manual sid 172 series

7/30/2019 Manual Sid 172 Series

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PROGRAMA

SUPPLEMENTAL INSPECTION DOCUMENT

SID

CESSNA 172 SERIES


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APENDICE C DEL PMA ASIGNACION DEL MANUAL

SUPPLEMENTAL INSPECTION DOCUMENT

SUPLEMENTO DEL PMA

SID


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APENDICE C DEL PMA INDICE GENERAL

INDICE GENERAL

LISTA DE CONTENIDO PAGINA

Asignacin del Manual a-1

ndice General a-2

Registro de Revisiones a-3

Lista de Paginas Efectivas a-4 to a-10

SECCION A - INFORMACION DE LOS DOCUMENTOS DE INSPECCIONSUPLEMENTAL (SID)

SA-0 to SA-1

SECCION B - PROCEDIMIENTO PARA LAS REVISIONES DEL MANUAL SB-0 to SB-2

SECCION C - 2A-10-00 LIMITES DE TIEMPO DE INSPECCION -ESTRUCTURAL

SC-0 to SC-13

SECCION D - 2A-12-01 FICHA DE INSPECCIONES SD-0 to SD-30

SECTION E - 2A-13-00 INTRODUCCION AL SID SE-0 to SE-9


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APENDICE C DEL PMA REGISTRO DE REVISIONES

REGISTRO DE REVISIONES

REVISIONFECHA DEREVISION

FECHA DEAPROBACION EFECTUADO POR

ORIGINAL 30-JUN-2012 MELQUIADES CHAVEZ GALDOS


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APENDICE C DEL PMA LISTA DE PAGINAS EFECTIVAS

LISTA DE PGINAS EFECTIVAS

No. PAGINA REVISION FECHA

01 CARATULA -- --

02 a-1 ORIGINAL 30-JUNIO-2012


04 a-3 ORIGINAL 30-JUNIO-201205 a-4 ORIGINAL 30-JUNIO-2012








13 SA-0 ORIGINAL 30-JUNIO-2012

14 SA-1 ORIGINAL 30-JUNIO-2012


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LISTA DE PGINAS EFECTIVAS (Cont)

No. PAGINA REVISION FECHA

31 SC-13 ORIGINAL 30-JUNIO-2012




35 SD-0 ORIGINAL 30-JUNIO-2012











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PAGINA REVISION FECHA












72 SE-0 ORIGINAL 30-JUNIO-2012




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LISTA DE PGINAS EFECTIVAS (Cont)No. PAGINA REVISION FECHA

92 SF-10 ORIGINAL 30-JUNIO-2012















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LISTA DE PGINAS EFECTIVAS (Cont)No. PAGINA REVISION FECHA

123 SG-17 ORIGINAL 30-JUNIO-2012








131 SG-25 ORIGINAL 30-JUNIO-2012132 SG-26 ORIGINAL 30-JUNIO-2012




136 SG 30 ORIGINAL 30 JUNIO 2012


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161 SG-55 ORIGINAL 30-JUNIO-2012162 SG-56 ORIGINAL 30-JUNIO-2012

163 SH-0 ORIGINAL 30-JUNIO-2012





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183 SI-13 ORIGINAL 30-JUNIO-2012



186 SI-16 ORIGINAL 30-JUNIO-2012187 SI-17 ORIGINAL 30-JUNIO-2012







194 SJ-0 ORIGINAL 30-JUNIO-2012




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APENDICE C DEL PMA SECCION A

SECCION

A


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APENDICE C DEL PMA SUPPLEMENTAL INSPECTION DOCUMENT

A.0. SUPPLEMENTAL INSPECTION DOCUMENTS (SIDs) INFORMATION

A.1. INTRODUCCIN

Cessna Aircraft Company ha publicado la Revisin Temporal D138-1-13 TR7 en el cual adicionala SECCION 2A. INSPECTION TIME LIMITS- STRUCTURE, e incorpora la siguienteinformacin:

1. Supplemental Inspection Documents (SIDs) Information.2. Corrosion Prevention and Control Program (CPCP) Information.3. Control Cable Inspection Information.

A.2. POLITICA

TRAVEL AIR E.I.R.L., tiene como poltica la mejora continua de su programa de mantenimiento,en tal sentido incorpora la edicin completa de la informacin de la SECCION 2A de la revisintemporal D2060-1TR7.

A.3. OBJETIVO.

El objetivo de este Programa INSPECTION TIME LIMITS- STRUCTURE es garantizar laaeronavegabilidad de cada una de nuestras aeronaves para brindar un servicio ms eficiente con


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APENDICE C DEL PMA SECCION B

SECCION

B


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B.0. PROCEDIMIENTOS PARA LAS REVISONES DEL MANUAL

B.1. CARATULA DEL PROGRAMA

Es la primera pgina de este Programa con el propsito de facilitar su identificacin.

B.2. CARATULA DE ASIGNACION DEL PROGRAMA

Es la Segunda Pagina de este Programa donde se registra el Numero del Manual asignado, el

Nmero de Revisin actual y el nombre del departamento, entidad o a quien es asignado elpresente el manual.

B.3. NUMERO DE CONTROL Y LISTA DE DISTRIBUCION DEL PROGRAMA

Los Programa asignados sern numerados correlativamente con un nmero de control. Eldepartamento de Control de Mantenimiento mantendr una Lista de Asignacin de los Manualesen la que incluir el nmero de control y las revisiones que se han incorporado.

01 Direccin General de Aeronutica Civil (D.G.A.C.) (CD)

02 Director de Mantenimiento

03 Departamento de Control de Mantenimiento

04 Estacin de Lnea Nazca


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B.5. REGISTRO DE ACTUALIZACIONES

El Departamento de Control de Mantenimiento, mantendr un registro de las enmiendas yrevisiones que contenga cada nmero de manual y a que persona o departamento hubiera sidoasignado que incluir tambin la fecha de insercin y fecha de vigente de las revisiones.

B.6. REVISIONES TEMPORALES

Debido a que este manual ser peridicamente adecuado, modificado, revisado y corregido, seinsertaran revisiones temporales en hoja A4 color amarillo con el ttulo REVISION TEMPORAL 01,02, 03 etc. El cual tendr una duracin de 3 meses desde su publicacin, hasta que se remita a laDGAC la revisin correspondiente para su aprobacin.

Las Revisiones temporales deben ser firmadas y aprobadas por el Director de Mantenimiento.


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APENDICE C DEL PMA SECCION C

SECCION C


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C.0. INTRODUCCION.

LIMITES DE TIEMPO DE INSPECCION - ESTRUCTURALC.1. ALCANCE

A. Este manual proporciona tiempo y plazos obligatorios de inspeccin para los componentes yestructura de una aeronave. Esta seccin tambin ofrece los datos necesarios para monitorearusando inspecciones programadas.Esta seccin aplica a los tems que podran sufrir fatiga tales como los componentes yestructuras los cuales son parte de los procedimientos de certificacin. Consulte el prrafosiguiente para obtener informacin detallada sobre cada una de estas secciones.

NOTA: Los plazos y los chequeos de mantenimiento que figuran en esta seccin son requisitosmnimos para los aviones explotados en condiciones normales. Para aviones que vuelen en zonasdonde las condiciones sean adversas para el funcionamiento, tales como ambientes de altasalinidad costeras, las zonas de alta temperatura y humedad, zonas en las que los contaminantesdel aire industriales o de otro tipo condiciones presentes, frio extremo, etc, los plazos deben semodificarn en consecuencia.

NOTA: Las guas de inspeccin que figuran en esta seccin no pretenden cubrir a todas, porqueno hay tales cartas que podan reemplazar el buen juicio, criterio y experiencia del mecnico conlicencia en estructuras y motor en el desempeo de sus funciones. Es el principal responsable dela aeronavegabilidad del avin, el propietario u operador debe seleccionar slo personal cualificadopara mantener el avin.

C.2. REQUISITOS DE INSPECCION


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B. Despus de que el uso operativo y el entorno operativo ha sido determinado, realice una entradaen libreta de avin en el que se indica la programacin de inspecciones (TIPICO O SEVERO o eluso de operaciones LEVE / MODERADA o SEVERO) se estn utilizando.

NOTA. Travel Air ha identificado para esta aeronave la Inspeccin SEVERA, descrita en elParrafo . 2. (A) (1) (a) 1 o 2 (A) (1) (a) 2.

C.3. DESCRIPCION

NOTE:A continuacin se ofrece una descripcin detallada y el propsito de las siguientes secciones.

A. LaSeccion C 2A-10-00. Time Limits/Maintenance Checks - General. Esta seccin proveeuna descripcin y propsito de los intervalos de tiempo.

B. La Section D 2A-10-01, Inspection Time Limits.

(1) En esta seccin se muestra, en formato grfico, con todos los requisitos de inspeccin que debenrealizarse. Cada pgina contiene las siguientes cinco columnas:

(a) Estado de la revisin proporciona la fecha en que un determinado item fue agregado,eliminado o revisado. Una entrada en blanco en esta columna indica que no hay cambiosdesde la reedicin de este manual.

(b) Proporciona una breve descripcin de los requisitos de inspeccin de un item demantenimiento.

(c) Indica la frecuencia de un tem y el Intervalo de inspecciones.


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C. En la seccin 2A-20-01, Mantenimiento Ampliado. En esta seccin se ofrece informacinadicional sobre algunos procedimientos de mantenimiento / inspeccin. En l se describe dondelos componentes / items estn localizados, para ser inspeccionados, cmo inspeccionar, etcrequisitos detallados, tales como chequeos funcionales, los chequeos operacionales, etc, seenumeran en la seccin correspondiente del Manual de Servicio Modelo 100 Series. Consulte laseccin correspondiente para obtener informacin detallada completa.

D. Seccin 2A-30-00, de Prevencin y Control de la corrosin (CPCP). Esta seccin ofrece lasdirectrices y las aplicaciones de la CPCP. Este es un programa usado para controlar la corrosin

en la estructura primaria del avin. El objetivo de la CPCP es ayudar a prevenir o controlar lacorrosin de modo que no cause un riesgo para el mantenimiento de la aeronavegabilidad delavin.

C.4. LIMITES DE TIEMPO DE INSPECCION

A. Una inspeccin completa del avin incluye todos los tems de inspeccin requeridos 14 CFR Part43, apndice D y detalles de inspeccin ANUAL/ 100 Horas.Refierase a Seccion 2 del Manualde Servicio del Series 100.

B. intervalos que se indican, recomiendan intervalos en los que los tems van a ser inspeccionados.

(1) Para los operadores de la Parte 14 CFR Part 91, los intervalos de inspeccin no debern serdesviados de los lmites de tiempo descritos en este manual a excepcin como se prevdebajo (Refer to 14 CFR 91.409)

(a) La aeronave puede excederse del punto programado para su inspeccin solamente en10 horas, si el avin esta en ruta para completar su inspeccin.

(b) En el caso de cumplimiento tardo de cualquier operacin programada, la operacin


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FECHA: 30-JUNIO-2012 REVISIN: ORIGINAL PAGINA: SC-4

INSPECTION TIME LIMITSC.5.1. Listado de items de Inspeccin (Hoja 1)

REVISIONSTATUS

TASK INTERVAL OPERATION ZONE

0Inspect aircraft records to verify that all applicable Cessna Service Information Letters,Cessna Service Bulletins and Supplier Service Bulletins are complied with.

Every 100 hours or 12 months,whichever occurs first.

1 ALL

0 Inspect aircraft records to verify that all applicable Airworthiness Directives and FederalAviation regulations are complied with.


1 ALL

0 Inspect aircraft records to verify that all logbook entries required by the FederalAviation Regulations are complied with.


1 ALL

0

Inspect aircraft records to verify that all SID Inspections have been complied with as

scheduled.

Every 100 hours or 12 months,

whichever occurs first. 1 ALL

0 Inspect rudder pedal torque tube and cable attachment arms. Refer to 2A-14-01,Supplemental Inspection Document 27-20-01, for inspection procedure.

Initial: 10,000 hours or 20 years,whichever occurs first; Repeat:3,000 hours or 5 years, whicheveroccurs first.

8 ALL

0

Elevator trim system for Models 150, 172, 175 and 182 (1962). 1. Inspect elevator trimbrackets and actuator support brackets. 2. Inspect pulleys, attaching structure andfasteners. Refer to Section 2A-14-02, Supplemental Inspection Document 27-30-01, forinspection procedures

Initial: 1,000 hours;Repeat: 1,000 hours

15330,340

0

Elevator trim system for Models 180, 182 (prior to 1962) and 185. 1. Inspect elevatortrim brackets and actuator support brackets. 2. Inspect pulleys, attaching structure andfasteners. Refer to Section 2A-14-03, Supplemental Inspection Document 27-30-02, for

inspection procedures.


15330,340

0For Models 180, 182 (prior to 1962) and 185, inspect trim screw barrels and stabilizerscrew-jack actuator threads. Refer to Section 2A-14-04, Supplemental InspectionDocument 27-42-01, for inspection procedures.


15330,340


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REVISIONSTATUS


0For Models 172, 175 and 182, replace U-bolts securing the flat leaf main landing gearassembly. Refer to Section 2A-14-05, Supplemental Inspection Document 32-11-01,for inspection procedures.


24721,722

0

For All Models, this inspection is for mild/moderate corrosion environment. Inspectmain landing gear spring and attach fittings for rust or damage to finish.Refer to Section 2A-14-06, Supplemental Inspection Document 32-13-01, forInspection procedure.

Initial: 20 years;Repeat: 10 years

11721,722

0

For All Models, this inspection is for severe corrosion environment. Inspect mainlanding gear spring and attach fittings for rust or damage to finish. Refer to

Section 2A-14-06, Supplemental Inspection Document 32-13-01, for inspectionprocedure.

Initial: 10 years;

Repeat: 5 years 13

721,

722

0For All Models, inspect main landing gear fittings and attachment of the fittings to thebulkheads. Refer to Section 2A-14-07, Supplemental Inspection Document32-13-02, for inspection procedure.


17 210

0 For All Models, inspect main landing gear axle. Refer to Section 2A-14-08,Supplemental Inspection Document 32-13-03, for inspection procedure.

Initial: 4,000 hours or 10 years,whichever occurs first; Repeat:1,000 hours or 3 Years,whichever occurs first.

7721,722

0

For Models 180 and 185, inspect main landing gearspring axle attach bolt holes. Refer to Section 2A-14-09, Supplemental Inspection Document 32-13-04, forinspection procedure.

Initial: Every time skis areinstalled or removed; Repeat:Every time skis areinstalled or removed

27721,722

0

For Models 180 and 185, this inspection is for mild/moderate corrosion environment. Inspect main landinggear spring axle attach bolt holes. Refer to Section 2A-14-10, Supplemental Inspection Document 32-13-05,for inspection procedure.


12721,722


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REVISION

STATUSTASK INTERVAL OPERATION ZONE

0For Models 180 and 185, this inspection is for severe corrosion environment. Inspectmain landing gear spring axle attach bolt holes. Refer to Section 2A-14-10,Supplemental Inspection Document 32-13-05, for inspection procedure.


14721,722

0For Models 150, 172, 175 and 182, inspect nose landing gear torque links, bolts,bushings and fork. Refer to Section 2A-14-11, Supplemental InspectionDocument 32-20-01, for inspection procedure.


9 720

0

For All Models, this interval is for mild/moderate corrosion environment. Inspect thecarry-thru spar area, door post bulkhead attach fittings and spar channel. Refer toSection 2A-14-12, Supplemental Inspection Document 53-11-01, for inspectionprocedure.


11 210

0For All Models, this interval is for severe corrosion environment. Inspect the carry-thruspar area, door post bulkhead attach fittings and spar channel. Refer to Section 2A-14-12, Supplemental Inspection Document 53-11-01, for inspection procedure.

Initial: 10 years;Repeat: 5 years 13 210

0

For Models 150, 172, 175, 180 and 185, this interval is for typical usage environment.Inspect fuselage forward doorpost bulkhead at the lower end, wing strut attach areaand door hinge area. Refer to Section 2A-14-13, Supplemental Inspection Document53-12-01, for inspection procedure.

Initial: 12,000 hours or 20 years,whichever occurs first; Repeat:2,000 hours or 10 years,whichever occurs first.

20 210

0

For Models 150, 172, 175, 180 and 185, this interval is for severe usage environment.Inspect fuselage forward doorpost bulkhead at the lower end, wing strutattach area and door hinge area. Refer to Section 2A-14-13, Supplemental InspectionDocument 53-12-01, for inspection procedure.


21 210

0 For Model 182, inspect forward doorpost and surrounding structure. Refer to Section2A-14-14, Supplemental Inspection Document 53-12-02, for inspection procedure.

Initial: 4,000 hours or 10 years,

whichever occurs first; Repeat:1,000 hours or 3 years, whicheveroccurs first.

7 210

0 For Models 172 and 175, inspect firewall structure. Refer to Section 2A-14-15,Supplemental Inspection Document 53-12-03, for inspection procedure.


23 210


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REVISION

STATUS


0For All Models, this interval is for mild/moderate corrosion environment. Inspect thecabin interior skin panels, frames and stringers. Refer to Section 2A-14-16,Supplemental Inspection Document 53-30-01, for inspection procedure.


11 210

0For All Models, this interval is for severe corrosion environment. Inspect the cabininterior skin panels, frames and stringers. Refer to Section 2A-14-16, SupplementalInspection Document 53-30-01, for inspection procedure.


13 210

0For Model 182, inspect vertical stabilizer attachment bolts, forward and aft verticalstabilizer structures and vertical stabilizer attach bulkheads. Refer to Section2A-14-17, Supplemental Inspection Document 53-42-01, for inspection procedures.

Initial: 1,000 hours;Repeat: 100 hours

28 310,320

0For All Models, this interval is for mild/moderate corrosion environment. Inspect seatrails for corrosion. Refer to Section 2A-14-18, Supplemental Inspection Document 53-

47-01, for inspection procedure.

Initial: 10 years;

Repeat: 10 years

18 211

0For All Models, this interval is for severe corrosion environment. Inspect seat rails forcorrosion. Refer to Section 2A-14-18, Supplemental Inspection Document53-47-01, for inspection procedure.


19 211

0For All Models, inspect horizontal stabilizer and elevator, including spars, ribs, hingebolts, hinge bearings, attach fittings and torque tube. Refer to Section 2A-14-19,Supplemental Inspection Document 55-10-01, for inspection procedures.


22330,340

0 For Models 172 and 175, inspect horizontal stabilizer forward spar. Refer to Section2A-14-20, Supplemental Inspection Document 55-11-01, for inspection procedure.

Initial: 100 hours or 1 year,whichever occurs first; Repeat:100 hours or 1 year, whicheveroccurs first.

25330,340

0 For Model 150, inspect horizontal stabilizer forward attachments. Refer to Section 2A-14-21, Supplemental Inspection Document 55-11-02, forinspection procedure.

Initial: 100 hours or 1 year,whichever occurs first; Repeat:100 hours or 1 year, whicheveroccurs first

25 330,340

0For All Models, inspect vertical stabilizer and rudder, including spars, ribs, hinge bolts,hinge bearings and attach fittings. Refer to Section 2A-14-22, Supplemental InspectionDocument 55-30-01, for inspection procedure.


22330,340


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REVISION


0

For All Models, this interval is for typical usage environment. 1. Inspect inboard wingstructure and wing attachment to fuselage including working rivets. 2. Inspect flapactuator support structure. Refer to Section 2A-14-23, Supplemental InspectionDocument 57-11-01, for inspection procedure.


20510,610

0

For All Models, this interval is for severe usage environment. 1. Inspect inboard wingstructure and wing attachment to fuselage including working rivets. 2. Inspect flapactuator support structure. Refer to Section 2A-14-23, Supplemental InspectionDocument 57-11-01, for inspection procedure.


21510,610

0For All Models, this interval is for mild/moderate corrosion environment. Inspect wingfor corrosion and missing or loose fasteners. Refer to Section 2A-14-24,Supplemental Inspection Document 57-11-02, for inspection procedure.


11

510,520,610,620

0For All Models, this interval is for severe corrosion environment. Inspect wing forcorrosion and missing or loose fasteners. Refer to Section 2A-14-24, SupplementalInspection Document 57-11-02, for inspection procedure.


13510,520,610,620

0 For Models 180 and 185, inspect wing main spar and rear spar. Refer to Section 2A-14-25, Supplemental Inspection Document 57-11-03, for inspection procedure.

Initial: 4,000 hours;Repeat: 100 hours

29

510,520,610,620

0For All Models, this interval is for mild/moderate corrosion environment. Inspect wingsplice joint at strut attach. Refer to Section 2A-14-26, Supplemental InspectionDocument 57-11-04, for inspection procedure.

Initial: 20 years,Repeat: 10 years,

11510,610

0 For All Models, this interval is for severe corrosion environment. Inspect wing splicejoint at strut attach. Refer to Section 2A-14-26, Supplemental InspectionDocument 57-11-04, for inspection procedure.

Initial: 10 years,Repeat: 5 years

13 510,610

0For All Models, this interval is for mild/moderate corrosion environment. Inspect wingroot rib. Refer to Section 2A-14-27, Supplemental Inspection Document57-12-01, for inspection procedure.


12510,610


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REVISION

STATUS


0For All Models, this interval is for severe corrosion environment. Inspect wing root rib.Refer to Section 2A-14-27, Supplemental Inspection Document 57-12-01, for inspection procedure.


14510,610

0For All Models, this interval is for typical usage environment. Inspect wing strut andstrut tube. Refer to Section 2A-14-28, Supplemental Inspection Document 57-40-01,for inspection procedure.


20510,610

0For All Models, this interval is for severe usage environment. Inspect wing strut andstrut tube. Refer to Section 2A-14-28, Supplemental Inspection Document 57-40-01,for inspection procedure.

Initial: 6,000 hours orC10 years,whicheverCoccurs first; Repeat:1,000 hours or 5 years, whicheveroccurs first.

21510,610

0 For All Models, inspect aileron hinges, hinge bolts, hinge bearings and hinge andpushrod attach fittings. Refer to Section 2A-14-29, Supplemental InspectionDocument 57-51-01, for inspection procedure.

Initial: 3,000 hours or 10 years,

whichever occurs first; Repeat:500 hours or 5 years, whicheveroccursfirst.

16 520,620

0For All Models, this interval is for mild/moderate corrosion environment. Inspect flaptracks for corrosion. Refer to Section 2A-14-30, Supplemental Inspection Document57-53-01, for inspection procedure


11510,620

0For All Models, this interval is for severe corrosion environment. Inspect flap tracks forcorrosion. Refer to Section 2A-14-30, Supplemental Inspection Document57-53-01, for inspection procedure.


13510,610

0

For All Models, inspect engine mount. Refer to Section

2A-14-31, Supplemental Inspection Document 71-20-01, for inspection procedure.

Initial: 10,000hours or 20 years,

whichever occursfirst; Repeat: AtEngine Overhaul

10 120

0 For Models 172 and 175, inspect engine mount brackets. Refer to Section 2A-14-32,Supplemental Inspection Document 71-20-02, for inspection procedure.


26120,210,


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REVISIONSTATUS


0

Fuselage lower internal structure beneath the floor panels for All Models. Make sureyou inspect these areas: 1. Cabin structure under floorboards. NOTE:Corrosion Prevention and Control Program Inspection item (baseline interval, refer toSection 2A-30-00 for additional inspection information).

Every 60 months 6 211

0

Fuselage internal structure in upper fuselage for All Models. Make sure you inspectthese areas: 1. Cabin bulkhead corners. 2. Fuselage skin. NOTE: Corrosion Preventionand Control Program Inspection item (baseline interval, refer to Section 2A-30-00 foradditional inspection information).


0

Areas of the cabin structure for All Models. Make sure you inspect these areas: 1.Firewall. 2. Firewall attachments. NOTE: Corrosion Prevention and Control ProgramInspection item (baseline interval, refer to Section 2A-30-00 for additional inspection

information).


0

Passenger/Crew door retention system for All Models. Make sure you inspect theseareas: 1. Bell cranks. 2. Pushrods. 3. Handle. 4. Pin retention. 5. Pins. 6. Lockplatesand guides. 7. Hinges. 8. Internal door framing. NOTE: Corrosion Prevention andControl Program Inspection item (baseline interval, refer to Section 2A-30-00 foradditional inspection information). Note: Remove interior panels for access.


0

Areas of the cabin structure for the passenger/crew door for All Models. Make sure youinspect these areas: 1. Door frames. 2. Door hinges. NOTE: Corrosion Prevention andControl Program Inspection item (baseline interval, refer to Section 2A-30-00 foradditional inspection information).


0

Areas of the cabin structure for All Models. Make sure you inspect these areas: 1.Cabin door forward and aft frames. 2. Window frames with emphasis at stringersand channel assemblies from aft of door frame to aft bulkhead. 3. Seat attachmentstructure. 4. Aft Cabin Bulkhead. NOTE: Corrosion Prevention and Control ProgramInspection item (baseline interval, refer to Section 2A-30-00 for additional inspectioninformation).



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APENDICE C DEL PMA LIMITES DE TIEMPO DE INSPECCION



REVISION


0Flaps (All Models). 1. Check flap travel cable tension and travel time. 2. Check flapcable system, control cables and pulleys, in accordance with the flight cableinspection procedures in Section 2A-20-01, Expanded Maintenance, Control Cables.

Initial: 100 hours; Repeat: every600 hours or 12 months,whichever occursfirst.

30210,510,610

0Aileron (All Models). 1. Check aileron travel and cable tension. 2. Check aileron cablesystem, control cables and pulleys, in accordance with the f light cable inspectionprocedures in Section 2A-20-01, Expanded Maintenance, Control Cables.

Initial: 100 hours; Repeat: every600 hours or 12 months,whichever occurs first.

30

210,510,520,610,620

0Elevator (All Models). 1. Check elevator travel and cable tension. 2. Check elevatorcable system, control cables and pulleys, in accordance with the flight cableinspection procedures in Section 2A-20-01, Expanded Maintenance, Control Cables.

Initial: 100 hours; Repeat: every600 hours or 12 months,whichever occurs first

30

210,510,520,610,620

0

Elevator Trim (All Models). 1. Check elevator trim travel and cable tension. 2. Checkelevator trim cable system, control cables and pulleys, in accordance with the flightcable inspection procedures in Section 2A-20-01, Expanded Maintenance, ControlCables.

Initial: 100 hours;Repeat: every 600 hours or 12months, whichever occursfirst.

30

210,310,330,340

0Rudder (All Models). 1. Check rudder travel and cable tension. 2. Check rudder cablesystem, control cables and pulleys, in accordance with the f light cable inspectionprocedures in Section 2A-20-01, Expanded Maintenance, Control Cables.

Initial: 100 hours;Repeat: every 600 hours or 12months, whichever occurs first.

30210,310,320

0

Wing structure internal for All Models. Make sure you inspect these areas: 1. Main sparupper and lower carry-thru fittings. 2. Main spar upper and lower caps. 3. Main sparweb. NOTE: Corrosion Prevention and Control Program Inspection item (baseline

interval, refer to Section 2A-30-00 for additional inspection information).

Every 12 months 2

510,520,610,

620

0

Wing structure internal for All Models. Make sure you inspect these areas: 1. Wingfront 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).

Every 60 months 6

510,520,610,620


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INSPECTION TIME LIMITS

C.5.9. Listado de items de Inspeccin (Hoja 9)

REVISIONSTATUS TASK INTERVAL OPERATION ZONE

0

Wing structure external for All Models. Make sure you inspect these areas: 1. Skinwith emphasis at skin overlaps and under access panels. 2. Rear spar upper and lowercaps. 3. Rear spar web. NOTE: Corrosion Prevention and Control Program Inspectionitem (baseline interval, refer to Section 2A-30-00 for additional inspection information).

Every 60 months 6

510,520,610,620

0

Aileron attachments for All Models. Make sure you inspect these areas: 1. Aileronhinges. 2. Hinge bolts. 3. Hinge bearings. 4. Hinge and pushrod support structure.NOTE: Corrosion Prevention and Control Inspection Item (baseline interval, refer toSection 2A-30-00 for additional inspection information). NOTE: Do not apply LPS-3Heavy Duty Rust Inhibitor on hinge bearing.

Every 24 months 3520,620

0

Vertical stabilizer structure for All Models. Make sure you inspect these areas: 1.Forward spar attachment to tailcone bulkhead. 2. Aft spar attachment to lower

vertical stabilizer spar. 3. Front and rear spars. 4. Rear spar rudder hinges. NOTE:Corrosion Prevention and Control Program Inspection item (baseline interval,refer to Section 2A-30-00 for additional inspection information)

Every 60 months 6 310,320,

0

Main landing gear axle assembly for All Models. Make sure you inspect these areas: 1.Main gear axle and attach bolts. 2. Wheel halves. NOTE: Corrosion Prevention andControl Program Inspection item (baseline interval, refer to Section 2A-30-00 foradditional inspection information). NOTE: Do not apply LPS-3 Heavy-Duty RustInhibitor to the bearing. NOTE: Coordinate with tire change.


0

Nose gear trunnion, steering assembly, torque link assembly, nose gear fork and axlefor All Models. 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 andattach bolt. 4. Nose gear fork. 5. Nose gear axle. NOTE: Corrosion Prevention andControl Inspection Item (baseline interval, refer to Section 2A-30-00 foradditional inspection information).


0

Nose gear trunnion, torque link assembly and nose gear fork for All Models. Make sureyou inspect these areas: 1. Nose gear trunnion upper and lower inner bore surface andbearing. 2. Torque link bolt and attach pin inner bore surface. 3. Nose gear fork luginner bore surface. NOTE: Corrosion Prevention and Control Inspection Item (baselineinterval, refer to Section 2A-30-00 for additionalinspection information).



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REVISIONSTATUS


0

Nose landing gear outer barrel assembly for All Models. Make sure you inspect theseareas: 1. Outer barrel assembly. 2. Upper strut end and lower collar assembly. NOTE:Corrosion Prevention and Control Inspection Item (baseline interval, refer to Section2A-30-00 for additional inspection information). NOTE: do not apply LPS-3 Heavy-DutyRust Inhibitor to the sliding surfaces of the oleo strut.


0

Nose gear axle assembly for All Models. Make sure you inspect these areas: 1. Nosegear axle and attach bolt. 2. Wheel halves. NOTE: Corrosion Prevention and ControlProgram Inspection item (baseline interval, refer to Section 2A-30-00 for additionalinspection information). NOTE: Disassemble the nose gear strut to get access. NOTE:Do not apply LPS-3 Heavy-Duty Rust Inhibitor to the sliding surfaces of the oleo strut.NOTE: Coordinate with tire change.


0

Horizontal stabilizer structure for All Models. Make sure you inspect these areas: 1.Stabilizer attachment to the tailcone bulkhead. 2. Front and rear spars. NOTE:

Corrosion Prevention and Control Program Inspection item (baseline interval, refer toSection 2A-30-00 for additional inspection information).

Every 60 months 6330,

340,

0

Elevator trim system for All Models. Make sure you inspect these areas: 1. Elevatortrim brackets. 2. Actuator support brackets and bearings. 3. Pulleys and attachingstructure. NOTE: Corrosion Prevention and Control Inspection Item (baseline interval,refer to Section 2A-30-00 for additional inspection information). NOTE: Do not applyLPS-3 Heavy Duty Rust Inhibitor on hinge bearing.


0

Rudder attachments for All Models. Make sure you inspect these areas: 1. Hingebrackets. 2. Hinge bolts. 3. Hinge bearings. NOTE: Corrosion Prevention and ControlInspection Item (baseline interval, refer to Section 2A-30-00 for additional inspectioninformation). NOTE: Do not apply LPS-3 Heavy Duty Rust Inhibitor on hinge bearing


0

Rudder structure for AllModels. Make sure you inspect these areas: 1. Skin. 2. Forward

and aft spars at hinge locations. NOTE: Corrosion Prevention and ControlInspection Item (baseline interval, refer to Section 2A-30-00 for additional inspectioninformation).


0

Engine support structure for All Models. Make sure you inspect these areas: 1. Enginetruss. Pay particular attention to vicinity of welds. NOTE: Corrosion Prevention andControl Program Inspection item (refer to Section 2A-30-00 for additional inspectioninformation).



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APENDICE C DEL PMA OPERACIONES DE INSPECCION

C.6. INSPECTION INTERVAL REQUIREMENTSC.6.1. Listado de Intervalos-(Hoja 1)

Operation Details

1 Every 100 hours of operation or 12 months, whichever occurs first.

2

Corrosion Prevention and Control Program Inspections (Baseline Program) items that are to

be examined every 12 months. Refer to Section 2A-30-00, Corrosion Prevention and ControlProgram, for additional information concerning repeat Corrosion Program Inspectionintervals.

3Corrosion Prevention and Control Program Inspections (Baseline Program) items that are tobe examined every 24 months. Refer to Section 2A-30-00, Corrosion Prevention and ControlProgram for additional information concerning repeat Corrosion Program Inspection intervals

4 Corrosion Prevention and Control Program Inspections (Baseline Program) items that are tobe examined every 36 months. Refer to Section 2A-30-00, Corrosion Prevention and ControlProgram for additional information concerning repeat Corrosion Program Inspection intervals

5Corrosion Prevention and Control Program Inspections (Baseline Program) items that are tobe examined every 48 months. Refer to Section 2A-30-00, Corrosion Prevention and ControlProgram for additional information concerning repeat Corrosion Program Inspection intervals


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C.6.2. Intervals-(Hoja 2)

Operation Details

13

Supplemental Inspection Document items that are to be examined after the first 10 years.The inspection is to be repeated every 5 years after the initial inspection has beenaccomplished, for airplanes operating in a severe corrosion environment.

14

Supplemental Inspection Document items that are to be examined after the first 3 years. Theinspection is to be repeated every 3 years after the initial inspection has been accomplished,for airplanes operating in a severe corrosion environment.

15Supplemental Inspection Document items that are to be examined after the first 1,000 hours.The inspection is to be repeated every 1,000 hours after the initial inspection has beenaccomplished.

16

Supplemental Inspection Document items that are to be examined after 3,000 hours or 10

years, whichever occurs first. The inspection is to be repeated every 500 hours or 5 years,whichever occurs first, after the initial inspection has been accomplished.

17Supplemental Inspection Document items that are to be examined after 3,000 hours or 5years, whichever occurs first. The inspection is to be repeated every 1,000 hours or 5 years,whichever occurs first, after the initial inspection has been accomplished.

18Supplemental Inspection Document items that are to be examined after the first 10 years.The inspection is to be repeated every 10 years after the initial inspection has been


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C.6.3. Intervals-(Hoja 3)

Operation Details

25

Supplemental Inspection Document items that are to be examined after the first 100 hours ofoperation or 1 year, whichever occurs first. The inspection is to be repeated every 100 hoursof operation or 1 year, whichever occurs first, after the initial inspection has been

accomplished.

26

Supplemental Inspection Document items that are to be examined after the first 2,500 hoursof operation or 5 years, whichever occurs first. The inspection is to be repeated every 2,500hours of operation or 5 years, whichever occurs first, after the initial inspection has beenaccomplished.

27Supplemental Inspection Document items that are to be examined every time when skis areinstalled or removed.

28Supplemental Inspection Document items that are to be examined after the first 1,000 hoursof operation. The inspection is to be repeated every 100 hours of operation, after the initialinspection has been accomplished.

29Supplemental Inspection Document items that are to be examined after the first 4,000 hoursof operation. The inspection is to be repeated every 100 hours of operation, after the initialinspection has been accomplished.

Expanded Maintenance Inspection items that are to be examined after the first 100 hours of


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APENDICE C DEL PMA SECCION D

SECCION


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D.1.INSPECTION OPERATION 1

Date: _______________

Registration Number: _______________

Serial Number: _______________Total Time: _______________

1. DescriptionA. Operation 1 gives Records Inspections items that are to be examined every 100 hours of

operation or 12 months, whichever occurs first.B. Inspection items are given in the order of the zone in which the inspection is to be completed.

Frequently, tasks give more information about each required inspection.C. The right portion of each page gives space for the mechanic's and inspector's initials and

remarks. A copy of these pages can be used as a checklist when these inspections arecompleted.

2. General Inspection CriteriaA. While each of the specified inspection tasks in this section are done, more general inspections

of the adjacent areas must be done while access is available. These general inspections areused to find apparent conditions which can need more maintenance.

B. If a component or system is changed after a required task has been completed, then thatspecified task must be done again to make sure it is correct before the system or component isreturned to service.


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Date: _______________


Serial Number: _______________

Total Time: _______________

1. Description

A. Operation 2 gives Corrosion Prevention and Control Program Inspections (Baseline Program)items that are to be examined every 12 months. Refer to Section 2A-30-00, CorrosionPrevention and Control Program, for additional information concerning repeat Corrosion

Program Inspection intervals.B. Inspection items are given in the order of the zone in which the inspection is to be completed.





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Date: _______________



Total Time: _______________

1. Description

A. Operation 3 gives Corrosion Prevention and Control Program Inspections (Baseline Program)items that are to be examined every 24 months. Refer to Section 2A-30-00, CorrosionPrevention and Control Program, for additional information concerning repeat CorrosionProgram Inspection intervals.

B. Inspection items are given in the order of the zone in which the inspection is to be completed.Frequently, tasks give more information about each required inspection.

C. The right portion of each page gives space for the mechanic's and inspector's initials andremarks. A copy of these pages can be used as a checklist when these inspections arecompleted.

2. General Inspection Criteria

A. While each of the specified inspection tasks in this section are done, more general inspections


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D.3.1.INSPECTION OPERATION 3 (CONT.)

TASK ZONE MECH INSP REMARKS

Rudder attachments for All Models. Make sureyou inspect these areas: 1. Hinge brackets. 2.Hinge bolts. 3. Hinge bearings. NOTE:Corrosion Prevention and Control InspectionItem (baseline interval, refer to Section 2A-30-00 for additional inspection information). NOTE:Do not apply LPS-3 Heavy Duty Rust Inhibitoron hinge bearing.

320

Rudder structure for All Models. Make sure you

inspect these areas: 1. Skin. 2. Forward andaft spars at hinge locations. NOTE: CorrosionPrevention and Control Inspection Item(baseline interval, refer to Section 2A-30-00 foradditional inspection information).

320

*** End of Operation 3 Inspection Items ***


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D.4. INSPECTION OPERATION 4

Date: _______________



Total Time: _______________

1. Description


B. Inspection items are given in the order of the zone in which the inspection is to be completed.

Frequently, tasks give more information about each required inspection.C. The right portion of each page gives space for the mechanic's and inspector's initials andremarks. A copy of these pages can be used as a checklist when these inspections arecompleted.


A. While each of the specified inspection tasks in this section are done, more general inspectionsof the djacent areas must be done while access is available. These general inspections are


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D.4.1. INSPECTION OPERATION 4 (CONT.)


Nose gear trunnion, torque link assembly and

nose gear fork for All Models. Make sure youinspect these areas: 1. Nose gear trunnionupper and lower inner bore surface andbearing. 2. Torque link bolt and attach pin innerbore surface. 3. Nose gear fork lug inner boresurface. NOTE: Corrosion Prevention andControl Inspection Item (baseline interval, referto Section 2A-30-00 for additional inspectioninformation).

720

Nose landing gear outer barrel assembly for AllModels. Make sure you inspect these areas: 1.Outer barrel assembly. 2. Upper strut end andlower collar assembly. NOTE: CorrosionPrevention and Control Inspection Item(baseline interval, refer to Section 2A-30-00 foradditional inspection information). NOTE: donot apply LPS-3 Heavy-Duty Rust Inhibitor tothe sliding surfaces of the oleo strut.

720


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Date: _______________



Total Time: _______________

1. Description

A. Operation 5 gives Corrosion Prevention and Control Program Inspections (Baseline Program)items that are to be examined every 48 months. Refer to Section 2A-30-00, CorrosionPrevention and Control Program, for additional information concerning repeat Corrosion

Program Inspection intervals.B. Inspection items are given in the order of the zone in which the inspection is to be completed.Frequently, tasks give more information about each required inspection.




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Date: _______________



Total Time: _______________1. Description





A. While each of the specified inspection tasks in this section are done, more general inspectionsof the adjacent areas must be done while access is available. These general inspections areused to find apparent conditions which can need more maintenance.

B. If a component or system is changed after a required task has been completed, then that


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D.6.1 INSPECTION OPERATION 6 (CONT.)


Areas of the cabin structure for All Models.Make sure you inspect these areas: 1. Cabindoor forward and aft frames. 2. Window frameswith emphasis at stringers and channelassemblies from aft of door frame to aft

bulkhead. 3. Seat attachment structure. 4. AftCabin Bulkhead. NOTE: Corrosion Preventionand Control Program Inspection item (baselineinterval, refer to Section 2A-30-00 for additionalinspection information).

210

Wing structure internal for All Models. Makesure you inspect these areas: 1. Wing upperand lower spar caps. 2. Wing attach sparfittings. 3. Wing lower skins. NOTE: Corrosion

Prevention and Control Program InspectionItem (baseline interval, refer to Section 2A-30-00 for additional inspection information).

510,520,

610,620

Wing structure external for AllModels. Makesure you inspect these areas: 1. Skin withemphasis at skin overlaps and under accesspanels. 2. Rear spar upper and lower caps.3. Rear spar web. NOTE: Corrosion Preventionand Control Program Inspection item (baseline

510,520,610,620


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Date: _______________




A. Operation 7 gives Supplemental Inspection Document items that are to be examined after thefirst 4,000 hours of operation or 10 years, whichever occurs first. The inspection is to berepeated every 1,000 hours of operation or 3 years, whichever occurs first, after the initialinspection has been accomplished.







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Date: _______________




A. Operation 8 gives Supplemental Inspection Document items that are to be examined after thefirst 10,000 hours of operation or 20 years, whichever occurs first. The inspection is to berepeated every 3,000 hours of operation or 5 years, whichever occurs first, after the initialinspection has been accomplished..







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Date: _______________











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Date: _______________




A. Operation 10 gives Supplemental Inspection Document items that are to be examined after thefirst 10,000 hours of operation or 20 years, whichever occurs first. The inspection is to berepeated at engine overhaul, after the initial inspection has been accomplished.


C. The right portion of each page gives space for the mechanic's and inspector's initials and






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Date: _______________




A. Operation 11 gives Supplemental Inspection Document items that are to be examined after thefirst 20 years. The inspection is to be repeated every 10 years after the initial inspection hasbeen accomplished, for airplanes operating in a mild or moderate corrosion environment.





B. If a component or system is changed after a required task has been completed, then thatspecified task must be done again to make sure it is correct before the system or component is


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D.11.1. INSPECTION OPERATION 11


For All Models,This interval is for mild/moderate

corrosion environment. Inspect wing splice jointat strut attach. Refer to Section 2A-14-17,Supplemental Inspection Document 57-11-03,for inspection procedure.

510,610

For All Models,This interval is for mild/moderatecorrosion environment. Inspect flap tracks forcorrosion. Refer to Section 2A-14-21,Supplemental Inspection Document 57-53-01,for inspection procedure.

510,610



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Date: _______________




A. Operation 12 gives Supplemental Inspection Document items that are to be examined after thefirst 5 years. The inspection is to be repeated every 5 years after the initial inspection has beenaccomplished, for airplanes operating in a mild or moderate corrosion environment.







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D.13.

INSPECTION OPERATION 13

Date: _______________



Total Time: _______________

1. Description

A. Operation 13 gives Supplemental Inspection Document items that are to be examined after thefirst 10 years. The inspection is to be repeated every 5 years after the initial inspection hasbeen accomplished, for airplanes operating in a severe corrosion environment.








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D.13.1 INSPECTION OPERATION 13 (CONT.)


For All Models, this interval is for severecorrosion environment. Inspect wing forcorrosion and missing or loose fasteners. Referto Section 2A-14-24, Supplemental InspectionDocument 57-11-02, for inspection procedure.

510,520,

610,620

For All Models, this interval is for severecorrosion environment. Inspect wing splice jointat strut attach. Refer to Section 2A-14-26,Supplemental Inspection Document 57-11-04,for inspection procedure.

510,610

For All Models, this interval is for severecorrosion environment. Inspect flap tracks forcorrosion. Refer to Section 2A-14-30,Supplemental Inspection Document 57-53-01,for inspection procedure.

510,610



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Date: _______________




A. Operation 14 gives Supplemental Inspection Document items that are to be examined after thefirst 3 years. The inspection is to be repeated every 3 years after the initial inspection has beenaccomplished, for airplanes operating in a severe corrosion environment.





B If a component or system is changed after a required task has been completed then that


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Date: _______________



Total Time: _______________

A. Description

A. Operation 15 gives Supplemental Inspection Document items that are to be examined after thefirst 1,000 hours. The inspection is to be repeated every 1,000 hours after the initial inspectionhas been accomplished.


C. The right portion of each page gives space for the mechanics and inspectors initials and






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Date: _______________



Total Time: _______________

1. Description

A. Operation 16 gives Supplemental Inspection Document items that are to be examined after thefirst 10 years. The inspection is to be repeated every 5 years after the initial inspection hasbeen accomplished.





A. While each of the specified inspection tasks in this section are done, more general inspectionsof the adjacent areas must be done while access is available. These general inspections are


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Date: _______________



Total Time: _______________

1. Description

A. Operation 17 gives Supplemental Inspection Document items that are to be examined after3,000 hours or 5 years, whichever occurs first. The inspection is to be repeated every 1,000

hours or 5 years, whichever occurs first, after the initial inspection has been accomplished.B. Inspection items are given in the order of the zone in which the inspection is to be completed.





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Date: _______________



Total Time: _______________

1. Description

A. Operation Operation 18 gives Supplemental Inspection Document items that are to beexamined after the first 10 years. The inspection is to be repeated every 10 years after theinitial inspection has been accomplished, for airplanes operating in a mild or moderatecorrosion environment.

B. Inspection items are given in the order of the zone in which the inspection is to be completed.Frequently, tasks give more information about each required inspection.C. The right portion of each page gives space for the mechanic's and inspector's initials and



A. While each of the specified inspection tasks in this section are done, more general inspectionsof the adjacent areas must be done while access is available These general inspections are


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Date: _______________



Total Time: _______________

1. Description

A. Operation 19 gives Supplemental Inspection Document items that are to be examined after thefirst 5 years. The inspection is to be repeated every 5 years after the initial inspection has beenaccomplished, for airplanes operating in a severe corrosion environment.






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Date: _______________



Total Time: _______________

1. Description

A. Operation 20 gives Supplemental Inspection Document items that are to be examined after12,000 hours or 20 years, whichever occurs first. The inspection is to be repeated every 2,000hours or 10 years, whichever occurs first, after the initial inspection has been accomplished, forairplanes operating in a typical usage environment.


Frequently, tasks give more information about each required inspection.C. The right portion of each page gives space for the mechanic's and inspector's initials andremarks. A copy of these pages can be used as a checklist when these inspections arecompleted.




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Date: _______________



Total Time: _______________

1. Description

A. Operation 21 gives Supplemental Inspection Document items that are to be examined after thefirst 6,000 hours of operation or 10 years, whichever occurs first. The inspection is to berepeated every 1,000 hours of operation or 5 years, whichever occurs first, after the initialinspection has been accomplished, for airplanes operating in a severe usage environment.




of the adjacent areas must be done while access is available. These general inspections areused to find apparent conditions which can need more maintenance.



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Date: _______________








A. While each of the specified inspection tasks in this section are done, more general inspectionsof the adjacent areas must be done while access is available. These general inspections areused to find apparent conditions which can need more maintenance


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Date: _______________



Total Time: _______________

1. Description







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D.24.


Date: _______________



Total Time: _______________

1. Description







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Date: _______________




A. Operation 25 gives Supplemental Inspection Document items that are to be examined after thefirst 100 hours of operation or 1 year, whichever occurs first. The inspection is to be repeatedevery 100 hours of operation or 1 year, whichever occurs first, after the initial inspection hasbeen accomplished.







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Date: _______________



Total Time: _______________

1. Description








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Date: _______________




A. Operation 27 gives Supplemental Inspection Document items that are to be examined everytime when skis are installed or removed.





B. If a component or system is changed after a required task has been completed, then thatspecified task must be done again to make sure it is correct before the system or component isreturned to service


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D.28.


Date: _______________



Total Time: _______________

1. Description

A. Operation 28 gives Supplemental Inspection Document items that are to be examined after thefirst 1,000 hours of operation. The inspection is to be repeated every 100 hours of operation,after the initial inspection has been accomplished.



remarks. A copy of these pages can be used as a checklist when these inspections arecompleted.2. General Inspection Criteria




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D.29.

INSPECTION OPERATION 29Date: _______________



Total Time: _______________

1. Description

A. Operation 29 gives Supplemental Inspection Document items that are to be examined after thefirst 4,000 hours of operation. The inspection is to be repeated every 100 hours of operation,after the initial inspection has been accomplished.




A. While each of the specified inspection tasks in t