manual sid 200 series

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PROGRAMA

SUPPLEMENTAL INSPECTION DOCUMENT

SID

CESSNA 200 SERIES


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APENDICE CDEL PMA INDICE GENERAL

SUPPLEMENTAL INSPECTION DOCUMENT

SUPLEMENTO DEL PMA

SID

MANUAL N


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APENDICE CDEL PMA REGISTRO DE REVISIONES

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-11

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-16

SECCION D - 2A-12-01 FICHA DE INSPECCIONES SD-0 to SD-37

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

SECTION F - 2A-13-01 REQUERIMIENTOS Y METODOS DE PND SF-0 to SF-23


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APENDICE CDEL 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











13 SA-0 ORIGINAL 30-JUNIO-2012

14 SA-1 ORIGINAL 30-JUNIO-2012


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LISTA DE PGINAS EFECTIVAS (Cont)


31 SC-13 ORIGINAL 30-JUNIO-2012




35 SD-0 ORIGINAL 30-JUNIO-2012




39 SD-4 ORIGINAL 30-JUNIO-201240 SD-5 ORIGINAL 30-JUNIO-2012




44 SD 9 ORIGINAL 30 JUNIO 2012


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PAGINA REVISION FECHA













73 SE-0 ORIGINAL 30-JUNIO-2012

74 SE 1 ORIGINAL 30 JUNIO 2012


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91 SF-8 ORIGINAL 30-JUNIO-2012





96 SF -13 ORIGINAL 30-JUNIO-2012








104 SF 21 ORIGINAL 30 JUNIO 2012


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121 SG-14 ORIGINAL 30-JUNIO-2012








129 SG-22 ORIGINAL 30-JUNIO-2012130 SG-23 ORIGINAL 30-JUNIO-2012






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164 SG ORIGINAL 30 JUNIO 2012


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181 SI-3 ORIGINAL 30-JUNIO-2012













S O G O


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211 AP1-5 ORIGINAL 30-JUNIO-2012







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APENDICE CDEL PMA SECCION A

SECCION

A


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APENDICE CDEL PMA SECCION A

A.0. SUPPLEMENTAL INSPECTION DOCUMENTS (SIDs) INFORMATION

A.1. INTRODUCCIN

Cessna Aircraft Company ha publicado la Revisin Temporal D2070-3TR10 en el cual adiciona laSECCION 2A. INSPECTION TIME LIMITS- STRUCTURE, e incorpora la siguiente informacin:

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 D2070-3TR10.

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 conun alto grado de seguridad para nuestros clientes.


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APENDICE CDEL PMA SECCION B

SECCION


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APENDICE CDEL 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 y estructuras

los cuales son parte de los procedimientos de certificacin. Consulte el prrafo siguiente paraobtener informacin detallada sobre cada una de estas secciones.

NOTA: Los plazos y los chequeos de mantenimiento que figuran en esta seccin son requisitos mnimospara los aviones explotados en condiciones normales. Para aviones que vuelen en zonas donde lascondiciones sean adversas para el funcionamiento, tales como ambientes de alta salinidad costeras, laszonas de alta temperatura y humedad, zonas en las que los contaminantes del aire industriales o de otrotipo condiciones presentes, frio extremo, etc, los plazos deben se modificarn en consecuencia.

NOTA: Las guas de inspeccin que figuran en esta seccin no pretenden cubrir a todas, porque no haytales cartas que podan reemplazar el buen juicio, criterio y experiencia del mecnico con licencia enestructuras y motor en el desempeo de sus funciones. Es el principal responsable de laaeronavegabilidad del avin, el propietario u operador debe seleccionar slo personal cualificado paramantener el avin.

C.2. REQUISITOS DE INSPECCION

A. Hay dos tipos de requisitos de inspeccin disponibles en funcin del uso operativo y los otros dos tipos


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

NOTA. Travel Air ha identificado para esta aeronave la Inspeccin SEVERA, descrita en el Parrafo .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 provee una

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 orevisado. Una entrada en blanco en esta columna indica que no hay cambios desde la reedicin deeste manual.

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

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

(d) Operaciones aplicable(s) indica la operacin de inspecciones aplicables actualizadas conteniendo el


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C. En la seccin 2A-20-01, Mantenimiento Ampliado. En esta seccin se ofrece informacin adicional

sobre algunos procedimientos de mantenimiento / inspeccin. En l se describe donde loscomponentes / items estn localizados, para ser inspeccionados, cmo inspeccionar, etc requisitosdetallados, tales como chequeos funcionales, los chequeos operacionales, etc, se enumeran en laseccin correspondiente del Manual de Servicio Modelo 206. Consulte la seccin correspondiente paraobtener 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 laestructura primaria del avin. El objetivo de la CPCP es ayudar a prevenir o controlar la corrosin de

modo que no cause un riesgo para el mantenimiento de la aeronavegabilidad del avin.

C.4. LIMITES DE TIEMPO DE INSPECCION

A. Una inspeccin completa del avin incluye todos los tems de inspeccin requeridos 14 CFR Part 43,apndice D y detalles de inspeccin ANUAL/ 100 Horas.Refierase a Seccion 2 del Manual deServicio del Modelo Series 200.

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 prev debajo(Refer to 14 CFR 91.409)

(a) La aeronave puede excederse del punto programado para su inspeccin solamente en 10horas, si el avin esta en ruta para completar su inspeccin.

(b) En el caso de cumplimiento tardo de cualquier operacin programada, la operacinsiguiente en la secuencia conserva el punto de hora programada debido a la programacin


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

C.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 SIDInspections have been complied with as scheduled.


1 ALL

0Wing structure internal. Make sure you examine these areas: 1. Main spar upper andlower 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).

Every 12 months 2510,520,610,620

0

Elevator and Elevator Tab. Inspect foam filled elevator trailing edge and foam filledelevator tab for corrosion. NOTE: Corrosion Prevention and Control ProgramInspection Item (baseline interval, refer to Section 2A-30-00 for additional inspectioninformation).

Every 12 months 2330,340

0

Aileron attachments. Make sure you inspect these areas: 1. Aileron hinges, 2. Hingebolts, 3. Hinge bearings, 4. Hinge and pushrod support structure. NOTE: CorrosionPrevention and Control Inspection Item (baseline interval, refer to Section 2A-30-00 foradditional inspection information). NOTE: Do not apply LPS-3 Heavy Duty Rust

Inhibitor on hinge bearing.


0

Elevator trim system. Make sure you inspect these areas: 1. Elevator trim 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.



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REVISIONSTATUS


0

Rudder attachments. Make sure you inspect these areas: 1. Hinge brackets. 2. Hingebolts. 3. Hinge bearings. 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.

Every 24 months 3 320

0

Rudder structure. Make sure you inspect these areas:1. Skin. 2. Forward and aft spars at hinge locations. NOTE: Corrosion Prevention andControl Inspection Item (baseline interval, refer to Section 2A-30-00 for additionalinspection information).


0

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


0

Nose gear trunnion, torque link assembly, and nosexgear fork . Make sure you inspectthese areas: 1. Nosexgear trunnion upper and lower inner bore surface andxbearing. 2.Torque link bolt and attach pin inner borexsurface. 3. Nose gear fork lug inner boresurface.xNOTE: Corrosion Prevention and Control InspectionxItem (baseline interval,refer to Section 2A-30-00 forxadditional inspection information).


0

Nose landing gear outer barrel assembly. Make sure you inspect these areas: 1. Outerbarrel 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

Passenger/Crew door retention system. Make sure you inspect these areas: 1. Bellcranks. 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 Section2A-30-00 for additional inspection information). Note: Remove interior panels foraccess.



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REVISIONSTATUS


0

Areas of the cabin structure for the passenger/crew door. Make sure you inspect theseareas: 1. Door frames. 2. Door hinges. NOTE: Corrosion Preventionand Control Program Inspection item (baseline interval, refer to Section 2A-30-00 foradditional inspection information).


0

Fuselage lower internal structure beneath the floor panels. Make sure you inspectthese areas: 1. Cabin structure under floorboards. NOTE: Corrosion Prevention andControl Program Inspection item (baseline interval, refer to Section 2A-30-00 foradditional inspection information).


0

Fuselage internal structure in upper fuselage. Make sure you inspect these areas: 1.Cabin bulkhead corners. 2. Fuselage skin. NOTE: Corrosion Prevention and ControlProgram Inspection item (baseline interval, refer to Section 2A-30-00 for additionalinspection information).


0Areas of the cabin structure. Make sure you inspect these areas: 1. Firewall. 2. Firewallattachments. NOTE: Corrosion Prevention and Control Program Inspection item(baseline interval, refer to Section 2A-30-00 for additional inspection information).


0

Areas of the cabin structure. Make sure you inspect these areas: 1. Cabin door forwardand aft frames. 2. Window frames with emphasis at stringers and channel assembliesfrom aft of door frame to aft bulkhead. 3. Seat attachment structure. 4. AftCabin Bulkhead. NOTE: Corrosion Prevention and Control Program Inspection item(baseline interval, refer to Section 2A-30-00 for additional inspection information).


0

Wing structure internal. Make sure you inspect these areas: 1. Wing main spar upperand 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

0

Wing structure external. Make sure you inspect these areas: 1. Skin with emphasis atskin overlaps and under access panels. 2. Rear spar upper and lower caps. 3. Rearspar web. NOTE: Corrosion Preventionand Control ProgramInspection item (baselineinterval, refer to Section 2A-30-00 for additional inspection information).

Every 60 months 6

510,520,610,620


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REVISIONSTATUS


0

Vertical stabilizer structure. Make sure you inspect these areas: 1. Forward sparattachment to tailcone bulkhead. 2. Aft spar attachment to tailcone bulkhead.3. Front and rear spars. 4. Rear spar rudder hinges. NOTE: Corrosion Prevention andControl Program Inspection item (baseline interval, refer to Section2A-30-00 for additional inspection information)


0

Nose gear axle assembly. Make sure you inspect these areas: 1. Nose gear axle andattach bolt. 2. Wheel halves. NOTE: Corrosion Prevention and Control ProgramInspection item (baseline interval, refer to Section 2A-30-00 for additional inspectioninformation). NOTE: Disassemble the nose gear strut to get access. NOTE: Do notapply LPS-3 Heavy-Duty Rust Inhibitor to the sliding surfaces of the oleo strut.NOTE: Coordinate with tire change.


0

Horizontal stabilizer and elevator structure. Make sure you inspect these areas: 1.Stabilizer attachment to the tailcone bulkhead, 2. Front and rear spars. 3. Elevatorstructure. 4. Elevator hinges, hinge bearings, and hinge fittings. NOTE: CorrosionPrevention and Control Program Inspection item (baseline interval, refer to Section 2A-30-00 for additional inspection information).

Every 60 months 6 330,340

0

Elevator trim system. 1. Inspect elevator trim pulley brackets and actuator supportbrackets. 2. Inspect pulleys, attaching structure, and fasteners. Refer to Section 2A-14-02, Supplemental Inspection Document 27-30-01, for inspection procedures.Coordinate with actuator overhaul.

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

7330,340

0

Flaps. 1. Check flap travel cable tension, and travel time. 2. Check flap cable system,control cables, and pulleys, in accordance with the f light cableinspection procedures in Section 2A-20-01, ExpandedMaintenance, Control Cables.

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

8210,510,610

0

Aileron. 1. Check aileron travel and cable tension. 2. Check aileron cable system,

control cables, and pulleys, in accordance with the f light cable inspection procedures inSection 2A-20-01, Expanded Maintenance, Control Cables.

Initial: 100 hours;

Repeat: every 600 hours or 12months, whichever occurs first 8

210,510

520,610,620

0Elevator. 1. Check elevator travel and cable tension. 2. Check elevator cable system,control cables, and pulleys, in accordance with the f light cable inspection procedures inSection 2A-20-01, Expanded Maintenance, Control Cables.

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

19210,

310,330340


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REVISIONSTATUS


0 Elevator Trim. 1. Check elevator trim travel and cable tension. 2. Check elevator trimcable 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

8 210,310,330340

0Rudder. 1. Check rudder travel and cable tension. 2. Check rudder cable system,control cables, and pulleys, in accordance with the f light cable inspection procedures inSection 2A-20-01, Expanded Maintenance, Control Cables.

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

8210,310,320

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

9 210

0Inspect horizontal stabilizer and elevator, including spars, ribs, hinge bolts, hingebearing, attachments and torque tube. Refer to Section 2A-14-19, Supplemental

Inspection Document 55-10-01, for inspection procedure.

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

whichever occurs first

9 330,340

0Inspect horizontal stabilizer and elevator, including spars, ribs, hinge bolts, hingebearings, and attach fittings. Refer to Section 2A-14-20, Supplemental InspectionDocument 55-10-02, for inspection procedures.


9 330,340

0Inspect vertical stabilizer and rudder, including spars, ribs, hinge bolts, hinge bearing,and attach fittings. Refer to Section 2A-14-22, Supplemental Inspection Document 55-30-01, for inspection procedure.


9 320

0Inspect nose landing gear torque links, bolts, bushings, and nose landing gear fork.Refer to Section 2A-14-07, Supplemental Inspection Document 32-20-01, forinspection procedure.

Initial: 3,000 hours or 5 years,whichever occurs first; Repeat:3,000 hours or 5 years, whichever

occurs first

10 720

0 Inspect seat rails for corrosion. Refer to Section 2A-14-18, Supplemental InspectionDocument 53-47-01, for inspection procedure.

Initial: 10 years;Repeat: 5 years

11 210


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REVISIONSTATUS


0Inspect nose landing gear lower trunnion fitting.Refer to Section 2A-14-08, Supplemental InspectionDocument 32-20-02, for inspection procedure.

Initial: 2,000 hours or 10 years,whichever occurs first; Repeat:1,000 hours or 1 year, whicheveroccurs first

12 720

0Inspect firewall. 1. Inspect around exhaust hanger brackets for cracks. 2. Inspect websand around stiffeners for cracks. Refer to Section 2A-14-14, Supplemental InspectionDocument 53-12-03, for inspection procedures.

Initial: 3,000 hours or 5 years,whichever occurs first; Repeat:500 hours or 1 year, whicheveroccursfirst

13 120

0This inspection is for mild or moderate corrosion environment. Inspect main landinggear spring for rust or damage to finish. Refer to Section 2A-14-04, SupplementalInspection Document 32-13-01, for inspection procedure.


14730,740

0

This inspection is for mild or moderate corrosion environment. Inspect the carry-thru

spar, upper portions of door posts, and wing attachments. Refer to Section 2A-14-09,Supplemental Inspection Document 53-11-01, for inspection procedure.

Initial: 20 years;Repeat: 10 years 14

210

0This inspection is for mild or moderate corrosion environment. Inspect the cantileveredcarry-thru spar, and wing attachments. Refer to Section 2A-14-10, SupplementalInspection Document 53-11-02, for inspection procedure.


14 120

0This inspection is for mild or moderate corrosion environment. Inspect wing forcorrosion and missing or loose fasteners. Refer to Section 2A-14-25, SupplementalInspection Document 57-11-03, for inspection procedure.


14510,610

0This inspection is for mild or moderate corrosion environment. Inspect the flap tracksfor corrosion. Refer to Section 2A-14-31, Supplemental Inspection Document 57-53-01,

for inspection procedure. (For Model 210.)


14510,610

0This inspection is for mild or moderate corrosion environment. Inspect the flap tracksfor corrosion. Refer to Section 2A-14-32, Supplemental Inspection Document 57-53-02,for inspection procedure. (For Model 206.)


14510,610


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REVISIONSTATUS


0This inspection is for mild or moderate corrosion environment. Cabin interior skinpanels. Inspect the cabin interior skin panels, frames, and stringers.Refer to Section 2A-14-15, Supplemental Inspection Document 53-30-01, forinspection procedure.


15 210

0This inspection is for mild or moderate corrosion environment. Inspect wing root rib.Refer to Section 2A-14-27, Supplemental Inspection Document 57-12-01, forinspection procedure.


16510,610

0This inspection is for severe corrosion environment. Inspect main landing gear springfor rust or damage to f inish. Refer to Section 2A-14-04, Supplemental InspectionDocument 32-13-01, for inspection procedure.


17730,740

0This inspection is for severe corrosion environment. Inspect wing for corrosion andmissing or loose fasteners. Refer to Section 2A-14-25, Supplemental InspectionDocument 57-11-03, for inspection procedure.


17510,520610,620

0This inspection is for severe usage environment. Inspect wing splice joint. Refer toSection 2A-14-26, Supplemental Inspection Document 57-11-04, for inspectionprocedure.

nitial: 10 years;Repeat: 5 years

17510,610

0This inspection is for severe corrosion environment. Inspect flap tracks for corrosion.Refer to Section 2A-14-31, Supplemental Inspection Document 57-53-01, forinspection procedure. (For Model 210.)


17510,610

0This inspection is for severe corrosion environment. Inspect flap tracks for corrosion.Refer to Section 2A-14-32, Supplemental Inspection Document 57-53-02, forinspection procedure. (For Model 206.)


17510,610

0

This inspection is for severe corrosion environment. Inspect the carry-thru spar, upper

portions of door posts, and wing attachments. Refer to Section 2A-14-09,Supplemental Inspection Document 53-11-01, for inspection procedure.

Initial: 10 years;Repeat: 3 years 18 210

This inspection is for severe corrosion environment. Inspect the cantilevered wingcarry-thru spar, and wing attachments. Refer to Section 2A-14-10, SupplementalInspection Document 53-11-02, for inspection procedure.


18 210


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REVISIONSTATUS


0 This inspection is for severe corrosion environment. Inspect the cabin interior skinpanels, frames, and stringers for corrosion. Refer to Section 2A-14-15, SupplementalInspection Document 53-30-01, for inspection procedure.


18 210

0This inspection is for severe corrosion environment. Inspect wing root rib. Refer toSection 2A-14-27, Supplemental Inspection Document 57-12-01, for inspectionprocedure.


19510,610

0 Engine mount structure. Inspect the tunnel structure side walls. Refer to Section 2A-14-33, Supplemental Inspection Document 71-20-01, for inspection procedure.

Initial: 10,000 hours or 20 years,whichever occurs first; Repeat:engine overhaul

20 120

0This inspection is for typical usage environment. Inspect the cantilevered wing carry-thru spar, and wing attachments. Refer to Section 2A-14-11, Supplemental InspectionDocument 53-11-03, for inspection procedure.


occurs first

21 210

0This inspection is for typical usage environment. Inspect wing for corrosion and missingor loose fasteners. Refer to Section 2A-14-24, Supplemental Inspection Document 57-11-02, for inspection procedure.

Initial: 12,000 hours or 20 years,whichever occurs first; Repeat:3,000 hours or 10 years,whichever occurs first

22

510,520,610,620

0This inspection is for typical usage environment. Inspect front spar and attachments.Refer to Section 2A-14-28, Supplemental Inspection Document57-30-01, for inspection procedure.

Initial: 12,000 hours or 20 years,whichever occursfirst; Repeat:3,000 hours or 10 years,whichever occurs first

22510,610

0Main landing gear saddle. Inspect main landing gear saddle for cracks. Refer toSection 2A-14-06, supplemental Inspection Document 32-13-03, for inspectionprocedure.

Initial: 1,000 hours;Repeat: 100 hours

23 210

0Tailcone bulkhead and vertical stabilizer attachment. 1. Inspect tailcone bulkhead forcracks. 2. Inspect vertical stabilizer attachment for cracks. Refer to Section 2A-14-17,Supplemental Inspection Document 53-42-01, for inspection procedure.

Initial: 1,000 hours;Repeat: 100 hours 23 510,610

0This inspection is for severe usage environment. Inspect the cantilevered carry-thruspar, and wing attachments. Refer to Section 2A-14-11, Supplemental InspectionDocument 53-11-03, for inspection procedure.

Initial: 6,000 hours or 3 years,whichever occurs first; Repeat:500 hours or 1 year, whicheveroccurs first

24 210


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REVISIONSTATUS


0This inspection is for severe usage environment. Inspect lower forward doorposts andstrut fittings. Refer to Section 2A-14-16, Supplemental Inspection Document 53-30-02,for inspection procedure.


30 210

0

This inspection is for severe usage environment. Inspect wing structure and wingattachment to fuselage including working rivets. Inspect flap actuator support structure.Refer to Section 2A-14-23, Supplemental Inspection Document 57-11-01, forinspection procedure.


25

510,520,610,620

0This inspection is for severe usage environment. Inspect cantilever wing structure.Refer to Section 2A-14-24, Supplemental Inspection Document 57-11-02, forinspection procedure.

Initial: 6,000 hours or10 years,whichever occurs first; Repeat:1,000 hours or 3 years, whicheveroccurs first

25

510,520,610,620

0 This inspection is for severe usage environment. Inspect front spar and attachments.Refer to Section 2A-14-28, Supplemental Inspection Document 57-30-01, forinspection procedure

Initial: 6,000 hours or 10 years,

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

25 510,610

0 Inspect main landing gear retraction system. Refer to Section 2A-14-03, SupplementalInspection Document 32-10-01, for inspection procedure.


26 210

0Inspect elevator with foam in trailing edge and elevator trim tab that is foam filled forsigns of corrosion, cracking or deterioration. Refer to Section 2A-14-21, SupplementalInspection Document 55-10-03, for inspection procedures.


27330,340

0 Inspect main landing gear fittings. Refer to Section 2A-14-05, Supplemental InspectionDocument 32-13-02, for inspection procedures.



28 330,340

0This inspection is for typical usage environment. Inspect the wing strut fitting andattachment of fitting to the bulkhead. Refer to Section 2A-14-16, SupplementalInspection Document 53-30-02, for inspection procedure.


29 210


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REVISIONSTATUS


0This inspection is for typical usage environment. Inspect wing structure and wingattachment to fuselage including working rivets. Inspect flap actuator support structure.Refer to Section 2A-14-23, Supplemental Inspection Document 57-11-01, forinspection procedure.

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

29510,520,610,620

0This inspection is for typical usage environment. Inspect strut and wing strutattachments. Refer to Section 2A-14-29, Supplemental Inspection Document 57-40-01,for inspection procedure.


29510,610

0This inspection is for severe usage environment. Inspect strut and wing strutattachments. Refer to Section 2A-14-29, Supplemental InspectionDocument 57-40-01, for inspection procedure.


occurs first

3510,610,

0 Inspect lower forward doorposts and strut fittings. Refer to Section 2A-14-13,Supplemental Inspection Document 53-12-02, for inspection procedure.


31 210

0 Inspect fuselage upper and lower forward doorposts. Refer to Section 2A-14-12,Supplemental Inspection Document 53-12-01, for inspection procedures.


31 210

0 Inspect aileron support structure. Refer to Section 2A-14-30, Supplemental InspectionDocument 57-51-01, for inspection procedures.



31 520,620


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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 3,000 hoursof operation or 5 years, whichever occurs first. The inspection is to be repeated every 500hours of operation or 1 year, whichever occurs first, after the initial inspection has beenaccomplished.

14

Supplemental Inspection Document items that are to be examined after the first 20 years.

The inspection is to be repeated every 10 years after the initial inspection has beenaccomplished, for airplanes operating in a mild or moderate corrosion environment.

15Supplemental Inspection Document items that are to be examined after the first 20 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.

16Supplemental Inspection Document items that are to be examined after the first 5 years. Theinspection is to be repeated every 5 years after the initial inspection has been accomplished,

for airplanes operating in a mild or moderate corrosion environment.

17Supplemental 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.

18Supplemental Inspection Document items that are to be examined after the first 10 years.The inspection is to be repeated every 3 years after the initial inspection has beenaccomplished, for airplanes operating in a severe corrosion environment.


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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 6,000 hoursof operation or 10 years, whichever occurs first. The inspection is to be repeated every 1,000hours of operation or 3 years, whichever occurs first, after the initial inspection has beenaccomplished, for airplanes operating in a severe usage environment.

26

Supplemental Inspection Document items that are to be examined after the first 6,000 hours

of operation or 10 years, whichever occurs first. The inspection is to be repeated every 1,000hours of operation or 3 years, whichever occurs first, after the initial inspection has beenaccomplished.

27Supplemental Inspection Document items that are to be examined after the first 5 years. Theinspection is to be repeated every 5 years after the initial inspection has been accomplished.

28

Supplemental Inspection Document items that are to be examined after the first 3,000 hoursof operation or 5 years, whichever occurs first. The inspection is to be repeated every 1,000

hours of operation or 5 years, whichever occurs first, after the initial inspection has beenaccomplished.

29

Supplemental Inspection Document items that are to be examined after the first 12,000 hoursof operation or 20 years, whichever occurs first. The inspection is to be repeated every 2,000hours of operation or 10 years, whichever occurs first, after the initial inspection has beenaccomplished, for airplanes operating in a typical usage environment.


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APENDICE CDEL PMA SECCION D

SECCION

D


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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 are completed.2. General Inspection Criteria

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

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

C. Do a preflight inspection after these inspections are completed to make sure all the required items


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Date: _______________



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 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 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 that


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Date: _______________



Total Time: _______________

1. Description

A. Operation 3 gives Corrosion Prevention and Control Program Inspections (Baseline Program) itemsthat are to be examined every 24 months. Refer to Section 2A-30-00, Corrosion Prevention andControl Program, for additional information concerning repeat Corrosion Program Inspectionintervals.


C. The right portion of each page gives space for the mechanic's and inspector's initials and remarks. Acopy of these pages can be used as a checklist when these inspections are completed.

2. General Inspection Criteria



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D.3.1.INSPECTION OPERATION 3 (CONT.)

TASK ZONE MECH INSP REMARKS

Rudder attachments. Make sure you inspectthese areas: 1. Hinge brackets. 2. Hinge bolts.

3. Hinge bearings.NOTE: Corrosion Prevention and ControlInspection Item (baseline interval, refer toSection 2A-30-00 for additional inspectioninformation).NOTE: Do not apply LPS-3 Heavy Duty RustInhibitor on hinge bearing.

320

Rudder structure. Make sure you inspect theseareas: 1. Skin. 2. Forward and aft spars at

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

320

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


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Date: _______________



Total Time: _______________

1. Description





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

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


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D.4.1.

INSPECTION OPERATION 4 (CONT.)


Nose gear trunnion, torque link assembly,and

nose gear fork. Make sure you inspect theseareas: 1. Nose gear trunnion upper and lowerinner bore surface and bearing. 2. Torque linkbolt and attach pin inner bore surface. 3. Nosegear fork lug inner bore surface. NOTE:Corrosion Prevention and Control InspectionItem (baseline interval,refer to Section 2A-30-00 for additionalinspection information).

720

Nose landing gear outer barrel assembly. Makesure you inspect these areas: 1. Outer barrelassembly.2. Upper strut end and lower collar assembly.NOTE: Corrosion Prevention and ControlInspection Item (baseline interval, refer toSection 2A-30-00 for additional inspectioninformation). NOTE: do not apply LPS-3 Heavy-Duty Rust Inhibitor to the sliding surfaces of theoleo strut.

720


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D.5.

INSPECTION OPERATION 5

Date: _______________



Total Time: _______________

1. Description








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Date: _______________



Total Time: _______________1. Description






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


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D.6.1.

INSPECTION OPERATION 6 (CONT.)


Areas of the cabin structure. Make sure youinspect these areas: 1. Cabin door forward andaft frames. 2. Window frames with emphasis atstringers and channel assemblies from aft ofdoor frame to aft bulkhead. 3. Seat attachment

structure. 4. Aft Cabin Bulkhead. NOTE:Corrosion Prevention and Control ProgramInspection Item (baseline interval, refer toSection 2A-30-00 for additional inspectioninformation).

210

Wing structure internal. Make sure you inspectthese areas: 1. Wing upper and lower sparcaps. 2. Wing attach spar fittings. 3. Wing lowerskins. NOTE: Corrosion Prevention and Control

Program Inspection Item (baseline interval,refer to Section 2A-30-00 for additionalinspection information).

510,520,610,

620

Wing structure external. Make sure you inspectthese areas: 1. Skin with emphasis at skinoverlaps and under access panels. 2. Rear sparupper and lower caps. 3. Rear spar web.NOTE: Corrosion Prevention and ControlProgram Inspection Item (baseline interval,

510,520,610,620


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Date: _______________




A. Operation 7 gives Supplemental Inspection Document items that are to be examined every 1,000hours.




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 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: _______________




A. Operation 8 gives Supplemental Inspection Document items that are to be examined at the first 100hours, then every 600 hours or 12 months, whichever occurs first, thereafter.







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D.8.1INSPECTION OPERATION 8


Flaps. 1. Check flap travel cable tension, andtravel time. 2. Check flap cable system, controlcables, and pulleys, in accordance with the

flight cable inspection procedures in Section2A-20-01, Expanded Maintenance, ControlCables.

210,510,

610

Aileron. 1. Check aileron travel and cabletension. 2. Check aileron cable system, controlcables, and pulleys, in accordance with theflight cable inspection procedures in Section2A-20-01, Expanded Maintenance, ControlCables.

210,510,520,610620



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Date: _______________




A. Operation 9 gives Supplemental Inspection Document items that are to be examined after the first10,000 hours of operation or 20 years, whichever occurs first. The inspection is to be repeatedevery 3,000 hours of operation or 5 years, whichever occurs first, after the initial inspection hasbeen accomplished.

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. Acopy of these pages can be used as a checklist when these inspections are completed.




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Date: _______________




A. Operation 10 gives Supplemental Inspection Document items that are to be examined after the first3,000 hours of operation or 5 years, whichever occurs first. The inspection is to be repeated every3,000 hours of operation or 5 years, whichever occurs first, after the initial inspection has beenaccomplished.







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Date: _______________




A. Operation 11 gives Supplemental Inspection Document items that are to be examined after the first10 years. The inspection is to be repeated every 5 years after the initial inspection has beenaccomplished.


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 are completed.





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Date: _______________



Total Time: _______________

1. Description

A. Operation 12 gives Supplemental Inspection Document items that are to be examined after the first2,000 hours of operation or 10 years, whichever occurs first. The inspection is to be repeated every1,000 hours of operation or 1 year, whichever occurs first, after the initial inspection has beenaccomplished.







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Date: _______________



Total Time: _______________

1. Description

A. Operation 13 gives Supplemental Inspection Document items that are to be examined after the first3,000 hours of operation or 5 years, whichever occurs first. The inspection is to be repeated every500 hours of operation or 1 year, whichever occurs first, after the initial inspection has beenaccomplished.






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Date: _______________



Total Time: _______________

1. Description

A. Operation 14 gives Supplemental Inspection Document items that are to be examined after the first20 years. The inspection is to be repeated every 10 years after the initial inspection has beenaccomplished, for airplanes operating in a mild or moderate corrosion environment.







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D.14.1INSPECTION OPERATION 14


This inspection is for typical usageenvironment. Inspect wing splice joint. Refer to

Section 2A-14-26, Supplemental InspectionDocument 57-11-04, for inspection procedure.

510,

610

This inspection is for mild or moderatecorrosion environment. Inspect the flap tracksfor corrosion. Refer to Section 2A-14-31,Supplemental Inspection Document 57-53-01,for inspection procedure. (For Model 210.)

510,610

This inspection is for mild or moderate

corrosion environment. Inspect the flap tracksfor corrosion. Refer to Section 2A-14-32,Supplemental Inspection Document 57-53-02,for inspection procedure. (For Model 206.)

510,610



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Date: _______________



Total Time: _______________

1. Description







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Date: _______________



Total Time: _______________

1. Description








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D.17. INSPECTION OPERATION 17

Date: _______________




A. Operation 17 gives Supplemental Inspection Document items that are to be examined after the first10 years. The inspection is to be repeated every 5 years after the initial inspection has beenaccomplished, for airplanes operating in a severe corrosion environment.


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


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 are used to findapparent conditions which can need more maintenance.

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


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Date: _______________



Total Time: _______________

1. Description








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Date: _______________



Total Time: _______________

1. Description








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Date: _______________



Total Time: _______________

1. Description

A. Operation 20 gives Supplemental Inspection Document items that are to be examined after the first10,000 hours of operation or 20 years, whichever occurs first. The inspection is to be repeated atengine overhaul.







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Date: _______________



Total Time: _______________

1. Description

A. Operation 21 gives Supplemental Inspection Document items that are to be examined after 12,000hours or 20 years, whichever occurs first. The inspection is to be repeated every 1,000 hours or 3years, whichever occurs first, after the initial inspection has been accomplished, for airplanesoperating in a typical usage environment.







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Date: _______________



Total Time: _______________

1. Description

A. Operation 22 gives Supplemental Inspection Document items that are to be examined after 12,000hours or 20 years, whichever occurs first. The inspection is to be repeated every 3,000 hours or 10years, whichever occurs first, after the initial inspection has been accomplished, for airplanesoperating in a typical usage environment.







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Date: _______________



Total Time: _______________

1. Description

A. Operation 23 gives Supplemental Inspection Document items that are to be examined after 1,000hours of operation. The inspection is to be repeated every 100 hours after the initial inspection hasbeen accomplished

.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.




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


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Date: _______________



Total Time: _______________

1. Description

A. Operation 24 gives Supplemental Inspection Document items that are to be examined after the first6,000 hours of operation or 3 years, whichever occurs first. The inspection is to be repeated every500 hours of operation or 1 year, whichever occurs first, after the initial inspection has beenaccomplished, for airplanes operating in a severe usage environment.






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Date: _______________



Total Time: _______________

1. Description

A. Operation 25 gives Supplemental Inspection Document items that are to be examined after the first6,000 hours of operation or 10 years, whichever occurs first. The inspection is to be repeated every

1,000 hours of operation or 3 years, whichever occurs first, after the initial inspection has beenaccomplished, for airplanes operating in a severe usage environment.






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D.26.

INSPECTION OPERATION 26

Date: _______________



Total Time: _______________

1. Description








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Date: _______________



Total Time: _______________

1. Description

A. Operation 27 gives Supplemental Inspection Document items that are to be examined after the first5 years. The inspection is to be repeated every 5 years after the initial inspection has beenaccomplished.







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Date: _______________



Total Time: _______________

1. Description







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Date: _______________



Total Time: _______________

1. Description

A. Operation 29 gives Supplemental Inspection Document items that are to be examined after the first12,000 hours of operation or 20 years, whichever occurs first. The inspection is to be repeatedevery 2,000 hours of operation or 10 years, whichever occurs first, after the initial inspection hasbeen accomplished, for airplanes operating in a typical usage environment.


Frequently, tasks give more information about each required inspection.C. The right portion of e