Documentação PT-KLM

ZAP AVIAÇÃO
CNPJ: 36.130.998/0001-96 		AERONAVE:
FABRICANTE:TEXTRONTSN:10261.5H
Rua da Prainha, n° 3320, Bairro Morada Nobre
Barreiras/BA, Brasil, CEP 47.810-047		MODELO:152
COM 3003-03/ANACS/N:152800628
Data de Emissão:2022-07-12 00:00:00
MOTOR
POSFABRICANTEMODELOS/NTSNMODELOS/NTSNCSNTSOTSLI
1LYCOMINGO-235-L2CL-19572-155311.572CKS6-0-54K67253425.2N/A1357.450.7
SUPPLEMENTAL INSPECTION DOCUMENTS - SID - D2064: Revision - 1, Revision Date - Oct 2, 1995
DADOS DO SERVIÇODADOS DA EXECUÇÃO
ULTIMO SERVIÇOPRÓXIMO SERVIÇO
OPERATIONSIDDESCRIÇÃOINTERVALOTIPO / SERVIÇOREFERÊNCIATSN/CSN/DATAREGISTRO/OBSVENCIMENTODISPONÍVELSTATUS
1N/AInspect aircraft records to verify that all applicable
Cessna Service information Letters, Cessna Service
Bulletins and Supplier Service Bulletins are complied
with; 		100HINSPEÇÃO10261.5HCad.001/PRKLK/14.ág.04910361.5H100HOK
--OK
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
Inspect aircraft records to verify that all applicable
Airworthiness Directives and Federal Aviation
regulations are complied with;		100HINSPEÇÃO10261.5HCad.001/PRKLK/14.ág.04910361.5H100HOK
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
Inspect aircraft records to verify that all applicable
Airworthiness Directives and Federal Aviation
regulations are complied with.		100HINSPEÇÃO10261.5HCad.001/PRKLK/14.ág.04910361.5H100HOK
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
Inspect aircraft records to verify that all SID
Inspections have been complied with as scheduled.		100HINSPEÇÃO10261.5HCad.001/PRKLK/14.ág.04910361.5H100HOK
C--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
57-53-01This interval is for mild/moderate corrosion
environment. Inspect flap tracks for corrosion.
Refer to Section 2A-14-20, Supplemental Inspection
Document 57-53-01, for inspection procedure.		INSPEÇÃO INICIAL2A-14-20--
-C-
240MD-D-DOK
INSPEÇÃO REPETITIVACad.001/PRKLK/14 Pág.033--
--
120M2018-10-09 00:00:00D2028-10-10 00:00:00D2282DOK
2Wing structure internal. Make sure you inspect these
areas: 1. Main spar upper and lower carry-thru fittings,
2. Main spar upper and lower caps, 3. Main spar web.
NOTE: Corrosion Prevention and Control Program
Inspection item (baseline interval, refer to Section
2A-30-00 for additional inspection information).		INSPEÇÃOCad.001/PRKLK/14 Pág.033--
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
3Aileron attachments. Make sure you inspect these
areas: 1. Aileron hinges, 2. Hinge bolts, 3. Hinge
bearings, 4. Hinge and pushrod support structure.
NOTE: Corrosion Prevention and Control Inspection
Item (baseline interval, refer to Section 2A-30-00
for additional inspection information). NOTE: Do
not apply LPS-3 Heavy Duty Rust Inhibitor on hinge
bearing.		INSPEÇÃOCad.001/PRKLK/14 Pág.033
-
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
4N/AMain landing gear axle assembly. Make sure you
inspect these areas: 1. Main gear axle and attach
bolts. 2. Wheel halves. NOTE: Corrosion Prevention
and Control Program Inspection item (baseline
interval, refer to Section 2A-30-00 for additional
inspection information). NOTE: Do not apply LPS-3
Heavy-Duty Rust Inhibitor to the bearing. NOTE:
Coordinate with tire change.		INSPEÇÃOCad.001/PRKLK/14 Pág.045--
--
36M2020-11-17 00:00:00D2023-11-18 04:48:00D494.2DOK
Nose gear trunnion, steering assembly, torque link
assembly, nose gear fork and axle. Make sure you
inspect these areas: 1. Nose gear trunnion surface.
2. Steering collar and steering collar attach bolt. 3.
Torque link, torque link attach pin, and attach bolt. 4.
Nose gear fork. 5. Nose gear axle. NOTE: Corrosion
Prevention and Control Inspection Item (baseline
interval, refer to Section 2A-30-00 for additional
inspection information).		INSPEÇÃOCad.001/PRKLK/14 Pág.045--
--
36M2020-11-17 00:00:00D2023-11-18 04:48:00D494.2DOK
4Nose landing gear outer barrel assembly. Make sure
you inspect these areas: 1. Outer barrel assembly. 2.
Upper strut end and lower collar assembly. NOTE:
Corrosion Prevention and Control Inspection Item
(baseline interval, refer to Section 2A-30-00 for
additional inspection information). NOTE: do not
apply LPS-3 Heavy-Duty Rust Inhibitor to the sliding
surfaces of the oleo strut.		INSPEÇÃOCad.001/PRKLK/14 Pág.028
-
36M2020-11-17 00:00:00D2023-11-18 04:48:00D494.2DOK
5Passenger/Crew door retention system. Make sure
you inspect these areas: 1. Bell cranks. 2. Pushrods.
3. Handle. 4. Pin retention. 5. Pins. 6. Lockplates
and guides. 7. Hinges. 8. Internal door framing.
NOTE: Corrosion Prevention and Control Program
Inspection item (baseline interval, refer to Section
2A-30-00 for additional inspection information). Note:
Remove interior panels for access.		INSPEÇÃO
-
48M2020-11-07 00:00:00D2024-11-07 14:24:00D849.6DOK
Areas of the cabin structure for the passenger/crew
door. Make sure you inspect these areas: 1. Door
frames. 2. Door hinges. NOTE: Corrosion Prevention
and Control Program Inspection item (baseline
interval, refer to Section 2A-30-00 for additional
inspection information).		INSPEÇÃOCad.001/PRKLK/14 Pág.028
-
48M2020-11-07 00:00:00D2024-11-07 14:24:00D849.6DOK
6Fuselage lower internal structure beneath the floor
panels. Make sure you inspect these areas: 1.
Cabin structure under floorboards. NOTE: Corrosion
Prevention and Control Program Inspection item
(baseline interval, refer to Section 2A-30-00 for
additional inspection information).		60Cad.001/PRKLK/14 Pág.028
C
M2017-10-06 00:00:00D2022-10-07 00:00:00D87DOK
Fuselage internal structure in upper fuselage. Make
sure you inspect these areas: 1. Cabin bulkhead
corners. 2. Fuselage skin. NOTE: Corrosion
Prevention and Control Program Inspection item
(baseline interval, refer to Section 2A-30-00 for
additional inspection information).		60Cad.001/PRKLK/14 Pág.028
C
M2017-10-06 00:00:00D2022-10-07 00:00:00D87DOK
Areas of the cabin structure. Make sure you inspect
these areas: 1. Firewall. 2. Firewall attachments.
NOTE: Corrosion Prevention and Control Program
Inspection item (baseline interval, refer to Section
2A-30-00 for additional inspection information).		60Cad.001/PRKLK/14 Pág.028
C
M2017-10-06 00:00:00D2022-10-07 00:00:00D87DOK
6Areas of the cabin structure. Make sure you inspect
these areas: 1. Cabin door forward and aft frames.
2. Window frames with emphasis at stringers and
channel assemblies from aft of door frame to aft
bulkhead. 3. Seat attachment structure. 4. Aft
Cabin Bulkhead. NOTE: Corrosion Prevention and
Control Program Inspection item (baseline interval,
refer to Section 2A-30-00 for additional inspection
information).		60Cad.001/PRKLK/14 Pág.028
C
M2017-10-06 00:00:00D2022-10-07 00:00:00D87DOK
6Wing structure internal. Make sure you inspect these
areas: 1. Wing front spar and lower spar caps.
2. Upper and lower wing attach spar fittings. 3.
Wing lower skins. NOTE: Corrosion Prevention and
Control Program Inspection item (baseline interval,
refer to Section 2A-30-00 for additional inspection
information).		INSPEÇÃOCad.001/PRKLK/14 Pág.028--
--
60M2017-10-06 00:00:00D2022-10-07 00:00:00D87DOK
Wing structure external. Make sure you inspect these
areas: 1. Skin with emphasis at skin overlaps and
under access panels. 2. Rear spar upper and lower
caps. 3. Rear spar web. NOTE: Corrosion Prevention
and Control Program Inspection item (baseline
interval, refer to Section 2A-30-00 for additional
inspection information).		INSPEÇÃOCad.001/PRKLK/14 Pág.028--
--
60M2017-10-06 00:00:00D2022-10-07 00:00:00D87DOK
727-20-01Wing structure internal. Make sure you inspect these
areas: 1. Main spar upper and lower carry-thru fittings,
2. Main spar upper and lower caps, 3. Main spar web.
NOTE: Corrosion Prevention and Control Program
Inspection item (baseline interval, refer to Section
2A-30-00 for additional inspection information).		10000HINSPEÇÃO INICIAL9402.3HCad.001/PRKLK/14 Pág.03319402.39140.8
--
240M2018-10-09 00:00:00D2038-10-12 00:00:00D5936DOK
3000HINSPEÇÃO REPETITIVA9402.3HCad.001/PRKLK/14 Pág.03312402.32140.8
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
55-30-01Inspect vertical stabilizer and rudder, including spars,
ribs, hinge bolts, hinge bearings and attach fittings.
Refer to Section 2A-14-12, Supplemental Inspection
Document 55-30-01, for inspectionVisual, Borescope and Eddy Current if needed. procedure.		10000HINSPEÇÃO INICIAL9402.3HCad.001/PRKLK/14 Pág.03319402.39140.8
--
240M2018-10-09 00:00:00D2038-10-12 00:00:00D5936DOK
3000HINSPEÇÃO REPETITIVA9402.3HCad.001/PRKLK/14 Pág.03312402.32140.8
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
832-20-01IInspect nose landing gear torque links, bolts, bushings
and fork. Refer to Section 2A-14-05, Supplemental
Inspection Document 32-20-01, for inspection
procedure.		3000HINSPEÇÃO INICIAL9402.3HCad.001/PRKLK/14 Pág.03312402.32140.8
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
3000HINSPEÇÃO REPETITIVA9402.3HCad.001/PRKLK/14 Pág.03312402.32140.8
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
9 57-53-01This interval is for mild/moderate corrosion
environment. Inspect flap tracks for corrosion.
Refer to Section 2A-14-20, Supplemental Inspection
Document 57-53-01, for inspection procedure.		3000HINSPEÇÃO INICIAL--
--
120MD-D-DOK
500HINSPEÇÃO REPETITIVA10007.3HCad.001/PRKLK/14 Pág.04510507.3245.8
--
60M2020-11-17 00:00:00D2025-11-18 00:00:00D1225DOK
1071-20-01Inspect tubular engine mount. Refer to Section
2A-14-21, Supplemental Inspection Document
71-20-01, for inspection procedure. 		2400HINSPEÇÃO INICIAL9402.3H11802.31540.8
--
2018-10-09 00:00:00D-D-DOK
3000HINSPEÇÃO REPETITIVA NO OVERHAUL DO MOTOR9402.3HCad.001/PRKLK/14 Pág.03312402.32140.8
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
1132-13-01This inspection is for mild/moderate corrosion
environment. Inspect main landing gear tubular
spring for rust or damage to finish. Inspect entry step
attachment. Refer to Section 2A-14-03, Supplemental
Inspection Document 32-13-01, for inspection
procedure.		INSPEÇÃO INICIAL--
--
240MD-D-DOK
INSPEÇÃO REPETITIVACad.001/PRKLK/14 Pág.021--
--
120M2014-04-23 00:00:00D2024-04-24 00:00:00D652DOK
53-11-01This inspection is for mild/moderate corrosion
environment. Inspect carry-thru spar area, wing
attach fittings, spar channel and lugs. Refer to Section
2A-14-06, Supplemental Inspection Document
53-11-01, for inspection procedure.		INSPEÇÃO INICIAL--
--
240MD-D-DOK
INSPEÇÃO REPETITIVACad.001/PRKLK/14 Pág.033--
--
120M2018-10-09 00:00:00D2028-10-10 00:00:00D2282DOK
53-30-01This interval is for mild/moderate corrosion
environment. Inspect the cabin interior skin panels,
frames and stringers. Refer to Section 2A-14-07,
Supplemental Inspection Document 53-30-01, for
inspection procedure.		INSPEÇÃO INICIALH--
--
240MD-D-DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
120M2018-10-09 00:00:00D2028-10-10 00:00:00D2282DOK
57-11-02This interval is for mild/moderate corrosion
environment. Inspect wing for corrosion and missing
or loose fasteners. Refer to Section 2A-14-15,
Supplemental Inspection Document 57-11-02, for
inspection procedure.		INSPEÇÃO INICIAL--
--
240MD-D-DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
120M2018-10-09 00:00:00D2028-10-10 00:00:00D2282DOK
57-11-03This interval is for mild/moderate usage environment.
Inspect wing splice joint at strut attach. Refer to
Section 2A-14-16, Supplemental Inspection Document
57-11-03, for inspection procedure.		INSPEÇÃO INICIAL--
--
240MD-D-DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.021--
--
120M2014-04-23 00:00:00D2024-04-24 00:00:00D652DOK
1257-12-01This interval is for mild/moderate corrosion
environment. Inspect wing root rib. Refer to Section
2A-14-17, Supplemental Inspection Document
57-12-01, for inspection procedure.		INSPEÇÃO INICIAL--
--
60MD-D-DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
13 32-13-01This interval is for severe corrosion environment.
Inspect main landing gear tubular spring for rust or
damage to finish. Inspect entry step attachment.
Refer to Section 2A-14-03, Supplemental Inspection
Document 32-13-01, for inspection procedure.		INSPEÇÃO INICIALHCad.001/PRKLK/14 Pág.033--
--
120M2014-04-23 00:00:00D2024-04-24 00:00:00D652DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.021--
--
60MD-D-DOK
53-11-01This interval is for severe corrosion environment.
Inspect carry-thru spar area, wing attach fittings,
spar channel and lugs. Refer to Section 2A-14-06,
Supplemental Inspection Document 53-11-01, for
inspection procedure.		INSPEÇÃO INICIALCad.001/PRKLK/14 Pág.033--
--
120M2018-10-09 00:00:00D2028-10-10 00:00:00D2282DOK
HINSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
1353-30-01This interval is for severe corrosion environment.
Inspect the cabin interior skin panels, frames and
stringers. Refer to Section 2A-14-07, Supplemental
Inspection Document 53-30-01, for inspection
procedure.		HINSPEÇÃO INICIALHCad.001/PRKLK/14 Pág.033--
--
120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
INSPEÇÃO REPETITIVAH--
--
60MD-D-DOK
1357-11-02This interval is for severe corrosion environment.
Inspect wing for corrosion and missing or loose
fasteners. Refer to Section 2A-14-15, Supplemental
Inspection Document 57-11-02, for inspection
procedure.		INSPEÇÃO INICIALH--
--
120MD-D-DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
57-11-03This interval is for severe usage environment. Inspect
wing splice joint at strut attach. Refer to Section
2A-14-16, Supplemental Inspection Document
57-11-03, for inspection procedure.		HINSPEÇÃO INICIALHCad.001/PRKLK/14 Pág.021--
--
120M2014-04-23 00:00:00D2024-04-24 00:00:00D652DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
60M2018-10-09 00:00:00D2023-10-10 00:00:00D455DOK
1357-53-01This interval is for severe corrosion environment.
Inspect flap tracks for corrosion. Refer to Section
2A-14-20, Supplemental Inspection Document
57-53-01, for inspection procedure.		INSPEÇÃO INICIAL--
--
120MD-D-DOK
HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.033--
--
60M2022-05-30 00:00:00D2027-05-31 00:00:00D1784DOK
1427-30-01Elevator trim system. 1. Inspect elevator trim brackets
and actuator support brackets. 2. Inspect pulleys,
attaching structure and fasteners. Refer to Section
2A-14-02, Supplemental Inspection Document
27-30-01, for inspection procedures.		1000HINSPEÇÃO INICIAL--
--
D-D-DOK
1000HINSPEÇÃO REPETITIVA9402.3HCad.001/PRKLK/14 Pág.03310402.3140.8
--
D-D-DOK
1532-13-02Inspect main landing gear fittings and attachment
of the fittings to the bulkheads. Refer to Section
2A-14-04, Supplemental Inspection Document
32-13-02, for inspection procedure.		3000HINSPEÇÃO INICIAL--
--
60MD-D-DOK
1000HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03311261.51000
--
60M2022-05-30 00:00:00D2027-05-31 00:00:00D1784DOK
16 53-47-01This interval is for mild/moderate corrosion
environment. Inspect seat rails for corrosion. Refer
to Section 2A-14-08, Supplemental Inspection
Document 53-47-01, for inspection procedure.		INSPEÇÃO INICIAL--
--
120MD-D-DOK
INSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
1753-47-01This interval is for severe corrosion environment.
Inspect seat rails for corrosion. Refer to Section
2A-14-08, Supplemental Inspection Document
53-47-01, for inspection procedure.		INSPEÇÃO INICIAL--
--
120MD-D-DOK
INSPEÇÃO REPETITIVAH--
--
120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
1857-11-01This interval is for typical usage environment. 1.
Inspect inboard wing structure and wing attachment
to fuselage including working rivets. 2. Inspect flap
actuator support structure. Refer to Section 2A-14-14,
Supplemental Inspection Document 57-11-01, for
inspection procedure.		12000HINSPEÇÃO INICIAL--
--
120MD-D-DOK
2000HINSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
19 57-11-01This interval is for typical usage environment. 1.
Inspect inboard wing structure and wing attachment
to fuselage including working rivets. 2. Inspect flap
actuator support structure. Refer to Section 2A-14-14,
Supplemental Inspection Document 57-11-01, for
inspection procedure.		6000HINSPEÇÃO INICIAL12000H180007738.5
--
120MD-D-DOK
1000INSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03311261.51000
--
60M2022-05-30 00:00:00D2027-05-31 00:00:00D1784DOK
2055-10-01Inspect horizontal stabilizer and elevator, including
torque tube, spars, ribs, hinge bolts, hinge bearings,
brackets and attach fittings. Refer to Section
2A-14-09, Supplemental Inspection Document
55-10-01, for inspection procedures.		10000HINSPEÇÃO INICIAL9604H196049342.5
--
120M2019-06-15 00:00:00D2029-06-16 00:00:00D2531DOK
2000HINSPEÇÃO REPETITIVA9604H116041342.5
--
120M2019-06-15 00:00:00D2029-06-16 00:00:00D2531DOK
2157-12-01This interval is for severe corrosion environment.
Inspect wing root rib. Refer to Section 2A-14-17,
Supplemental Inspection Document 57-12-01, for
inspection procedure.		3000HINSPEÇÃO INICIAL--
--
MD-D-DOK
3000HINSPEÇÃO REPETITIVA9402.3HCad.001/PRKLK/14 Pág.03312402.32140.8
--
M2018-10-09 00:00:00D-D-DOK
2255-41-01Inspect rudder spar. Refer to Section 2A-14-13,
Supplemental Inspection Document 55-41-01, for
inspection procedure.		100HINSPEÇÃO INICIAL10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
55-11-03Vertical Fin. Inspect the vertical fin attachment.
Refer to Section 2A-14-22, Supplemental Inspection
Document, 55-11-03 for inspection procedure.		100HINSPEÇÃO INICIAL10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
27-20-02Inspect the rudder horn. Refer to Section 2A-14-23,
Supplemental Inspection Document 27-20-02 for
inspection procedure.		100HINSPEÇÃO INICIAL10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
100HINSPEÇÃO REPETITIVA10261.5H10361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
2355-11-02Inspect vertical stabilizer attach bracket and horizontal
stabilizer rear spar attachments. Refer to Section
2A-14-11, Supplemental Inspection Document
55-11-02, for inspection procedure.		2000HINSPEÇÃO INICIAL9402.3H11402.31140.8
--
48M2018-10-09 00:00:00D2022-10-09 14:24:00D89.599999999999DOK
HINSPEÇÃO REPETITIVAHCad.001/PRKLK/14 Pág.033--
--
120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
24Flaps. 1. Check flap travel cable tension, and travel
time. 2. Check flap cable system, control cables,
and pulleys, in accordance with the flight cable
inspection procedures in Section 2A-20-01, Expanded
Maintenance, Control Cables.		100HINSPEÇÃO INICIALH--
--
12MD-D-DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
Aileron. 1. Check aileron travel and cable tension.
2. Check aileron cable system, control cables,
and pulleys, in accordance with the flight cable
inspection procedures in Section 2A-20-01, Expanded
Maintenance, Control Cables.		100HINSPEÇÃO INICIALH--
--
12MD-D-DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
--
120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
Elevator. 1. Check elevator travel and cable tension.
2. Check elevator cable system, control cables,
and pulleys, in accordance with the flight cable
inspection procedures in Section 2A-20-01, Expanded
Maintenance, Control Cables.		100HINSPEÇÃO INICIAL10261.5HCad.001/PRKLK/14 Pág.03310361.5100
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12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
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120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
Elevator Trim. 1. Check elevator trim travel and cable
tension. 2. Check elevator trim cable system, control
cables, and pulleys, in accordance with the flight cable
inspection procedures in Section 2A-20-01, Expanded
Maintenance, Control Cables.		100HINSPEÇÃO INICIAL10261.5HCad.001/PRKLK/14 Pág.03310361.5100
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12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
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120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
Rudder. 1. Check rudder travel and cable tension.
2. Check rudder cable system, control cables,
and pulleys, in accordance with the flight cable
inspection procedures in Section 2A-20-01, Expanded
Maintenance, Control Cables.		100HINSPEÇÃO INICIAL10261.5HCad.001/PRKLK/14 Pág.03310361.5100
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12M2022-05-30 00:00:00D2023-05-30 09:36:00D322.4DOK
100HINSPEÇÃO REPETITIVA10261.5HCad.001/PRKLK/14 Pág.03310361.5100
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120M2022-05-30 00:00:00D2032-05-31 00:00:00D3611DOK
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