MANTENIMIENTO

ORDEN DE TRABAJO
TaE=Em,f= TMA-MANT-001

15. REM®Vlso 16. INSTALAcO 17. CUMPLIDA 18. ]NspECcloNAne

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Certifieado de Retorno al Servicio de las actividades de EI Trabajo especificado arriba, fie ejeentado de aenerdo con lag
mantenimiento ejecutadas de aouerdo con regu]ad6n ap]icada. regu]aciones ap]icables del RAG, y con respecto a ese trabajo ]a
Aeronave es aprobada para retormar al servicto.
UAEAC TAR TADEMA SA.S. CDF-059

Note: Los Reportes adicionales que se originen en la presente lnspecci6n, se cobraran al precio de horas hombre.

FECHA DE REVIS[6N ANEXO D REVISION PAGINA

30 MAYO 2017 ORbEN DE TRABAJO NO9 1de1

 BASE: BUCARAMANGA FECHA: 2 2/julio/2019
0.T: 19-137, MARCA MODELO SERIF T.T DURG
AVI®N PIPER PA-28R-201T 28R-7703265 2184:58 N/A
MOTOR1 CONTINENTAL TSIO-360-FB 305925 967:53 306:55
HELICE1 HARTZELL BHC-C2YFI a.F AM-3290B 2184:58 243 10

a. ENGINE GF`OUP {PA-28R-201T} -(CONTINENTAL}

Description Technician : Inspector
WARNING

WHEN WORKING ON ENGINE, ENSURE THAT MAGNETO PFRIMARY CIFRCUITS ARE GROUNDED.

NOTE

SEE NOTE 5 AND 18 BEFORE COMPLETING THIS INSPECTION GFROUP.

•.0
1. FRemove to engine cowling.
2. Drain oil sump while engine is sli!l warm
diRE ,-
-1
t-
Lvi:E
3. Change full flow (spin-on type) oil filter element. Thoroughly inspectelementforforeilgnparticles.
'--+fffF£.`. ffidr
4. Inspect oil temperature sender for leaks and security. S .EEF§
` \`_ ,Pz'
5. Inspect oil lines, hoses, and fittings for leaks, security, chafing, dents and
cracks. r'-,. RT¢Sii¥
+yl q 0 '

CAUTION
D0 NOT USE MULTIGRADE OIL UNTIL HARTZELL SERVICE BULLETIN 1428 HAS BEEN COMPuED
IN_ITf..__ ___ _ «_ -
6. FIll engine oil sump with per approved information cowl, or lubrication
chart. (Faefer to section 11). fa,63h! 3) :±.fagr#¢
 MANTENIMIENTO
SERVICIO 50 HORASPA-28R-201T
TMA-028
TEE=Er[EiE FORMATO Not,

FECHA DE REVISION ANEXO D REVISION PAGINA

30 MAYO 2017 SERVICIO DE 50 HORAS 1 2de8
 D. ENGINE GRouP tpA.28Rr2o], . {LycoM,NG,
DesJcription Teichai€ian i I-,2€tor
1. Remove en.gine cowl and inspect for damage.
ayff) \ sNapoo # Wife
t7-_ff'=
2. Drain oil sump while engine is still warm.3.cleanoilsuctionandoilpressurestrainers at oil change; lnspectstrainersforforeignparticles. g*g~O

ii{., E5S z.8

4` Change full flow (cartridge type) oil filter element. Inspect elementthoroughlyforforeignpartic!es`
•-:;I.;-+-:-I:== t \
a
5. Inspect oil temperature sender unit for leaks and security.
6. Inspect oil lines, hoses, and fittings for leaks, security, chafing, dents, andcracks.
REJRE=
'Q,_,A
fldiin
7. Clean and Inspect oil radiator cooling fins. Verify that there is no radiator
damage. :,}F,.a`i;``.=`^_I •,ii
fiijHi-5!--
8. Fill engine with oil per lu'brication chart in Section 1!. TT?q_.RE i.Lfiriixpr=
`'J[[[[[[[[-EREE-'4ffi*

CAUTION

|jjj§§iTN%%LLE#B'gAGPEANLE`8E'E*?NEGCs?UT'°NN°TT°C°NTAM!NATEVACUUMPUMP(#rfe¥lTHz8tBke\
_±d]' r `9
9. Clean engine.
10.Inspect condition Of spark plugs (clean and adjust as required). (Refer tolatestrevisionofLycomingserviceInstruction142).
` `,..ai.qER EJ FREi§=
tJfty . §.

C+_I,NOTE`if¥5i,ag

lffouling of spark plugs are apparent, rotate bottom plugs to upperplugs, and viceve=. fr i ~

11. Inspect spark plug harness leads and ceramics for corrosion and deposits J:.i @¥SiRTty
i;5i:i`-g*:*
12.Inspect rcoker box covers for evidence df oil leaks. If found, replace
gasket(s)a Torque cover screws 50 inch pounds. -,,i,ill ERE!
ELffiffiE¢
13.Inspect ignition harness and insulators. (High tension leakage and
continufty t\e§ts. ) •:,t!. =-`-I:
M!ffi,,¥
14.Remove air filter and tap gently to remove foreign dirt particles (replaceifrequired).

15.clean fuel injector inlet line screen. (See Note 30).

rHFTii
'us+Jf i
tlh®if%Z5Th
er-, ,9A5^, cezfflffg' i
16. Inspeqt condition ``Of injeictor, altemate air door and box. (See Note 7.)
A(g#'
17. Inspect vent lines for evidence of fuel or oil seepage #vy= „r_gr- I

18a Inspect intake seals for leaks and for tight clamps.
19. Inspect all air inlet duct hoses (replace as required).
Arid__qgse;I %',.a
-'`I Jrf€ I
i
20.Clean gascolator bowl and screens. r.Ri*±
_?tnyAAITRE
.€r.E
21. inspect fuel system for leaks. erG _ -a:

22.Inspect exhaust stacks, cQnneStions, and gaskets (replace gaskets as

required) =ix:I `=5B--= \
23.Inspect muffler system„ heat-`€kchange, and baffles. (Refer to latest
revision Of Piper Service Bulletin 691.) i,-:-S-a 'c`S`i`-
24.Check fluid in brake reservoir (fill as required).
rfu#|g¥J `.¥-S````
%ELi
25.Install engine cowling.
-i ® i-i
I:;I ds
FECHA DE REVISION I ANEXO D I REVISION I PAGINA
30 MAY0 2017 I SERVICIO DE 50 HORAS 1 3de8
 MANTENLMIENTO
c SERVIC10 50 HORASPA-28R-201T
Tf=E==l'-:i,a TMA-028
FORMATO Not.

E. CABIN AND COCKPIT GROUP.

Description Tecn2E|cian tryspector
1. Inspect cabin entrance door and windows for damage9 operation, and rf, . `,.id,,

security
2. Check landing, navigation, cabin, and instrument lights
3. Cycle each cireuit br`eakerwith airplane power off. .
REFEE"
.``.`u`. , -` ^?€- `¥
ERE,{FH
•`%.,S+_

_____ _ _ %`.se!!IImRI
F, FUSELAGE AND EMPENNAGE GROUP. +~ ` +
escription Technician i lrspectot
1. Inspect battery, box, and cables for corrosion, damage, frayed cables, Jr--i
and loose terminals. Refer to paragraph 11 rfe9 or ben instructions.
2. Check hydraulic pump fluid level {service as required). e#gr_ "8.
3. Inspect for obstructions and contamination jn inlet Of backup landing gear
extend?r actuator inlet head (if applicable)® (See Note 19.} I,,%RE-<fri
4. Inspect refrigerant charge in sight gauge of receiverLdehydrator. (Refer
to Section XIV.) RECREE`'
5. Inspect air conditiciner condenser air scoop rigging
#nd sets
a;a |2_ arf3.f
`.q9q
6. Lubricate per lubrication chart in Section 11. z:.Jl.`rlv.I
rTKg.i)
G. VVING GROUP. -+ ,-
Description Technician
1. Inspect exterior surfaces, skins, and tips for damage ancl loose or missing GSa'`1

fasteners, and condition of walk-way, as applicable. \S.

2. Lubricate per !ubrieation chart in Section 11.
EL#:REEREl ffffi¥
t55#J +' ``ct`...., Ft
H. LANDINGGEARGR UP. +
Description
1. Cheek olee struts for proper extension and evidence of fluid leakage,
2, See Landin Gears Section 1!
3. Check tire pressure. (Referto Section 11.) I;.Ref-
Ail-`rREJ
4. Inspect brake linings and discs for condition and wear.
i-F]REE§EgEL ELffffi g '--
v¢iffiffife
fi aevty a.,ITseed
5. Inspect nose gear downlock hoc}k for Condition.
6. Lubricate per lubrication chart in Section 11.
yatY© ¢'ffff

I. SPECIALINSPECTION.
escription ec nician lpepeetor
1. See Paragraph "3-8. Special !nspections'' A. Requirements. Perform all
special insp,ections app]i;cable to your aireraft and currently due per the
given Inspection interval.
 MANTEN[MIENTO
SERV]CIO 50 HORASPA-28R-201T
TMA-028
TF=E=Erh,a=F©6:®f=deB`4cBFr*©f"7"l®fl9®Aea-Grfearflee=®
FORMATO N°|0

J. OPERATIONAL INSPECTION.
Description Tecrmician ; Inspector
3. Check oil pressure and temperature indications
1frj:+I
#,, _c``c
#ffffz%
u . TF\ - i
4. Check altemator performance
5. Check manifold pressure indications L/ •,( ¢o.

6. Check altemate air operation o a;`

S. ffrgi
- ,-|/fJRE;RE~
7. Check parking brake operation
LELffi!'=i:5HH
8. Check engine driven vacuum gauge indication
:`-ffiffREf
.:i .:`
9. Check gyros for noise and roughness
';ff3ffi `1`<s§..%`
10.Check cabin heater operation rty i`,
/
11.Check magneto switches operation •.I(.:Bfc+i
0,
(,,` - iif :`3r-?
12.Check each magneto RPM variation; drop, etc.
13.Check throttle and mckture operation I `ltt'ts±€
14.Check propeller operation and smoothness 8REffiRTREV
V/ ``.-±
15.Check propeller governor operation and reaction
Bffi:*iRE I #FBS_eso_a
16.Check engine idle operation
17.Check electronic equipment operation
•,,
ffl-`
VffiifRfffif#
_CJ
18.Check automatic pitch trim, and manual/electric trim operation.
7f5i'l,
(See Note 16.) tlRT€'--`

19.Check air conditioner compressor clutch operation .I ` .- . .. _irr\ {|{`ir3.S33Sti.!.`

20.Check air conditioner condenser Scoop operation rr qI,I+
I.
21.Check landing gear system. (See Note 12.)
J| Bjz€:igE
22.After shutdowng check auxiliary electric driven vacuum gauge indication
in I.` `e;
L/ |LJt ,Ou.T
K. GENEFRA,L
Description Tee a,nician i ,• .s. .(eetor
1. Aireraft conforms to FAA Specifications
.j!|fl.;` t- ,
2. Latest revision of applicable FAA Airworthiness Directives complied with
(a
T`
3. Current and correct Pilot's Operating Handbook (POH) is in the airplane I+'
4.In spect airplane for required placards as identified in Section 2 of the
POH
_-.:ffl_ffAJ_I.i ![;,yg=\/i,
5. Appropriate entrl-es made in the Aircraft and Engine Log books
PELfiJi,,--
6.Ad rworthiness & Registration Certificates in the aircraft ancl properly ay/ ,A
splayed
®a

-
7.A reraft Equipment List, Weight and Balance and FAA Form(s) 337 (if TL1`/,B
a pplieable) are jn the aircraft and in proper order
8. Operational inspection and run-up completed
9.A ireraft cleaned and lubricated after wash (as required)
DE:e
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/
Liti.a,-£`
5
flwTiAiae.. i lw` `.
i .-

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FECHA DE REVISION ANEXO D REVISION PAGINA

30 MAYO 2017 SERVICIO DE 50 HORAS 1 5de8
 )TF=E=E I.-n.F= MANTENIMIENTO
SERVIC[0 50 HORASPA-28R-201T
TMA-028
FORMATO N°|o

NOTES:

1. Refer to Pipers Customer Service Information File P/N 1753-755 for latest revision dates to Piper
!nsp.ection F3eports"anuals and this service manual. References to section, paragraph, figure, or
table are to the appropriate section, paragraph, figure, or table in this manual.

WARNING: INSTFaucTIONS FOR CONTINUED AIRWORTHINESS (lcA) FOR ALL NON-PIPEFa

APPFROvED STC INSTALLATIONS ARE NOT INCLUDED IN THIS MANUAL. WHEN A NON-PIPER
APPRovED STC INSTALLATloN IS iNcoRpoFaATED oN THE AiRPLANE, THoSE PORTIONS oF THE
AIRPLANE AFFECTED BY THE INSTALLATION MUST BE INSPECTED IN ACCORDANCE WITH THE
ICA PUBLISHED BY THE OWNER OF THE STC. SINCE NONnpIPEF3 APPROVED STC INSTALLATIONS
MAY CHANGE SYSTEMS INTEFRFACE, OPEFRATING CHARACTERISTICS AND COMPONENT LOADS
OR STRESSES 0N ADJACENT STRUCTURES, THE PIPER PROVIDED ICA MAY NOT BE VALID FOR
AIRPLANES SO MODIFIED.

2. !nspeetions or operations are to be performed as indicated by a "0" at the 50 or 100 hour inspection
interval. Inspections or operations (i.e. -component overhauls/replacements, etc.) required outside
the 50 / 100 hour eycle are listed as speicial inspections in Paragraph 3no. Inspections must be
accomplished by persons authon.zed by the FAA or appropriate National Aviation Authority. Checks
may be accomplished by a pilot who is qualified on the airplane.
(a) The 50 hour inspection accomplishes preventive maintenance8 lubrication and servieing as
well as inspecting critical components.
(b) The 100 hour inspection is a complete inspection of the airplane, identiJcal to an annual
inspection.

E!Q|E: A LOG BOOK ENTRY SHOULD BE MADE UPON COMPLETION OF ANY INSPECTIONS®

3. Piperservice Bulletins are Of special importance and Piperconsiders compliance mandatory. In all
cases3 s,ee Service Buj!etin/Service Letter Index P/N 762-332 to verify latest revision. See also
paragraph 3-9.
4® Piper Serviice Letters are product improvements an'd service hints p.ertaining to serviicing the
airplane and should be given careful attention.
5. Inspe`ctions given for the pewer plant are based on the engine manufacturer's operators manual
{Continental Part No. X-30583) or (Lycoming Part No. 60297-12) for this airplane. Any changes
issued to the engine manufacturers operat®r's manual supersede or supplement the insp`ections
Outlined in this report. Should fuel otherthan the specified octane rating for the power plant be usejdg
refer to the latest revision of Lycoming Service Letter No. L185 for additional information and
recommended service procedures.
6. Faeplace as required or at engine overhaul. (Refer to latest revision of Hartzell Service Letter 61.)
For engine ovemaul, refer to latest revision of one of the following: Lycoming Service Instructions
No.1009, for recemmendecl engine oveinaul period, or TOM SIL-98-9A, for recomm`ended engine
Overhaul period. a.
7. Check throttle body attaching screws for tightness; the correct torque for these screws is 40 to 50
inch pounds.
8. Rotate spark plugs from upper to lower positions and vice-versa {o lengthen plug service life.
9. Check cylinders for evidence of excessive heat which is indicated by burnt paint ®n the cylinders.
This condition is indicative Of intemal damage to eylinder(s) and, if found, its cause must be
determined and corrected before the aireraft is returned to service. Heavy discoleratien and
appearance Of seepage at ther'eyljnder head barrel attachment area is usually due to emission of
thread !uE)riGant used during asschb!y of the barrel at the factory, or by slight gas leakage which
stops after the cylinder has been in `service for a while. This condition is neither harmful nor
detrimental to engine perfermanc6 anc3 operation. If it can be proven that leakage exceeds these
conditionsS the cylinder must be replaced.
FECHA DE REVISION ANEXO D REVISION PAGINA
30 MAYO 2017 SERVICIO DE 50 HORAS 1 6de8 I
 MANTENIMIENTO
SERVICIO 50 HORASPA-28R-201T
TF=E==[||E TMA-028
FORMATO N°|o

10. If the altimeter is damaged, defective or inaccurate, work must be done by an FAA ap,proved
instrument repair facility only. A logbook entry must be made.
11. The compressor oil level should not be checked unless the system has been opened, or a refr.Igerant
leak occurred which requires an addition of refrigerant to the system.
12. Aireraft must be flown to check the landing gear system in accordance with instructions outlined in
Section Vl, ®f the Servi'ce Manual. (Faefer to latest revision of Piper Service Bulletin 810).
13. F®r operation above 12,00'0 feet8 more frequent.ignition system maintenance is required® (Refer to
latest revision of Continental Servilce Bulletin M78-8).
14® Faefer to latest revision of Piper Service Bulletin 578.
15. Inspect brushes every 100 hours if used for training or every 500 hours if used for normal service.
(Refer to latest vendor servi,ce publications.)
16. Refer to flight manual supplement for preflight and flight checkB for intended function in all modes.
17. Refer to latest revision of TOM Service Bulletin 6438 for inspection of magneto and ignite
harnesses.
18. Refer to latest revision TOM Critical Service Bulletin CS896-13.
19. Refer to latest revision of Piper Service Bulletin 866A. Aireraft S/N's 2837001 (PA-28R-201) and
up8 and S/N's 2803001 (PA-28R-201T) and up, have no backup extender system in the landing
gear system installed as standard equipment.
20. Ensure after cleaning engine that all rod end bearings are lubricated with at least 3 drops of 100W
motor Oil.
21. Refer to latest revision Of Piper Service Bulletin 856.
22. Inspect Teflon bushing (tower to upper cowling attachment) for condition at each 100 hours.
Replace bushing on condition, but no later than 500 hours time in service. Inspect pin for condition
and rep!.ace as necessary`
23. If not already installed, add access panels per instructions in Section lv, Paragraph 4-55a. F3efer to
the latest revision of Piper Service Bulletin 977.
24. Special care should be taken to inspect stabi!ator control cables beneath aft baggage compartment
floor. Add access panels per instructions in Section !V9 Paragraph 4-55a, to ease this inspection.
25. SIoshing ®f fuel tanks not approved. For airplanes with fuel tanks which have previously bieen
s!oshedo perform Sloshed Fuel Tank 100 Hour Inspection Paragraph 9J5a.
26. Inspection of hydraulic pump brushes applies only to Prestolite pumps. When the brushes wear out,
replace pump with a new Oil dyne pump - replacement brushes are no longer availak)le.
27. Verify initial compliance with Piper Service Bulletin No. 886A.
28. In S/N's 28Fa-7737002 thru 28FR-7837317 and 28FR-7703001 thru 28FR-7803374, which have not
installed Piper Kits No. 767-397 €LH) and 767-398 (RH) per Piper Service Bulletin No.1161 a conduct
the 100 hour inspection under Special Inspections, Procedures, Wing Rib Assembly W.S. 49.25
Inspections.
29. Use of magneto manufacturer publications is recommended:
€a) For airplanes equipped with TCM/Bendix Magnetos: inspect magnets(s) perthe procedures
in the Periodic Maintenance section of the applicable Service Support Manual, available
from Teledyne Continental Motors, lnc„ PH: (Solo) 718-3411, or http://www.tgrnl_ink_._CLQm±:
(b) For airplanes equipped with slick Magnetos: inspect magneto(s) per the appropriate 100
Hour Inspection in the Slick F110'O Master Service Manual, available from Unison
. Industries, PH: (904) 7394000, or http://www.unisonindustries.com/.
30. At the first 100-hour inspection on new, rebuilt or overhauled engines, remove fuel injection nozzles.
Clean ,nozzles by soaking in lacquer thinner, acetone ®r methy! ethyl ketone (MEK).
31. Forairplanes equipped with Parker Hannifin / Airborne vacuum pump(s), verify compliance with
• Parker Hannifin / Airborne Service Letter No. 72.
32. For gi.pelgnes with rudder pedal assemblies which have accumulated 1,200 hours or more time in
serv!cg,: Inspect per Piper Service Bulletin 1242 or latest revision.
..

FECHA DE REVISION ANEXO D REVISION PAGINA

30 MAY0 2017 a SERVICIO DE 50 HORAS 1 7de8
 MANTENIMIENTO
SERVICIO 50 HORASPA-28R-201T
TEB=lilE TMA-028
FORMATO Not,

Se certifica que esfa a,eronave ha sido inspeccionada de acuerdo al MP[ DEL TAR-TADEMA S.A.S. CDF059
aprobacl® per la UAEAC y de acuerdo al manual de mantenimiento PIPER PA-28-201T P/N 761rfe39 revisi6n
ENEFRO 15 de 2016 per servicio de 50 horas, de acuerdo con lo establecido en el programa de mantenimiento
y se ha encontrado en condiciones de aeronavegabilidad.

a ®3® @ a ©_

I.¢ - i -. , . -.`- - 2 -`.' I ,,

Personal Tdrnico
T6cni,co LICENCIA #++ Flun i`\
A,.13+

Ibe`-,.'` i`,`+\clc`.,( . 7zpz5Bzffiffi

`:- .`':.`.-` `=-..``` ?.`, -``.``
fro ®Egr ® -/fif lf enFf;R§oEa§
Vc-
if
Por lo tanto se libera al servicjo como aeronave Aeronavegable.

#rmaAIT hic\emcia N9 Fecha

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)ctavio 8arcta -=:i./::,.-:--._-`-):,I, `
AIT1952/CDF.059
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ESPACIO DEJADO EN BLANCO

FECHA DE REVISION ANEXO D REVISION PAGINA

30 MAYO 2017 SERVICIO DE 50 HORAS 1 8de8