rotables Serviced oxygen bottle to 1750 with Aviators Breathing oxygen.

~4. Installed new 011 pressure switch pin 587-961 behind co-pilots side instrument panel.

25. Installed two new cotter pins pin: MS24665-1 32 for torque link bolts on left landing gear .

26. Installed new nose landing gear limit switch actuator pin: JE-6. Ops checked good.

21 Trimmed gap seal away to clear aileron edge on left aileron.

28 Trimmed the end of the static wick on the left aileron.

29. Provided chafe protection with tywraps to the electric wires on pitot I static tubes and union b-nuts inside left wing 011tboard of landing gear.

30. Removed old static wick and installed new pin: 494-678 on the base of the right aileron.

' Iterations i Number of cific entries.}

I

,

'

--:1 Cleaned both wing fuel cap seals with isopropyl alcohol.

• _ Installed a new cotter pin pin- MS24665-132 on left wing flap control art rod end.

23 Cleaned both wing tip lenses .

• tl Installed new rudder lower bearing pin: 452-387.

"5 Checked and retorqued hardware on vertical stabilizer per Piper Maintenance Manual. Section 55. General.

:~ Media blasted. cleaned. and painted the cap and brake reservoir vent tube .

.: - Cleaned corrosion on aircraft battery with caking soda and treated metal straps with Corrosion X.

38. Installed one new pull type rivet in nutplate and sealed nutplate strap to batte1y box with with RTV sealant.

: 3. Secured wire harness under copilots instrument panel with tywraps and existing strap clamp. Moved controls ·".rough pull travel No further chafes noted.

-0 Resecured the glove box plasllc cover with black RTV sealant.

-11. CompUed with ICA for "STC SA948NE LP Aero Plastics Windows" . No c'lefects noted.

- h ee Wing Aviation Group. LLC 400 Great Meadow Rd Stratford. CT 0661 5

·anc identified was repaired and inspected in accordance with current r return to service Shop Or er MA-15-3064.

~~~~IS'

Alteratlo"b te Number of ecific entries.)

2 D

-

Thr ee \\t ing J1 111ation Group , LLC CRSc SL 5R20lN l"K):: AV-15-1666

N8214H Pipe r PA-32R-301T SN: 32R-80~9093 5/S/2015 Tach : 3441. 6

Remov~d transponaer Garmi n GT)(-~30 PN: 011-00455-00 SN : 84134121 and shipped to Garmin for upgrade to ES (ADS-B Out ) .

Installed RS-232 data wi re between GNS-530W RS-?32 out 1 and GTX-330 RS-~32 In 1. Replaced existing GTX-330 c1 rcuit breaker with a PN : 7277-2 - 5 pull able breaker.

Updated the e-..i ~ting Garmin GNS-530-.'i PN: 011-01064-00 SN: 23820360 from Main software 3 . 30 and GPS SW 3.2 t:O Main SW 5.20 and GPS SW 5.0 IA'w Garmin SSS 1225 Re v B, 1315 Rev A, 1317 Rev A. 1401 Rev A. 1403 Rev B, 1461 Re v A, ;ind 1474 Re v A.

Replaced GNS-530W AFMS with new PN: 190-00357-03 Re vis i on E dated 11/20/ 2014. Pr int:ed and placed in aircraft records package soow Series ICA document PN: 190-00357-65 Re vision o. Installed Garmin GTX-330ES Transponder with ADS-B out functionality PN: 011-00455-60 SN: 84134721 IAW FAA STC SA01714WI and Garmin Installation Manual PN: 190-00734-10 Rev. 4 dated September 2014. Aircraft i s listed on the AML fo r STC SA01714WI .

GTX-330ES transponder tested good per secti on 7 & 8 of the t:he STC Installation Manual and per FAR 43 APP F. Updated weight and Balance and Equ i~ment: li st. Filed FAA Form 337 .

Installed FAA Approved Flight Manual supplement: PN : 190-00734-15 Rev 1 dated 5/ 1/2013 into POH supplements section.

END

~~~/r-' Kamlesh Rana SL5R201N Date

-

-

Alterations te Number of 1ecific entries.

I

]

'

"

-s RECORDING YACH TIME

TODAY'S FLIGHT


Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Reoalr Facllltv. <See back oaaes for other soecific entries.)

Three wing Aviation Group, LLC CRS " SLSR201N r/O• AV-15-1'774

NS214H Piper PA-32R-30lT SN: 32R-8029093 11/3(1/ 2015 Tach: 3451.8

compl ied with FAR' s 91.4111413 Test s

Tested Aspen EFD-1000 PFD PN : 910-00001-001 SN: 4341 per FAK 43 App E :mo A~pen Tech Note 2009-09 Re~ c dated 2/~0i20l3 t o 30.000 feet. Tested good .

Removed backup altimeter united 59 34P-1A.83 SN: OJ447 and tested to 20.000 feet oer FAR 43 App E. Tested good and re1nstalle~.

Tested transponder G.:irmin GTX-330ES PN: 011-00455-60 $N: 34134721 ( S\>I 7.04) p~~ FAR 43 App F. Tested good .

Tested Trans-Cal $SD120-30N-RS~3~ SN : Nll9 72 encoder per FAR 43 App E Para c. Tested good.

Tested static system pe r FAR ~3 App E. T~sted good.

ENO

- ~------t-11 t-----t-------

YEAR 20 _ _ DATE

RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back paoes for othAr snAcific entries.)

Date: 411512016. Aircraft N8214H: Type: PA-32R-'301T: S/N: 32R-8029093' Tach: 3453.60

Har1Zell min HC-E3YR-1RF sin FM1576B Prop TT. 255 71 TSMOH. NIA

1. Removed propeller from N8714ti .. --------:-END------- -

ThrE-e Wing Avmbon Group LLC 400 Great Mead9v+Rd Stratford. CT 06615

Th;s aircraft. a1rtrame. angine or appliance identified was repail ed and inspecten ~g~cordance ,With current reglilations of the FAA and is approved for return to·serv1ce. Shop Order MA-16- •· '

· ~ \tiA.J). -, ~ . : Michael T. GavaghanA&P347342 IA

4"' / S-: fjOI_'-_ - date

~ • ~ ', 'r••" ·. . ,~,

-··' ~ .. i.i ..!- ~.: •'; .'.i.· -

__ L____,__~J,_----

--- --------~~~~~~~~~~~~~~-,--,---,-,-,-~-,-~~,..,,-

Date: 5110'2016. Aircraft: N8214H: Type: PA-32R-301T: SIN: 32R-8029093: Tach: 3453.64; Total Time: IS UR

.) :-e

3453.64

1 I certify that this aircraft has been inspected in accordance with an ANNUAL INSPECTION and current FAA Regulations and was determined to be in an airworthy condition. Time in service since last annual inspection= 12.04 hours Pertinent details are on file at this facility under Shop Order# MA-16-3405

2. Removed. cleaned. and inspected the engine fuel controller fuel inlet screen.

3. Inspected ann ops tested ELT min ME406 sin 197-11356 per FAR 91.207!d). Battery replacement is due 3131'2018. Reinstalled EL Tin aircraft and armed Ops checked good.

4. 1nstallec1 new 83-5-1 vacuum regulator filter

5 !nspected and cleaned main fuel filter. Reinstalled using new MS29512-043 o-ring. No leaks noted.

6. Serviced tires with air: N = 35 psi. M = 38 psi. Serviced brake reservoir.

7. Landing gear cleaned and lubed. Landing gear operation checked-normal and emergency. Ops checked good.

8. Inspected and weighed portable fire extinguisher min RT-A600 sin Y-491182. Weight 1 lb. 9.7 oz.

9. Painted red witness mark on bottom cowling right forward latch.

1 O Installed new bearing pin 0812~ and race pin 08231 in no~e wheel left side · ~ Secured loose strobe light iens 1n left wingtip with RTV108 Sealant.

- _ubed and freed seized aileron control cable pulleys in both wings outboard of the tie down rings.

'3 nstalled new bonding jumper pin 469-600 on left aileron.

6 Complied with Instructions for.continued AlrNorth1ness for the Aspen Avionics EFD-1000 IAW Aspen Jocument # 900-00012-001 Revision W Sections 11 & 12. No defects noted.

~.:;;"stalled new left forward trim r.able pin MC62701-135 IAVV Maintenance Manual Section 27-30-002 (bl

'E !nstalled one rivet pin MS20470AD4-4 on each forward oxygen cylinder mount support stiffener.

•ations iber of 3ntries.)

YEAR 20_ DATE

17. Adjusted stabilator rigging and cable tensions IAW Maintenance Manual Section 27-30-00 (2) (a-1 ) and figure 20.

18. Service oxygen system to 1850 psi 'Mth Aviatiors Breatlling Oxygen.

19. Note: AD 2015-19-07 Amendment 39-18269 P.ffecbve Nov 3.2015 is due at Tach 3541 .6 (88 hrs to go). inspection of fuel injector fuel lines and support clamps.

20. Note: AD 91-?. 1-01R1Amendment39-9470 effective June 27 1996 Inspection of exhaust system is due at racn 3541 o. (88 hours to go).

21 . Note: AD 93-05-06 Amendment 30-8511 Inspection and lubrication of Gerdes ignition switch is due at Tach 3925.7

22. Note. AD 2005-·l 2-06 Inspection of the Magneto lrnpulse coupling is due at Tach 3757.8. (304.2 hours to 901.

23. Note. AD 2013-02-13 Stabilator Control system inspection is due attach 5403.9 or by 5131/2020.

24. Complied with ICA for Garmin GDL-69 IAW Document#190-00355-00 Rev E Dated 5-9-2011. No defects noted.

25. Complied with ICA for Garmin GA-37 Antenna IAW Document# 190-00673-01 Rev F dated 8/2i/2007. No defects noted.

26 Complied with ICA for Precise Flight Standby Vacuum System SVS V. IAW Document No. 08072 Section 3 3 1. 1. No defects noted.

27. Installed 3 new bushings pin 95061-00!? in cabin center noor.

28. Comµlied With ICA for flap hinge fairings and gap· seals by visual inspection. No defects noted.

29. Complied with aircraft battery capacity check using BC-7000 battery tester for Gill rn/n G-35 s/n G02761844. Battery tested good. Recharged battery and reinstalled.

30. Installed new cabin heat inlet duct pin SCAT 12.

31. Installed new 011 cooler air inlet duct pin 18013

rati< -nber entri1

-ns >f s.)

32. Installed new alternator belt p/n 73965-003 Tensioned belt and safetied tensioner bolt.

33 Removed and replaced rivnut ptn NAS 1329A06K075 on flap hinge fairing.

34. Removed propeller min HC-E3YR-1 RF sin FM 15769 cind sent to New England Propeller Service for overhaul. Reinstalled propeller min HC-E3YR-1 RF s/n FM 15768 after overhaul IAW Piper Maintenance Manual Section 61-1 0-00 Figure 4 and Chart 3. Blade track checked good. See FAA Form 8130-3 dated 4127/2016 work order# CR-42612 from New England Propeller. Inc.

Three Wing Aviation Group. LLC 400 Great Meadow Rd Stratford. CT 06615

This aircraft. airirame. engine or appliance identified was repaired and inspected in accordance with current regulations or the FAA and is approved for return to service. Shop Order MA-16-3405.

1/V\Q-r,_21z9> Michael T. Gavaghan A&P 3473342 IA

I

S-,,;o~:J.ol< date

:Jate· 1/30/201i: Aircraft. N82t4H: Type: PA-32R-301T: SIN: 32R-8029093: Tach: 3475.38

• Removed Gill battery pin G-35 s/n G02761844. Installed new Concorde battery pin RG-35AXC sin 40828676. Updated Weight Jnd Balance Equipment List.

~ Serviced tire~ with air N= 35 psi: M= 38 psi.

n ree Wing Aviation Group. LLC 400 Great Meadow Rd Stratford. CT 06615

- his aircraft. airframe. engine or appliance identified was repaired and inspected in accordance with current regulations of the FAA and •s a~proved for retu t ervice. Shop Order MA-1 7-~pa. I "1ic~ael T. Gavag an A&P 34 7 2 IA

1 I j5 ~ / Z

- I

terations lumber of ic entries.)

YEAR 20 _ Date. 6/2012017: Aircraft· NB214H: Type: PA-32R-301T. S/N: :l2R-8029093, Tach: 3475.69

DATE Hartzell min HC-E3YR-1RF s/n fM1576B Prop TT. 277.76 TSMOH: 22 05

I . Removed propeller from NB214H -·------END---- -------Three Wing AYlation Group, LLC 400 Great Meadow Rd Stratford. CT 06615

Shop Order MA-17-3798

~/.

.

-

'Iona 1r of ries. '

i '

• RI Date: 10/2512017; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Hobbs: 383.40; Total Time: Tl 3475.69 Tl

1. I certify that this aircraft has been inspected in accordance with an ANNUAL INSPECTION and current FAA Regulations and was determined to be In an airworthy condition. Time In service since last annual Inspection = 22.05 hours. Pertinent details are on file at this facility under Shop Order# MA-17-3788.

2. Inspected and ops tested ELT min ME406 s/n 197.11356 per FAR 91.207(d). Battery replacement Is due 3/31 /2018. Reinstalled EL T In aircraft and armed. Ops checked good.

3. Installed new B3-5-1 vacuum regulator filter.

4. Inspected and cleaned main fuel filter. Reinstalled using new MS29512-043 o-ring. No leaks noted.

------11-- 5. Serviced tires with air: N = 35 psi; M = 38 psi. Serviced brake reservoir and hydraulic power pack reservoir.

6. Landing gear cleaned and lubed. Landing gear operation checked-normal and emergency. Ops checked c-=-----1-- good.

- 7. Inspected and weighed portable fire extinguisher m/n RT-A600 sin Y-491182. Weight 1 lb. 9.5 oz ..

----1-- 8. Secured loose heat shield material in engine top cowl as necessary with 3M-847 adhesive.

----+-- 9. Resealed windshields and side windows as needed with RTV-102 sealant.

10. Installed new p/n 469-600 bonding jumper on left wing flap.

11. Installed new pin 09-18-1 Instrument air inlet filter.

12. Serviced aircraft oxygen system to 1850 PSI with aviators breathing oxygen.

ind Alterations ificate Number of ir specific entries.)

YEAR R 13. Installed new pin 67026-007 bushings and pin AN175-32 bolt in right MLG torque link top position. Shimmed and Alterat 20 __ Tl as needed with p/n 2JHC9 shims. Checked good for play. ificate NumbE DATE Tl

~r specific ent 14. Installed two new pin 08125 bearings and pin 08231 races In nosewheel.All wheel bearings were cleaned and greased with Mobil #28 grease.

15. Serviced both MLG struts with Nitrogen to 4.5" of exposed tube.

16. Installed new p/n 1g3_1 O hose for AUX vacuum system in engine compartment.

17. Complied with Instructions for Continued Airworthiness for the Aspen Avionics EFD-1000 IAW Aspen Document# 900-00012-001 Revision Y Sections 11 & 12. No defects noted. Internal backup battery passed 30 minute capacity check. Recharged battery.

18. Complied with Instructions for Continued Airworthiness for Garmin GNS-530W IAW Garmin Document pin: 190-00357-65 Revision D dated 1112012014. No defects noted.

19. Complied with ICA for Garmin GDL-69 IAW Document #190-00355-00 Rev F Dated 6111/2015. No defects noted.

20. Complied with ICA for Garmin GA-37 Antenna IAW Document# 190-00673-01 Rev F dated 8/27/2007. No defects noted.

21. Complied with ICA for Garmin GTX 330ES transponder IAW document No. 190-00734-11 Rev. 5 dated 10/512016. No defects noted.

22. Complied with ICA for Precise Flight Standby Vacuum System SVS V, IAW Document No. 08072 Section 3.3.1.1. No defects noted.

23. Complied with ICA for Knots 2U flap hinge fairings and gap seals by visual inspection. No defects noted.

--rhree Wing Aviation G.roup, LLC 400 Great Meadow Rd Stratford, CT 06615

This aircraft, airframe, engine or appliance identified was repaired and inspected In accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-17-3788. · ··

rM.Q _.., I\ f\. io- cl.')~ d.017 ......... '\

Michael T. Gavaghan A&P 347~1A date

-s 'EAR Date: 10/25/2017; Aircraft: N8214H; Type: PA·32R·301T; S/N: 32R·8029093; Tac~: 1119'1 l~~O'f ~

1. Complied with FAR'S 91.411/413 Tests _,,.... __ _ Tested Aspen EFD-1000 PFD PN: 910-00001-001 SN: 4341 per FAR 43 App E and Aspen Tech Note 2009-09

- - -- Rev D dated 417/2016 to 30,000 feet. Tested good.

Removed backup altimeter United 5934P-1A.83 SN: OJ447 and tested to 20,000 feet per FAR 43 App E. Tested --- good and reinstalled.

--- Tested transponder Garmin GTX-330ES PN: 011-00455-60 SN: 84134721 (SW 7.04) per FAR 43 App F. Tested good.

---

Tested Trans-Cal SSD120-30N-RS232 SN: N11972 encoder per FAR 43 App E Para C. Tested good.

Tested static system per FAR 43 App E. Tested good.

Three Wing Aviation Group, LLC 400 Great Meadow Rd Stratford, CT 06615

Work Order AV-17-2099.

identified was repaired and inspected in accordance with current regulations tion and Is approved for return to irvice. epair Station No. SL5R201 N.

lq l. I I ~_..--..::;,~~-tC--~~~~~

Date

1irs and Alterations I Certificate Number of r other specific entries.)

YEAR 20 __

DATE

RE CORI TACff TIME Date: 6/01/2018; Aircraft: N8214H; Type: PA-32R-301T; SIN: 32R-8029093; Tach: 3517.40

-----+-- Serviced tires with air: N = 35 psi; M = 38 psi. Serviced brake reservoir.

Lubed all exterior flight controls, hinges, and rod-ends.


This aircraft, airframe, engine or appliance identified was repaired and inspected in accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-18-

- - ---+---4196.

6-/-IY' date

----11--- - Date: 8/06/2018; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Tach: 3535.00

----+-- - Removed ELT min: Artex ME-406 s/n: 197-11356. Installed new battery p/n: 452-6499 rev: F s/n: 377464-051 . Reinstalled EL T Artex ME-406 into aircraft. Ops checked good with unit switch and

----+---with remote switch per FAR 91 .207 (d). Battery expires June 2025.

-----+---Three Wing Aviation Group, LLC 400 Great Meadow Rd Stratford, CT 06615

-----+---This aircraft, airframe, engine or appliance identified was repaired and inspected In accordance with current regulations o AA and is approved for return to service.

-----+--- Shop Order ~,,...Rl'Z

Altera :e Numb ecific en

Date: 9/05/2018; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Tach: 3566.54

Complied with AD 2015-19-07 dated Nov 3, 2015. Inspected fuel injector lines and clamps per Service Bulletin 342G. No defects noted. Next inspection due if fuel lines or clamps are loosened or moved, after engine overhaul, 110 hours time in service since last inspection. Next Inspection due at 3670.5 hours tach time.

Complied with /\D 91-21-01 r~ ·l dcluJ Jun 27, 1996 paragiaph (a)(2) inspected exhaust system. No defected noted. Next inspection due at 3666.5 hours tach time.


This aircraft, airframe, engine or appliance Identified was repaired and inspected In accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-18-4303.

<::t/sjA?t~ 1 ate

Date: 9/05/2018; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Tach: 3566.54 .

Placard ADF inop. Label wire ADF and disconnected from KR-87 circuit breaker Insulated wire and secured to wire bundle under panel.


This aircraft, airframe, engine or appliance identified was repaired and inspected in accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-18-

--4303.

~~~ Kei.BoT &P IA 3492553 --9-·5-{fF

date

airs and Alterations :l Certificate Number of ir other specific entries.)

YEAR 20 _ _

DATE

Date: 1210512018; Aircraft: N8214H; Type: PA-32R-301T; SIN: 32R-8029093; Hobbs: 459.10; Tach: 3582.43; Total Time: 3582.43

1. I certify that this aircraft has been inspected in accordance with an ANNUAL INSPECTION and current FAA Regulations and was determined to be in an airworthy condition. Time in service since last annual Inspection= 106.74 hours. Pertinent details are on file at this facility under Shop Order# MA-18-4388.

2. Inspected and ops tested EL T min ME406 sin 197-11356 per FAR 91 .207(d). Battery replacement is due 612025. Reinstalled EL T in aircraft and armed. Ops checked good.

3. Installed new 83-5-1 vacuum regulator filter.

4. Inspected and cleaned main fuel filter. Reinstalled using new o-ring pin MS29512-043. No leaks noted.

5. Serviced tires with air: N = 35 psi; M = 38 psi. Serviced brake reservoir and hydraulic power pack reservoir.

6. Installed new right landing gear down lock spring pin 487-495. Installed new left landing gear trunnion pin 67926-040. Reassembled left landing gear using original shock strut with new MS28775-327 ,MS28775-227, MS28775-21 o 0-rings, pin 484-828 seal and pin 187-630 wiper. Serviced with Mil-5606A fluid and air. Installed left gear. Installed new nose landing gear up stop bumper pin 37970-005. Landing gear G:leaned and lubed. Landing gear operation

checked-normal and emergency. Ops checked good.

and Alterations ·tificate Number of 1er specific entries.)

7. Inspected and weighed portable fire extinguisher min RT-A600 sin Y-491182. Weight 1 lb. 9.5 ------oz ..

8. Installed new stabilator trim indicator pin S8488.002. Rigging checked good.

9. Installed new CHT probes pin 2853 sin 25759 in engine cylinder #5, sin 26202 in cylinder #1. Ops checked good.

1 O. Installed new pin 469-600 bonding jumper on left wing flap.

11. Tightened alternator mounting bolt.

12. Serviced aircraft oxygen system to 1850. PSI with aviators breathing oxygen.

13. Cleaned both fuel cap seals.

14. Removed corrosion from both ends of bonding jumper on the right aileron. Removed corrosion from both ends of the right wing flap bonding jumper. Removed corrosion from the right landing gear from around screw head in web for the brake hose clamp. Removed corrosion from the left wheel well. Treated areas with Alumi-prep 225$, primed and touched up paint.

15. Installed right aileron new outboard hinge rib p/n 86398-809. Installed new inboard hinge

ng p/n 86392-003. fit ti

16. Cleaned wing flap gap seals with solvent.

17. Tightened one attach bolt in the left fuel quantity sender. Removed fuel stain. No further lea ks noted. •

18. Tightened stabilator left bearing hardware. No further play noted.

19. Treated area in aft cabin tunnel with Corrosion-X spray.

20. Installed new pilot and copilot FAA-PMA approved manufacturer Premier Aerospace rvices & Technology Inc., replacement trim cover pin H66615-14. Se

21. Complied with aircraft battery capacity test. Concord battery p/n RG-35AXC s/n 40828676 ssed test. Recharged and reinstalled. pa

22. 36

AD 2015-19-07 dated 11/3/15 fuel injector line and clamp inspection next due attach time 76.54 or if fuel lines or clamps are loosened or moved or at engine overhaul.

23. AD 91-21-01 R1 dated 6/27/96 Inspection of the exhaust for cracking or distortion per para (2). Next due attach time 3666.54 (a)

24. AD 2013-12-06 dated 3/11/2013 inspection of the stabilator control system. Next due attach

s and Alteratlons ertificate Number of ther specific entries.)

o3.9 or by 513112020. • --------54

25. AD 2005-12-06 dated 7/19/2005 inspection of magneto impulse coupling. Next due attach 75.69. 39

26. AD 93-05-06 dated 4/29/1993 inspection of the Gerdes ignition switch. Next due attach time 25.13. 39

27. AD 2017-14-04 dated 8/15/2017 inspection of oil cooler hoses does not apply due to hoses n TSO-C53A Type D. p/

YEAR 20 _ DATE

28. Complied with Instructions for Continued Airworthiness for the Aspen Avionics EFD-1000 IAW Aspen Document# 900-00012-001 Revision Y Sections 11 & 12. No defects noted. Internal backup battery passed 30 minute capacity check. Recharged battery.

29. Complied with Instructions for Continued Airworthiness for Garmin GNS-530W IAW Garmin Document pin: 190-00357-65 Revision D dated 11 /20/2014. No defects noted.

30. Complied with ICA for Garmin GDL-69 IAW Document #190-00355-00 Rev F Dated 6/11/2015. No defects noted.

31 . Complied with ICA for Garmin GA-37 Antenna IAW Document# 190-00673-01 Rev F dated 8/27/2007. No defects noted.

32. Complied with ICA for Garmin GTX 330ES transponder IAW document No. 190-00734-11 Rev. 5 dated 10/5/2016. No defects noted.



35. Complied with ICA for LP Aero Plastics inc. For the windshield and windows IAW LP Aero Plastics inc. STC#SA00047NY and STC# SA948NE and STC A7SO ICA Doc dated 8/27/01.

s and Alterations ertificate Number of ther specific entries. \

RECOROllll! TftftAV'" TftTH "'----~-&! --- -· •-- -JACH TIME

Date: 5/1 012019; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Tach: 3622.41

Installed new left and right stabilator hinge bearings pin 452-394, using 2 new bolts pi n 402 -680 and 2 new lock nuts pin MS21042-4. Lubricated bearings with LPS-2 lubricant. Stabilator rigging checked good. No defects noted.


This aircraft, airframe, engine or appliance identified was repaired and inspected in accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-19-4520.

sfi~ Date: 6/06/2019; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Tach: 0.51

1. Lubed external flight controls.

2. Inspected tires and brakes for condition T checked good main= 38 nose= 35. s. ires and brakes are serviceable. Tire pressures

3. Checked external lights, stall warning, and pilot heat. All checked good.

Three Wing Aviation G LLC 4 roup, 00 Great Meadow Rd Stratford, CT 06615

!:~~~:c~:·~~r~~~n/!~~l~~o~:~~~e ldenti~ed.was repaired and inspected In Shop Order MA-19-4544. e FAA and 15 approved for return to service.

·~ ~ 1 date

~ Alterations :e Number of ecific entries.)

YEAR 20 _ DATE

RECORDING YACH TIME

TODAY'S TOTAL FLIGHT TIME IN

SERVICE

Description of Inspections, Tests, Repairs ant Entries must be endorsed with Name, Rating and Certific Technician or Repair Facility. (See back pages for others

Date: 10/07/2019; Aircraft: N8214H; Type: P.A-32R-301T; S/N: 32R-8029093; Tach: 3692.72

1. Serviced tires with air: N = 35 psi; M = 38 psi. Serviced brake reservoir.

2. Ops checked all exterior lights, pilot heat, and stall warning.

3. Checked tires and brakes for wear.

4. Lubed all exterior flight controls, hinges, and rod-ends.

5. Checked and serviced hydraulic power pack with 5606 fluid .


This aircraft, airframe, engine or appliance identified was repaired and inspected in accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-19- 7.

~R

JE

RECORDING TACH TIME


SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number o' Technician or Repair Facility. (See back pages for other specific entries.

Date: 11/27/2019; Aircraft: N8214H; Type: PA-32R-301T; SIN: 32R-8029093; Tach: 3708.20

Removed existing gyro, Edo-Aire Mitchell SOOOE-9 PN: 23-501-05-2 52067 SN: X55386H.

Installed overhauled gyro, , Edo-Aire Mitchell 5000E-9 PN: 23-501-05-2 52067 SN: X55406H, overhauled by Castleberry Instruments CRS# CIYR304X 20, Nov, 2019 WO# W13960.

Replaced central vacuum filter 09-18-1 and regulator filter 83-5-1 with new.

Ran engine and ops checked gyro and autopilot. Ops checked good.

Comply with FAR's 91.411/413 Tests

Tested Aspen EFD-1000 PFD PN: 910-00001-001 SN: 4341 per FAR 43 App E and Aspen Tech Note 2009-09 Rev G dated 2/8/2019 to 30,000 feet. Tested good.

Removed backup altimeter United 5934P-1A.83 SN: OJ447 and tested to 20,000 feet per FAR 43 App E. Tested good and reinstalled.

Tested transpontler Garmin GTX-330ES PN: 011-00455-60 SN: 84134721 (SW 7.04) per FAR 43 App F. Tested good.

Tested Trans-Cal SSD120-30N-RS232 SN: SRN-11972 encoder per FAR 43 App E Para C. Tested good.

Tested static system per FAR 43 App E. Tested good.

-

YEAR 20_ DATE

. RECORDING TACH TIME -

TODAY'S FLIGHT


Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of TP.r.hnir.i"1n rir f:li:::in<>ir i::,,,...i!;n, 'c,..,.. i...AAt. -- -- ~ for other specific entries.

. .


Work Order AV-19-2479.

This aircraft airframe or appliance identified was repaired and inspected in accordance with current regu'lations of

0

the Federal Aviation Administration and is approved for return to service only f o B ed. Repair Station No. SL5R201N.

Date /I /1.1/till1

I I

-15 I .)

RECORDING TACH TIME


SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

Date: 2/18/2020; Aircraft: N8214H; Type: PA-32R-301T; S/N: 32R-8029093; Tach: 3712.83; Total Time: 3712.83

1. I certify that this aircraft has been inspected in accordance with an ANNUAL INSPECTION and current FAA Regulations and was determined to be in an airworthy condition. Time In service since last annual inspection = 130.4 hours. Pertinent details are on file at this facility under Shop Order# MA-20-4758.

2. Inspected and ops tested EL T min ME406 s/n 197-11356 per FAR 91.207(d). Battery replacement is due June 2025. Reinstalled EL T in aircraft and armed. Ops checked good.

3. Installed new 83-5-1 vacuum regulator filter.

4. Inspected and cleaned main fuel filter. Reinstalled using new MS29512-043 0-ring. No leaks noted.

5. Serviced tires with air: N = 35 psi; M = 38 psi. Serviced brake reservoir and hydraulic power pack reservoir.

6. Landing gear cleaned and lubed. Landing gear operation checked-normal and emergency. Ops checked good.

7. Inspected and weighed portable fire extinguisher m/n RT-A600 s/n Y-491182. Weight 706 grams.

8. Repaired induction air filter housing with fiberglass cloth and epoxy resin.

YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alteratlt 20 _ _ TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number

DATE TIME SERVICE Technician or Repair Facility. (See back pages for other specific entri

9. Replaced damaged antichafe tape on engine top cowl as required.

10. Removed surface corrosion from engine cowl right side louver. Treated area with Alumiprep 225S, primed, and touched up paint.

11. Replaced defroster duct and vacuum pump cooling air duct in engine compartment with new Scat #6 duct. Secured as needed. Repositioned cooling shroud for clearance.

12. Installed new pin 100586-008 lock assembly in forward cabin door.

13. Replaced damaged section of engine baffle seal outboard of cylinder No. 1 with new pin 05-04657 seal.

14. Adjusted compressor bypass door magnetic latch for positive closing.

15. Installed new pin 37A19773-367 alternator belt. Set tension and safetied tensioner bolt. Reinstalled propeller IAW AMM Sec. 61-10-00.

16. Installed new pin SW10-96 static wick on left wing flap.

17. Installed new fuel type placard pin 456-682 on left wing near fuel filler.

18. Replace left main tire with new pin 070-317-0 sin 9011 S00046 tire and new tube pin 092-500-0. Torqued wheel half hardware to 150 in lb and inflated to 38 PSI.

19. Reinstalled Oxygen bottle pin 800112-21 sin 24080W after hydrostatic test by Aerospace Turbine Rotables Inc. Serviced to 1850 PSI. No leaks noted. Next test is due by 212025.

I I I

ration RECOROING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations nber of - YACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of entries. TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.) ___,

--_J_ 20. Removed surface corrosion from right aileron attach bracket. Treated area with Alumiprep 2255, primed, and touched up paint.

- --- 21 . Installed new FAA-PMA engine controls placard assembly p/n H69669-44.

- --- 22. Fabricated and installed new .032 aluminum vertical supports for oxygen bottle mounting structure right side forward and left side aft.

- - 23. Tightened and safetied rudder upper hinge bolt. No play noted.

- - --24. Complied with aircraft battery capacity test using BC-7000 battery tester. Concord battery pin - - RG-35AXC s/n 40828676 passed at 98.3%. Recharged and reinstalled.

- - 25. Repaired battery box cover vent nipple with epoxy adhesive.

- 26. Replaced all brake linings with new p/n 066-10500 linings. Conditioned linings.

- 27. Replaced right main tire with new pin 070-31 7-0 sin 2090500133 tire and new tube p/n 092 -500-0. Torqued wheel half hardware to 150 in lb and Inflated to 38 PSI.

-28. Replaced pilots PTT switch p/n 39-1 and wiring from switch to splices in wire bundle.

- · 29. Installed new electric trim switch kit p/n 764-401V. Ops checked good.

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I I I I ~ . . -

= - .

- .... I -

. . - , :t ·~ - -... ~\- --- .. YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alteration.. 20_ TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number a- 1 DATE TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries

8 - -30. Removed parking brake cylinder disassembled and cleaned. Installed new 0-rings pin MS28775-012, MS28775-114, MS28775-113, and new dyna-seal pin 494-062. Reassembled, bench bled, and reinstalled. Brakes ops checked good. , 31 . Installed new cabin heat duct Skeet #12 between heat shroud and control valve housing In engine compartment.

"' 32. Complied with Instructions for Continued Airworthiness for the Aspen Avionics EFD-1000 IAW Aspen Document# 900-00012-001 Revision AA. No defects noted. Installed new internal battery

. pin 409-00003-001 sin 191500050.

33. Complied with Instructions for Continued Airworthiness for Garmin GNS·530W IAW Garmin Document p/n: 190-00357-65 Revision D dated 11/20/2014. No defects noted. "

34. Complied with ICA for Garmin GDL-69 IAW Document #190-00355-00 Rev F Dated 6/11 /2015. No defects noted.

l

35. Complied with ICA for Garmin GA-37 Antenna IAW Document# 190-00673-01 Rev F dated 8/27/2007. No defects noted.

36. Complied with ICA for Garmin GTX 330ES transponder IAW document No. 190-00734-1 1 Rev. 7 dated 09/09/2019. No defects noted. ·'


l

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t

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---

RECORDING JACH TIME


SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)


39. Complied with ICA for LP Aero Plastics inc. For the windshield and windows IAW LP Aero . STC#SA00047NY d STC# SA94BNE d STC A7SO ICA Doc dated 8/27/01 Plastics inc. an an


This aircraft, airframe, engine or appllance identified was repaired and inspected in accordance with current regulations of the FAA and is approved for return to service. Shop Order MA-20-4758.

~ 'Z~ &-1 ~~ ao:J.O Michael T. GavaghanA 3473342 IA date

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