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EDITADO POR: MELQUIADES CHAVEZ GALDOS Sign up to vote on this title
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PROGRAMA DE
MANTENIMIENTO CESSNA MODEL
172
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
INDICE
INDICE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
INDICE CONTENIDO INDICE PROCEDIMIENTO PARA LA REVISION DEL PMA LISTA DE PAGINAS EFECTIVAS REGISTRO DE REVISIONES CAPITULO I (Procedimientos de Inspección) CAPITULO II ( Formatos de Inspección) CAPITULO III (Registro de Overhaul \ Reemplazos) ANEXO “A” CONTINUED AIRWORTHINESS PROGRAM (CAP),
PRESENTADO POR SEPARADO. SUPPLEMENTAL L INSPECTION DOCUMENT (SID) ANEXO”B” SUPPLEMENTA PRESENTADO POR SEPARADO.
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PARA LA AERONAVE CESSNA 172B
PROCEDIMIENTOS PARA LA REVISION DEL PMA
PROCEDIMIENTO PARA LA REVISION DEL PMA Sign up to vote on this title
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PROGRAMA DE MANTENIMIENTO APR
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PARA LA AERONAVE CESSNA 172B
PROCEDIMIENTOS PARA LA REVISION DEL PMA PROCEDIMIENTOS PARA LAS REVISONES DEL PMA CARATULA DEL PROGRAMA Es la primera página sin numeración numeración de este Programa con el el propósito su identificación. CARATULA DE ASIGNACION DEL PROGRAMA
Es la Segunda Pagina sin numeración de este Programa donde se re Numero del Manual asignado, el Número de Revisión actual y el no departamento, entidad o a quien es asignado el presente el manual. NUMERO DE CONTROL Y LISTA DE DISTRIBUCION DEL PROGRAMA
Los Programa asignados asignados serán numerados numerados correlativamente correlativamente con un nú control. El departamento departamento de Control de Mantenimiento mantendrá un Asignación de los Manuales en la que incluirá el número de control y las que se han incorporado. 01 02 03 04 05 06 07
Dirección General de Aeroná Aeronáutica utica Civil (D.G.A.C.) (CD) Director de Mantenimiento Departamento de Control de Mantenimiento Estación de Línea Nazca Línea Ica Departamento de Instrucción y Publicaciones TMA/OMA – Contratado (CD) Sign up to vote on this title
PROCEDIMIENTOS PARA LAS REVISIONES Useful Not useful
En este párrafo se establecen los procedimientos para que el PMA (Pro
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PARA LA AERONAVE CESSNA 172B
PROCEDIMIENTOS PARA LA REVISION DEL PMA
El responsable de la revisión remitirá al IPM de Travel Air, a través de partes del MTC, una carta de presentación con el logo tipo de la comp firma del Director Dir ector de Mantenimiento junto con un ejemplar de las páginas r y dos copias de la lista de páginas efectivas.
Una vez aprobada la revisión, con la refrenda del IPM en la lista de las efectivas, el Departamento de Control de Mantenimiento sacará copias su de las revisiones para su distribución a las diferentes áreas. REGISTRO DE ACTUALIZACIONES
El Departamento de Control de Mantenimiento, mantendrá un registro d enmiendas y revisiones que contenga cada número de manual y a que p o departamento hubiera sido asignado que incluirá también la fecha de inserción y fecha de vigente de las revisiones. . REVISIONES TEMPORA TEMPORALES LES
Debido a que este manual será periódicamente adecuado, modificado, re corregido, se insertaran revisiones temporales en hoja A4 color amaril
título “REVISION TEMPORAL 01, 02, 03 etc.” El cual tendrá una durac
meses desde su publicación, hasta que se remita a la DGAC la correspondiente para su aprobación.
Las Revisiones temporales deben ser firmadas y aprobadas por el Dir Mantenimiento.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
LISTA DE PAGINAS EFECTIVAS
LISTA DE PÁGINAS EFECTIVAS
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
LISTA DE PAGINAS EFECTIVAS LISTA DE PÁGINAS EFECTIVAS Nº DE PAGINA i-0 i-1 ii-0 ii-1 ii-2 iii-0 iii-1 iii-2 iv-0 iv-1 I-0 I-1 I-2 I-3 I-4 I-5 I-6 I-7 I-8 I-9 I-10 I-11 I-12 II-0 II-1 II-2 II-3 II-4 II-5 II-6
Nº DE REVISION FECHA EFECTIVA R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 Sign up to vote on this title R-21 30-JUNIO-2012 Useful Not useful R-21 30-JUNIO-2012 R-21 30-JUNIO-2012
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
LISTA DE PAGINAS EFECTIVAS Continuacion
LISTA DE PÁGINAS EFECTIVAS Nº DE PAGINA II-16 II-17 II-18 II-19 II-20 II-21 II-22 II-23 II-24 II-25 II-26 II-27 II-28 II-29 II-30 II-31 II-32 II-33 II-34 II-35 II-36 II-37 II-38 III-0 III-1 III-2 III-3 III-4 III-5
Nº DE REVISION FECHA EFECTIVA R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 R-21 30-JUNIO-2012 Sign up to vote on30-JUNIO-2012 this title R-21 useful R-21 30-JUNIO-2012 Useful Not R-21 30-JUNIO-2012 R-21 30-JUNIO-2012
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
REGISTRO DE REVISIONES
REGISTRO DE REVISIONES
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
REGISTRO DE REVISIONES REGISTRO DE REVISIONES REVISIÓN
FECHA REVISIÓN
ELABORADA POR
FECHA APROBACION
INSERTA
ORIGINAL
26 Set 2000
C. Palacín C.
26 Oct 2000
A. Coca
R-1
10 Ene 2002
L. Chicoma F.
18 Ene 2002
A. Coca
R-2
18 Abr 2002
C. Palacín C.
05 Jun 2002
A. Coca
R-3
26 Mar 2003
J. Ventura A.
05 Jun 2003
A. Coca
R-4
30 Jun 2004
A.Coca Tello
26 Jul 2004
A. Coca
R-5
30 Ago 2004
A. Coca Tello
14 Set 2004
A. Coca
R-6
02 Ene 2005
A. Coca Tello
17 Feb 2005
A. Coca
R-7
30 Mar 2005
A. Coca Tello
29 Abr 2005
A. Coca
R-8
11 Jul 2005
A. Coca Tello
18 Ago 2005
A. Coca
R-9
02 Set 2005
A. Coca Tello
11 Oct 2005
A. Coca
R-10
10 Nov 2006
A. Coca Tello
27 Dic 2006
A. Coca
R-11
27 Ago 2007
A. Coca Tello
20 Set 2007
A. Coca
R-12
15 Abr 2008
A. Coca Tello
15 May 2008
E.Mendo
R-13
26 Jul 2008
A. Coca Tello
19 Ago 2008
E.Mendo
R-14
10 Nov 2008
A. Coca Tello
04 Dic 2008
E.Mendo
R-15
26 Mar 2009
A. Coca Tello
14 Abr 2009
E.Mendo
R-16
12 Ago 2009
A. Coca Tello
28 Set 2009
E.Mendo
R-17 R-18 Reedición R-19
15 Mar 2010
A. Coca Tello
07 May 2010
E.Mendo
10 Ago 2010
Carlos Palacin C.
18 Nov 2010
Carlos Palacin C.
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30 Set 2010
E.Mendo
07 Feb 2011
V. Lleren
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION
CAPITULO I PROCEDIMIENTOS DE INSPECCION Sign up to vote on this title
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMI PROCEDIMIENTOS ENTOS DE INSPECCION 1.
INFORMACION GENERAL:
Travel Air EIRL, posee un Permiso de Operaciones de Transporte Aéreo No Regular, Transporte Aéreo Aéreo Especial Turístico y de Observación, con Operaciones en el Aeródromo Las Dunas de Ia ciudad de Ica y una Es
Línea en el Aeródromo Aeródromo “María Reiche” de la ciudad de Nazca. Las Las t
mantenimiento serán efectuadas por un Taller de Mantenimiento Aer (TMA) u Organización de Mantenimiento Aeronáutico (OMA) aprobad autoridad Aeronáutica, para tal efecto ambas partes celebraran un co mantenimiento.
El presente present e manual contiene co ntiene la información y los procedimientos procedimientos necesa el desarrollo de las labores de mantenimiento de la aeronave Cessna S Modelo 172 B que opera la Compañía.
Es de suma importancia resaltar que la aeronave Cessna 172B se e certificada bajo el Type Certificate Certificate Nº 3A12.
2.
MARCO DE REFERENCIA:
Travel Air E.I.R.L con Permiso de Operaciones No. 28, en su calidad de exp Transporte Aéreo Nacional No Regular, Transporte Aéreo Especial Turís Observación, Observaci ón, reconoce recono ce como autoridad autor idad a la Dirección General de Aeronáutica lo que la confección del presente presente Manual ha sido realizada de de acuerdo con e de Servicio P/N D2070-3D20 70-3-13, 13, Boletines Bolet ines del fabricante, la Ley 27261 y su reglam como las Directivas DGAC, NTC´s, RAP´s, y las recomendaciones dadas e 9389-AN/919 de la OACI,
3.
DISTRIBUCION Y APLICACION APLICACION DE ESTE PROGRAMA PROGRAMA Refiérase a la página ii-1 de este manual
Sign up to votecomo on this title La Autoridad que aprueba el presente P.M.A. así sus modifica actualizaciones, es la DGAC. Useful Not useful
4.
RESERVADO
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMI PROCEDIMIENTOS ENTOS DE INSPECCION
El Programa de Mantenimiento Aprobado (P.M.A.) (P. M.A.) se ha desarrollado con la de dar cumplimiento a lo dispuesto por: a) b) c) d)
7.
Ley de Aeronáutica Civil Nº 27261, su reglamento y disp vigentes. RAP (Regulaciones Aeronáuticas del Perú) Recomendaciones OACI Oficios Circulares DGAC
PROGRAMA DE MANTENIMIENTO MANTENIMIENT O APROBADO (P.M.A.)
Travel Air E.I.R.L basado en las recomendaciones de Cessna y la experiencia pr compañia, ha desarrollado el Programa de Mantenimiento Aprobado Aprobado (P.M.A.) (P.M.A.) q en una serie de inspecciones del Avión, nominadas de 25, 50, 75,100 horas, Insp Especiales Especial es de 1000 horas, hor as, y RII. Así A sí como también el cumplimiento de Boletines d y Directivas de Aeronavegabilidad Aeronavegab ilidad,, Normas Técnicas Técnic as Complementarias y Normas Extraordinarias aplicables. Adicionalmente a la Guía de Inspección se dará estricto cumplimiento a las Servicio y Lubricación proporcionadas por el fabricante.
Asimismo, en el anexo “A” se encuentra el Programa de Aeronaveg
Continuada (CAP) desarrollado por TRAVEL AIR AIR E.I.R.L. en base al Manual publicado por Cessna Aircraft Company, como un complemento al Prog
Mantenimiento Aprobado por la DGAC, y en el Anexo “B” se encu
Supplemental Inspection Document (SID) desarrollado por TRAVEL AIR E base al Manual D138-1-13 Seccion 2ATR7 publicado por Cessna Aircraft C como un complemento al Programa de Mantenimiento Aprobado Aprobado por la DG 8.
FASES DE INSPECCIONES
En el Capitulo II de este programa se incluye unas guías de inspección de 25, 50 horas e Inspecciones Especiales de 1000 horas elaboradas por Travel Air EIRL e Ground handling/Servicing Inspection del Manual de Servicio del Fabricante. Los Inspección Especial que requieran Inspección cada 1000 horas, seráncumplid Sign up to vote on this title su cumplimiento de ac decima Inspección de 100 horas o cuando corresponda Useful Not useful P/N D138 las recomendaciones descritas en el Manual de Servicio delfabricante programación programaci ón para el cumplimiento de todas las tareas descritas anteriorme cargo del Departamento de Control de mantenimiento bajo la supervisión de
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMI PROCEDIMIENTOS ENTOS DE INSPECCION
identificadas por números y letras, los cuales deben ser verificados en los i de 25, 50, 75 y 100 horas, según corresponda la acción de mantenimiento. a) FASE DE 25 HORAS.
Esta fase de inspección esta detallada en la Guía de Inspección de 25 h deberá cumplirse a intervalos de 25 horas de operación después de una insp de 100 horas, mas m as las Inspecciones Especiales (SPC) e Items RII de ser requ
b) FASE DE 50 HORAS.
Esta fase de inspección esta detallada detal lada en la Guía de Inspección de 50 horas cumplirse a intervalos de 50 horas de operación, después de una Inspecció horas, mas las Inspecciones Especiales (SPC) e Items RII de ser requerida
c) FASE DE 75 HORAS: Esta fase de inspección esta detallada en la Guía de Inspección de 75 horas todos los detalles de la Guía de Inspección de 25 horas, y deberá cump después de una Inspección de 50 Horas, mas las Inspecciones Especiales Items RII de ser requeridas.
d) FASE DE 100 HORAS: Esta fase de inspección esta detallada en la Guía de Inspección de 100 horas todos los detalles de la Guía de Inspección de 25, 50, y 75 horas y deberá cu intervalos de 100 horas de operación, mas las Inspecciones Especiales (SP de Inspeccion Requerida (RII).
e) INSPECCIONES ESPECIALES DE 1000 HORAS: Esta inspección estará anexada en la decima Inspeccion de 100 horas y se c intervalos de 1000 horas, asimismo se cumplirá con la Inspeccion de cor acuerdo con las recomendaciones del fabricante.
Adicionalmente a cada Fase de Inspección se dará cumplimiento estri requerimientos de las Cartas de Servicio y Lubricación detallada Sign up to vote on this title por el fa Directivas de Aeronavegabilidad y BoletinesdeUseful Servicos aplicables a la ae useful Not componentes.
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMI PROCEDIMIENTOS ENTOS DE INSPECCION
El mantenimiento será ejecutado por una organización de mantenimiento a (OMA) de acuerdo a la RAP 145. (135.1410 ( 135.1410 (a)(3). Los datos registrados por la tripulación en el registro técnico de vuelo (RT base fundamental para la programación de los eventos de mantenimiento los reportes de discrepancias surgidas durante un vuelo.
Basados en esta información el Departamento de Control de Mantenimiento estas horas de vuelo al sistema computarizado a fin de tener contro programación de cada una de las tareas de mantenimiento.
El encargado encarg ado del Departamen De partamento to del Control de Mantenimiento solicitara med carta y/o orden de trabajo con 10 horas de anticipación el cumplimiento de l de mantenimiento ( 50, 100, 200 horas ) al Taller de Mantenimiento Aeroná Aeroná u Organización de Mantenimiento Aeroná Aeronáutico utico (OMA) aprobadas por la DG
Debiendo elaborar el TMA/OMA la apertura de su orden de trabajo, re discrepancias y la apertura de todos los formatos de inspección conte correspondiente Manual de Procedimientos de Inspección (MPI) o Man Organización de Mantenimiento (MOM) en forma integral para su cumplim
El encargado o Control de Calidad del TMA u OMA autorizado por la DGAC DGAC que todas las tareas de mantenimiento, hayan sido satisfactoriamente cul los récords de mantenimiento hayan sido debidamente registrados y (Libreta de Avión, Motor y Hélice, como así también el ITV correspo Constituyendo este procedimiento la certificación de la aeronave para re servicio.
El Programa de mantenimiento como es establecido por el fabricante, Cessn Company, consiste básicamente en inspecciones que se llevan a cabo periódicam acuerdo a lo establecido en correspondiente ficha de inspección, si la aerona menos de 100 horas anuales o no tiene operación por un periodo máximo de 0 continuos, será necesario necesario efectuar una inspección completa (100 Horas, Item Directivas de Aeronavegabilidad, Boletines de Servicio , control de Corrosión yo Sign up to vote on this title aeronave, motor, hélice y accesorios antes de retornarla al servicio.
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No es la política de la Travel Air EIRL exceder los limite estipulados para para el cumpli cumpl inspecciones programadas, Directivas de Aeronavegabilidad, Normas
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMI PROCEDIMIENTOS ENTOS DE INSPECCION
Para las inspecciones enunciadas como Pre y Post Vuelo, el fabricante Cessn Company, no ha contemplado en el manual de mantenimiento de la aeronave las mencionadas inspecciones, sin embargo Travel Air EIRL utilizando el me criterios criteri os propios y las recomendaci rec omendaciones ones de la D.G.A.C., ha elaborado un form el Pre/Post vuelo utilizando como referencia el Manual de Operaciones del fa copia del cual anexamos en las paginas II-2 al II-5 de este manual.
Para los efectos de Post Vuelo de esta aeronave, se utilizará la misma cartilla d Vuelo con las variantes aplicables para efectos de Post-Vuelo, ejemplo:
1. Cockpit Central Lock ……………………………………... ……………………………………... Install and Secure
NOTA: El PRE-VUELO debe ser registrado en el Informe Técnico de Vuelo c acción de mantenimi ma ntenimiento ento y apropiadamente firmado por el mecánico antes d vuelo del día. 11.
ITEMS DE INSPECCIÓN REQUERIDA. REQUERIDA.
Los Ítems que Requieren Inspección (R.I.I.) son aquellos trabajos en unidades ó en las cuales su mantenimiento, Alteración ó Reparación debe ser inspeccionad de concluido o completado por un Inspector ó su designado. Los Item que Inspección (R.I.I.) deben ser inspeccionados y firmados solamente por un autorizado.
12.
CUMPLIMIENTO DE DIRECTIVAS DE AERONAVEGABILIDA AERONAVEGABILIDAD, D, BOLET SERVICIO, NORMAS TÉCNICAS COMPLEMENTARIAS, Y NORMAS T EXTRAORDINARIAS.
Dada la gran importancia para Travel Air EIRL, como empresa aeron conservación, mantenimiento y seguridad de vuelo; que las Direc Aeronavegabilidad, Normas Técnicas Técnicas Complementaria Complementarias,Norma s,Normass Tecnicas Tecnicas Extra y Boletines de Servicio representan, esta no dudará a la recepción recepción de estos doc do en efectuar efect uar su cumplimiento cumplim iento dentro den tro del termino ter mino especificado, haciendo para esto información Técnica recibida y actualizada, las mismas que serán registrad up to vote X-79 on this (FORM title formatos contenidos en la página X-77 (FORMSign CP-367), CP-3 (FORM CP-366), del MGM/MCM. Useful Not useful
13. CONTROL DE CORROSION
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMI PROCEDIMIENTOS ENTOS DE INSPECCION
Este Programa de Mantenimiento cuenta con varios Anexos Complement cuales ayudan a que éste se cumpla eficazmente y en forma precisa. Estos
Anexo “B” Continued Airworthiness Program (CAP)* Anexo “C” Supplemental Inspection Document (SID)
Cessna Service Manual P/N.D138-1-13* Cessna Parts Manual P/N. P257-12* Teledyne Continental Motor Overhaul Manual FORM X-30013*
* Tomos presentados por separado.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION EXTINTOR MANUAL DE FUEGO – DESCRIPCIÓN Y OPERACIÓN GENERALIDADES:
El Extintor de Fuego portátil, es operado manualmente, esta montado y localiza lugar de fácil acceso, para ser usado en un evento de fuego.
DESCRIPCIÓN Y OPERACIÓN:
El Extintor de fuego portátil, operado manualmente esta montado debajo de delantera del asiento del Piloto, el agente extintor es HALOTRON y puede s sobre combustibles sólidos, líquidos y eléctricos, el extintor de fuego esta mont conjunto de soporte y abrazadera de liberación rápida. El servicio del extintor p manejado por los distribuidores del equipo de fuego.
1. Conjunto de soporte (Bracket). (Bracket). 2. Boquilla de extintor de fuego. 3. Palanca de descarga. 4. Pines de seguridad. 5. Maneta 6. Instrumento Instrumento de Presión. 7. Conjunto de Extintor de Fuego. 8. Abrazadera de liberación rápida.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION
PAGINA EN BLANCO DEJADO INTENCIONALMENTE I NTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION PRESERVACION DE LA AERONAVE
Debido a la influencia principalmente de los elementos climatológicos, es importancia tomar en cuenta aspectos concernientes a la forma como se debe pr aeronave, para este efecto Cessna Aircraft Company describe en forma detalla sección 2 de su manual de Servicio N° D138-1-13, los procedimientos a seguir. abreviada podemos describir los siguientes periodos o lapsos de almacenamie Aeronave:
a) Preservación en Condición Operativa: Se define de este modo la condición la Aeronave va a permancer en tierra por un periodo máximo de 30 dias, sin qu sea corrido (REF. Manual de Servicio, Item 2-7). 2 -7).
b) Preservación Temporal: Se define como la condición en la que la Aeron permanecer en condición inoperativa por un máximo de 90 dias (REF. M Servicio, Item 2-8).
c) Preservación Indefinida: Se define como la condición en que la Aeron permanecer en condición inoperativa por un periodo indefinido de tiempo (REF de Servicio, Item 2-9). NOTA:
Adicionalmente es altamente recomendable el frecuente lavado con agua dul superficies de la Aeronave, encerado y limpieza, como asi tambien el uso de cub plugs en los orificios de ventilación, de preferencia la aeronave debe debe permanecer un hangar sobre todo en las proximidades del mar.Sign up to vote on this title
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION
PAGINA EN BLANCO DEJADO INTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION
PAGINA EN BLANCO DEJADO INTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO I. PROCEDIMIE PROCEDIMIENTOS NTOS DE INSPECCION
PAGINA EN BLANCO DEJADO INTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATOS DE INSPECCION
CAPITULO II
FORMATOS DE INSPECCIO TABLA DE CONTENIDO -
INSPECCION DE PRE-VUELO
II-1 al II-7
-
FORMATOS FORMAT OS DE CORRIDA DE MOTOR
II-8 al II-9
-
FORMATO FORMAT O DE INSPECCION DE 25
II-10 al II-11
-
FORMATO FORMAT O DE INSPECCION DE 50
II-12 al II-17
-
FORMATO FORMAT O DE INSPECCION DE 75 HORAS
II-18 al II-19
-
FORMATO FORMAT O DE INSPECCION DE 100 HORAS
II-20 al II-30
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-
FORMATO DE INSPECCIONES ESPECIALES FORMATO ESPECIALES DE II-32 al II-33 Useful Not useful 1,000 HORAS
-
FORMATO FORMAT O DE CORROSION
II-34 al II-35
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. I I. INSPECCION DE PREVUELO
INSPECCIÓN DE PRE-VUELO
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. INSPECCION DE PREVUELO
INSPECCION PRE-VUELO y POST-VUELO POST-VUELO CESSNA 172B OB-584 1.- CABINA
Documentación completa (ITV, Certificados de Aeronavegabilidad y Matrícula, POH, MEL, cartillas de pasajeros, etc.). Seguro de control de mandos. Interruptor de ignición. Interruptor de aviónicos. Interruptor maestro. Indicadores de cantidad de combustible por correcta indicación. Interruptor maestro. Válvula Selectora de Combustible, en posición tanque mas lleno. Control de compensadores. Válvula alterna de presión estática (si está instalada). Asientos, cinturones y arneses de seguridad en buen estado Placards legibles y/o completos (ver MEL si es necesario) Controles de motor por condición general, recorrido y libre operación. Botiquín de primeros auxilios completo y lista actualizada Extintor por seguridad y fecha de vencimiento GPS AERA 500 (para los cuidados cui dados refiérase a la pagina 148 del PILOT GUIDE P/N 19001117-02 19001117-02 Rev. A). 1.-Máster ON – el equipo debe encender automáticamente – Máster OFF.
VERIFICAR REMOVER OF F OF F ON
VERIFICAR OF F POSICIONAR NEUTRAL OF F
VERIFICAR
VERIFICAR
CHEQUEAR
VERIFICAR
VERIFICAR
VERIFICAR
2.- EMPENAJE
Superficies de control por libertad de movimiento y seguridad. Puertas, seguros por correcto funcionamiento.
VERIFICAR REVISAR
3.- B ORDE DE SAL IDA AL A DERECHA
Alerón, por libertad de movimiento y seguridad.
VERIFICAR
4.- AL A DERECHA
Ventilación del tanque de combustible, por obstrucción. Llanta del tren principal (presión 24 psi). Antes del primer vuelo del día y después de cada recarga de combustible usar un vasito drenador completamente limpio, por presencia de agua, sedimentos y grado apropiado de combustible. NOTA: Si el combustible no está libre de contaminantes, incluido agua (aeronave NO-GO). Notifique a su supervisor inmediatamente. La cantidad de combustible (usando la regla). Tapa de tanque de combustible segura y orificio de ventilación sin obstrucciones.
VERIFICAR
VERIFICAR
VERIFICAR
VERIFICAR
VERIFICAR
5.- NARIZ
Hélice y cono, por aseguramiento, aboll abolladuras aduras y fuga de aceite. Diariamente o después de cada cada Sign up to vote on this title vuelo examine por rajaduras melladuras, ralladuras, y corrosión. NOTA: Ejercite extrema precaución al girar manualmente la hélice, en caso de ser necesario. Useful Not useful Entradas de aire, inducción de aire al motor sin restricciones. Amortiguador del Tren de nariz (aprox. 4 pulgadas de luz) deberá tener después de actuar el amortiguador (subir y bajar).
CHEQUEAR
VERIFICAR
VERIFICAR
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PROGRAMA DE MANTENIMIENTO APR
PARA LA AERONAVE CESSNA 172B O
CAPITULO II. INSPECCION DE PREVUELO INSPECCION PRE-VUELO PRE-VUELO y POST-VUELO (Continuación) 6.- ALA IZQUIERDA IZQUIERDA
Llanta del tren principal (presión 24 psi). Antes del primer vuelo y después de cada recarga de combustible, usar el vasito drenador y vaciar una pequeña cantidad de combustible por la válvula de drenaje y si existe presencia de agua, sedimentos y grado apropiado de combustible. NOTA: Si el combustible no está libre de contaminantes, incluido agua, (aeronave NOGO). Notifique a su supervisor inmediatamente Cantidad de combustible (usando la regla). Tapa de tanque de combustible segura y orificio sin obstrucciones. Orificio de entrada de presión estática, sin obstrucciones.
VERIFICAR
VERIFICAR
VERIFICAR VERIFICAR VERIFICAR
7.- BORDE DE ATA QUE ALA IZQUIERDA IZQUIERDA
Retirar cubierta del tubo espu y orificio sin obstrucciones. Aleta de advertencia de perdida, libre de movimiento, mientras el interruptor maestro esta puesto momentáneamente en ON (la sirena debe sonar cuando la aleta es empujada hacia arriba). Ventilación de tanque de combustible por obstrucciones. Luz de taxeo y aterrizaje, por condición, limpieza y operatividad, asimismo verificar luces de navegación, espué y stroboscopica.
VERIFICAR VERIFICAR VERIFICAR VERIFICAR
8.- BORDE DE SALIDA .
Alerón, por libertad de movimiento y seguridad.
VERIFICAR
9.- MOTOR
Remover el cowling del motor e inspeccionar por fugas (aceite, gasolina), mangueras y VERIFICAR cables por rozamiento, y la toma de aire por obstrucción, instalar el cowling y verificar que no hayan broches, tornillos sueltos. Nivel de aceite del motor. No operar con menos de 6/4 Qts.(Correcto nivel 8/4 Qts.) VERIFICAR Tapa de aceite del motor cerrado correctamente. CHEQUEAR Respiradero del carter del motor por obstrucción. Filtro de Combustible: Antes del primer vuelo del día y después de cada recarga de combustible, jalar la perilla del drenador del filtro principal de combustible cerca de 04 segundos para limpiar el filtro VERIFICAR de posible contenido con tenido de agua o sedimentos, verifi car que quede bien cerrado cerrado el drenaje. Si se observa agua continuar drenando. NOTA: Si combustible no está libre de contaminantes y agua, (aeronave NO-GO). CHEQUEAR Controles de motor por condición general, recorrido y libre operación. CHEQUEAR Cableado, espué, y sistema de ignición VERIFICAR Filtro de aire del sistema de inducción deberá ser inspeccionado y limpiado de ser necesario Ref. (M/S sección 2) NOTA: Arranque y corra el motor de ser necesario por cualquier ítem reparado y chequee por fugas de aceite y com de retornar al servicio. Sign up to vote on this title
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PROGRAMA DE MANTENIMIENTO APR
PARA LA AERONAVE CESSNA 172B O
CAPITULO II. INSPECCION DE PREVUELO
PAGINA EN BLANCO DEJADO, INTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. INSPECCION DE PREVUELO
PAGINA EN BLANCO DEJADO INTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. INSPECCION DE PREVUELO
OPERACIÓN EN CLIMA FRIO La zona de operación de esta Aeronave (Costa peruana), no ofrece condic operación en clima frio, sin embargo creemos creemos conveniente tomar en cuenta las recomendaciones: En adición a la inspección de prevuelo prevuelo normal, remueva el hielo, hielo, nieve y escarc alas, cola, superficie de control y bisagras, helice, parabrisas, tapas de re combustible, líneas líneas de ventilación ventilación de combustible, combustible, si usted usted no tiene manera esta formaciones de hielo, nieve y escarcha evite la operación de la aeronav depositos pueden cambiar cambiar los perfiles aerodinamicos y perturbarlos considerabl destruirlos, constituyendo un grave peligro para la seguridad de vuelo. Com procedimiento de pre-vuelo normal y verifique el completo y libre movimiento de la de control.
Durante el proceso proceso de recarga recarga de combustibles a bajas temperaturas, existe existen nc mas favorables favor ables para la l a formación de humedad debido a condensación dentro de los especial atención debe tomarse a fin de drenar el sistema adecuadamente.
MOTOR Particular cuidado debe tomarse en utilizar el grado y tipo de aceite adecuado, adecuado, en 2 del Manual de Servicio Parte No D138-1-13 (Servicing) se describe el grado grado y tip del aceite a usarse, asi mismo previo al arranque, es recomendable girar la hélic varias veces antes del arranque, tomando las precauciones pertinenentes (Magne Mixture Cut OFF, acelerador Closed, calzas puestas). Tambien es recomendable el uso de una fuente externa. Durante condiciones extremas de frio, puede ser necesario precalentar el aceite antes del arranque, un arranque con el aceite congelado en el sistema sistema puede pro indicación de presión de aceite normal pero la misma puede disminuir cuando residual dentro del motor es bombeado dentro del sumidero conteniendo aceite co esta aeronave no cuenta con sistema de precalentador de aceite, por lo que la ope climas extremadamente frio no es permitido (-05º C). Es espués recomendable luego del arranque arranque en clima clima frio observar cuidado Sign up vote on this title durante el calentamiento del motor, las temperaturas deto aceite, debido a que e exceder la temperatura de cabeza de cilindro, cilindro, tratando hacer hace subir la tempe Not ruseful Usefulde aceite, por lo que se recomienda el minimo de RPM durante este proceso abi mismo ejercitar la hélice durante varias veces a fin de remover el aceite frio del H
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. INSPECCION DE PREVUELO USO DE FUENTE EXTERNA
Durante el uso de planta auxiliar o fuente externa de energia debemos tomar en c siguientes precauciones:
1. Esta aeronave esta equipada con un sistema sistema eléctrico de polo negativo a tie vital importancia asegurarnos de conectar el teminal positivo de la planta auxi terminal positivo del receptáculo de la aeronave y el terminal negativo con e negativo del receptáculo. Voltage positivo tambien se debe aplicar al pequeño del receptáculo. Muy particular cuidado deberá tomarse para verificar el uso d correcto (12 VDC).
2. Para prevenir la formación de arco eléctrico entre el receptaculo y el conec fuente externa, la conexión debe efectuarse sin energia en la línea (Power O
3. Asegurese de que que el switch de bateria bateria de la aeronave se encuentre en ON, los y los switchs eléctricos eléctricos en OFF, a fin de que que la bateria este en línea con e antes de conectar la fuente externa esto protege los sistemas electronicos electronicos aso posibles picos de corriente electrrica.
ARRANQUE DE MOTOR USANDO FUENTE EXTERNA 1. 2. 3. 4. 5. 6. 7. 8. 9.
Battery switch Alternator, Electrical, and Avionics Equipment Auxiliary Power Unit Auxiliary Power Unit Auxiliary Power Unit Engine Auxiliary Power Unit Auxiliary Power Unit Alternator Switch
ON OFF CONNECT SET OUTPUT (Max. 16 Vdc on 12 Vdc ON START (use normal start procedures) OFF (after engine has been started) Sign up to vote on this title DISCONNECT ON Useful Not useful
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATOS DE CORRIDA DE MOTOR
TAXEO Y CORRIDA DE MOTOR
El Taxeo como en cualquier otro avión deberá hacerse tomando las debidas preca fin de evitar daños a la aeronave, al equipo en tierra o a personas.
Particular cuidado se tomara a fin f in de comprobar el correcto funcionamiento del si frenos antes de iniciar el rodaje.
Para las corridas del motor, se utilizará un área debidamente habilitada, el mecánic del mantenimiento de la aeronave, tomará la precaución de verificar verificar la disponibili extintor de fuego, una persona apropiadamente calificada (asistente) permanecer momento fuera de la aeronave, en coordinación, vigilando el área y alertara al m abordo sobre cualquier eventualidad como así también estará listo para la utiliz extintor de incendio en caso de ser necesario. Las siguientes acciones serán tomadas antes de iniciar la corrida de m otor.
1.- UBICAR LA AERONAVE EN ZONA AUTORIZADA 2.- ASEGURAR EL AREA DE CORRIDO DE MOTOR, LIBRE DE OBST PERSONAS AJENAS O EXTRAÑAS, EXTINTOR A LA MANO Y ASISTENT 3.- CALZAS PUESTAS, AREA DE LA HELICE LIBRE 4.- LA PERSONA A BORDO A CARGO DEL ARRANQUE, ALERTARA HACIA EL E CON LA VOZ :
L IB RE ¡!!! 5.6.- PROCEDIMIENTO DE ARRANQUE NORMAL 7.- NOTA : CORRIDAS DE DE MOTOR A MÁXIMA MÁXIMA POTENCIA SERAN EF SOLAMENTE SOBRE TERRENO PAVIMENTADO O CEMENTADO, Y E AUTORIZADA. Sign up to vote on this title
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATOS DE CORRIDA DE MOTOR CORRIDA DE CONTINENTAL MOTOR S O-300-D
Inspección Programada (ANTES), Arranque y corra el Motor de acuerdo a las las instrucciones del M VUELO. Tomando nota de cualquier discrepancia o anormalidad, durante el corrido observe lo sig TIPO DE AVION: ___________________ ___________________
S/N: AVION __________ ________________ ______
ENGINE MODEL: ___________________
S/N. MOTOR _________________
CORRIDO DE MOTOR
1.
Válvula Selectora.
2.
Calentar el motor , mezcla rica , paso de hélice adelante
3.
Chequeo de Magnetos (Ajuste el acelerador a 1600 RPM)
4. 5.
Chequeo de Mezcla Corrido Estático (Potencia de decolaje) Enfrentar el avión a la dirección del viento
6.
Temperatura de Aceite
7.
Presión de Aceite
8. 9. 10. 11.
CHT (Temperatura. Cabeza Cilindros)
FECHA: ________________
PARAMETROS Opere el motor colocando en posición LH, RH, BOTH y OFF
OBSER
ANTES DE LA INSP.
LH…………. RH ………... Off ………… Both ……..…
1000 RPM Las Caída de RPM no debe exceder los 150 RPM en ambos magnetos, 75 RPM de diferencia entre ambos Magnetos. Ajustar a 1000 RPM, Lentamente Cortar la mezcla (25 RPM Máximo a 1000 RPM).
RH ……… LH ………. Incre ….…..
-- 2350 RPM en tierra. -- 2700 RPM Max. Arco verde Operación. Normal Línea Roja 225o F Máximo 10 PSI Mínimo 30-60 PSI Operación Normal 100 PSI Máximo 350 – 475o F Operación Normal 525º F Máximo
Chequeo de Alternador (1000 RPM)
Switch ALT
Indicador de succión
3.8 – 4.2 In. Hg ( Ventury)
Respuesta de Motor a cambios de potencia
MATRICULA: _________ ______________ _____
acelerador
OFF-ON N/A
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12.
Funcionamiento del Motor
1.- Ruidos Extraños Useful 2.- Vibraciones
13.
RPM Mínimo
600(+)(-) 25 RPM
Not useful
1 ……….…. 2 ……….…
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 25 HORAS INSPECTION SHEET 25 HOURS AND ITEMS ESPECIALS DATE
AIRCRAFT
ENGINE
PROPE
MODEL TYPE SERIAL NUMBER TOTAL TIME TIME SINCE O/H REGISTRATION No
FECHA DE INICIO
TIPO INSPECCION
FECHA TERMINO 2 5
DESCRIPTION
S P C
MECH.
IN
NOTE:. NOTE:. Before beginning the inspection, determine that engine and propeller performance is normal and tha all system function properly. 50- Hour and 75-hour inspection are 25-hours inspection repeat at these interv check any Items of servicing and lubrication required at these intervals. 1.
2.
Engine and engine compartment for fuel and oil leaks, security of parts, correct engine and propeller control travel, proper safetying, and visible defects.
X
Propeller and spinner for apparent damage or defect X
3.
4.
Remainder of airplane for security of attaching bolts, screws, and rivets, broken spot-welds, fuel leaks and apparent exterior damage or defects.
X
a. Items for servicing and lubrications in accordance with figure 2-4 (Refer to M/S 2-8) as required at 25 hours intervals.
Sign up to voteXon this title
b. Battery
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 25 HORAS INSPECTION SHEET 25 HOURS AND ITEMS ESPECIALS
PAPER REQUIREMENTS 1 2 3
MECH
SERVICE BULLETINS/AIRWORTHINES DIRECTIVES Check that all applicable Cessna Service Bulletins and Supplier Service Bulletins are complied with. A compliance record shall be filled every inspection. Check that all applicable Airworthiness Directives, Normas Técnicas Complementarias and RAP´s are complied with. Ensure all Maintenance Maintena nce Record Entries required by RAP´s are completed before returning the airplane to service. After the inspection has been completed, an engine RUN UP should should again be performed to determine that any discrepancies or abnormalities have been corrected.
DATE OF COMPLETION ____ / ____ / _____
TASKS PERFOR INSPECTOR
MECHANIC NAME
LICENSE No
SIGN.
NAME
LICENSE N
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS INSPECTION SHEET 50 HOURS AND ITEMS ESPECIALS DATE
AIRCRAFT
ENGINE
PROPE
MODEL TYPE SERIAL NUMBER TOTAL TIME TIME SINCE O/H REGISTRATION Nº
FECHA DE INICIO
TIPO INSPECCION
FECHA TERMINO
DESCRIPTION
5 0
R S I P I C
MECH.
NOTE:. NOTE:. Before beginning the inspection, determine that engine and propeller performance is normal and tha all system function properly. 50- hour and 75-hour inspection are 25-hours inspection repeat at these interva check any Items of servicing and lubrication required at these intervals. 1.
2.
Engine and engine compartment for fuel and oil leaks, security of parts, correct engine and propeller control travel, proper safetying, and visible defects.
X
Propeller and spinner for apparent damage or defect X
3.
4.
Remainder of airplane for security of attaching bolts, screws, and rivets, broken spot-welds, fuel leaks and apparent exterior damage or defects. a. Items for servicing and lubrications in accordance with figure 24 (Refer to M/S 2-8) as required at 25 hours intervals.
X
X
Sign up to vote on this title b. Battery Check level of electrolyte every 25 hours (or at least every 30Useful Not useful days), oftener in hot weather. weather. Maintain level of electrolyte electrolyte even 1 with the horizontal baffle plate or split ring at the bottom of the filler X holes by adding distilled water water only
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS
INSPECTION SHEET 50 HOURS AND ITEMS ESPECIALS
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS 5 0
DESCRIPTION
R S I P I C
MECH.
AIRFRAME 29. Aileron control system system : a.- Ailerons for correct direction of movement when operated from X the cabin. b.- Pulleys for security, cleanliness, binding, misalignment,, crcks, X crcked or deformed deform ed pulley brackets, and chipped or broken flanges. c.- Cables for cleanliness, security of terminals, corrosion, fraying, correct tension, and safetying of turnbuckles.
X RII
Bellcran ks and push-pull pu sh-pull rods for cleanliness, lubrication, lubrication, security, X d.- Bellcranks binding, cracks, and distortion.
e.- Fairleads and calbe guards for security and excessive wear.
X
f.- Aileron system for correct rigging and proper travel.
X RII
30. Aileron for security of attachment, smooth operation, security of X balance weights, cracks, corrosion, and skin or structural dam age. 31 Flap Control System : a.- Pulleys for security, cleanliness, binding, misalignment, cracks, X cracked or deformed pulley brackets, and chipped or broken flanges.
b.- Cables for cleanliness, security of terminals, corrosion, fraying, correct tension, and safetying of turnbuckles.
X
RII
Bellcrank s and push-pull pus h-pull rods for cleanliness, lubrication, security, security, X c.- Bellcranks binding, cracks, and distortion. Sign up to vote X on this title wear. d.- Fairleads and cable guards for security and excessive
e.- Flap system for correct rigging and proper travel.
Useful
Not useful X
RII
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS DESCRIPTION 33. Elevator control system : a. Elevators for correct direction of movement when operated from the cabin. b. Pulleys for security, cleanliness, binding, misalignment, cracks, cracked or deformed pulley brackets, and chipped or broken flanges. flanges. c. Cables for cleanliness, security of terminals, corrosion, fraying, correct tension, and safetying of turnbuckles. lubrication,, security, security, d. Bellcranks and push-pull rods for cleanliness, lubrication binding, cracks, and distortiton. e. Fairleads and cable guards for f or security and excessive wear.
5 0
R S I P I C
MECH.
X X X
RII
X X
f. Elevator downspring system for security and proper operation. Where the attachment to the push-pull tube is adjustable, check that X the downspring system applies load to the elevator as it reaches the streamlined position (with stabilizer leading edge full down). g. Elevator system for correct rigging and proper travel. X RII 34. Elevators for security of attachment, smooth operation, security of balance weights, cracks, corrosion, and skin or structural damage. X Elevator or Stabilizer Trim Control System : 35. a.- Elevator trim tab or stabilizer for correct direction of movement X when operated from the cabin. b.- Pulleys and sprockets for security, cleanliness, binding, X misalignment, cracks, cracked or deformed brackets brackets and chipped chipped or broken flanges or teeth. c.- Cables and chains for cleanliness, security of terminals, X RII corrosion, fraying, correct tension, broken or damaged links, and safe safett in of turn turnbu buck ckle les. s. d.- Push-pull rod for security, cracks, and distortion. X e.- Fairleads, cable guards, and chain guards for security and X excessive wear. f. Trim control wheel for lubrication, cleanliness, security, binding, X and operation of friction stop and position indicator; indicator for correct indexing and legible markings. lubrication g. Trim tab or stabilizer actuators for security cleanliness,Sign up to vote X on this title proper operation, corrosion, cracks, and excessive wear. Useful Not useful h. – Trim control system for correct rigging and proper travel. X RII
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS INSPECTION SHEET 50 HOURS AND ITEMS ESPECIALS
DESCRIPTION
5 0
R S I P I C
Continuacion : X d- Cables for cleanliness, security of terminals, corosion, fraying, correct tension on « closed« systems, and safetying safetying of turnbuckles. e- Fairleads and cable uards for X f or security and excessive wear.
RII
f- Rudder system for crrect rigging and proper travel.
RII
X
MECH.
38. Rudder for security of attachment, sooth operation, security of X
balance weight, cracks, corrosion, and skin or structural damage. 39 Rudder trim control system: a- Trim control wheel f or lubrication, cleanliness, security, binding, and proper operation.
b- Position indicator for proper operation, correct indexing, legible markings, and security. c- Bungee for cleanliness, security, proper operation, excessive wear, and correct safetying. d- Chain for cleanliness, proper tension, broken or damaged links, corrosion, and binding. e- Sprockets and connecting shaft for security, binding, misalignment, cracks, excessive wear, cleanliness, and chipped or broken teeth. f- Trim control system for correct rigging. 40.
41.
X
X X X X X
RII
Wings, wing wing struts, and empennage for security of attachment, cracked fittings, loose or missing rivets and bolts, security of hinges, defective bearings, and evidence of elongated bolt holes X and excessive wear of attaching parts. aplicar Nota: Cuando se instale o remueva el Comando de copiloto aplicar Sign up to vote on this title los Procedimien Proce dimientos tos de Inspección especificados en los puntos: 29a, X Useful Not useful 31e, 33a, 35a, 37a.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS INSPECTION SHEET 50 HOURS AND ITEMS ESPECIALS
PAPER REQUIREMENTS
MECH
1.
SERVICE BULLETINS/AIRWORTHINES DIRECTIVES Check that all applicable a pplicable Cessna Service Bulletins and Supplier Supplier Service Bulletins are complied with. A compliance record shall be filled every inspection. 2. Check that all applicable Airworthiness Directives, Normas Técnicas Complementarias and RAP´s are complied with. 3 Ensure all Maintenance Record Entries required by RAP´s are completed before returning the airplane to service. After the inspection has been completed, an engine RUN UP should again be performed to determine that any discrepancies or abnormaliti abnormalities es have been corrected.
DATE OF COMPLETION ____ / ____ / _____
TASKS PERFOR INSPECTOR
MECHANIC NAME
LIC. No
SIGN.
NAME
LIC. No
NOTA: Para el caso en el que durante un procedimiento de mantenimiento rutinario (Ejem.: Inspe 100, 200 horas, Inspecciones Especiales de 1000 horas), en que no aplique la ejecución de un haberse efectuado instalación, ajuste, calibración o reglaje), en el espacio correspondiente se ano Sign up to vote on this title N/A (no Aplicable).
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 50 HORAS
PAGINA EN BLANO DEJADO INTENCIONALMENTE
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 75 HORAS INSPECTION SHEET 75 HOURS AND ITEMS ESPECIALS DATE
AIRCRAFT
ENGINE
PROPE
MODEL TYPE SERIAL NUMBER TOTAL TIME TIME SINCE O/H REGISTRATION Nº
FECHA DE INICIO
TIPO INSPECCION
FECHA TERMINO
DESCRIPTION
7 5
R S I P I C
MECH.
NOTE:. Before beginning the inspection, determine that engine and propeller performance is norm all system function properly. 50- hour and 75-hour inspection are 25-hours inspection repeat at the Also check any Items of servicing and lubrication lubrication required at these intervals intervals 1. Engine and engine compartment for fuel and oil leaks, security of X parts, correct engine and propeller control travel, proper safetying, and visible defects. 2. Propeller and spinner for apparent damage or defect X 3.
4.
Remainder of airplane for security security of attaching bolts, screws, and rivets, broken spot-welds, fuel leaks and apparent exterior damage or defects. a. Items for servicing and lubrications in accordance with figure 2-4 (Refer to M/S 2-8) as required at 25 hours intervals.
X X
b. Battery Check level of electrolyte every 25 hours (or at least everySign 30 up to vote on this title Useful Not useful days), oftener in hot weather. weather. Maintain level of electrolyte electrolyteeven 1 with the horizontal baffle plate or split ring at the bottom of the filler X holes by adding distilled water only
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 75 HORAS INSPECTION SHEET 75 HOURS AND ITEMS ESPECIALS PAPER REQUIREMENTS
MECH.
1.
SERVICE BULLETINS/AIRWORTHINES DIRECTIVES Check that all applicable Cessna Service Bulletins and Supplier Service Bulletins are complied with. A compliance record shall be filled every inspection. 2. Check that all applicable Airworthiness Directives, Normas Técnicas Complementarias and RAP´s are complied with. 3 Ensure all Maintenance Record Entries required by RAP´s are completed before returning the airplane to service. After the inspection inspection has been completed, an engine RUN UP should again be performed to determine that any discrepancies or abnormalities have been corrected.
DATE OF COMPLETION ____ / ____ / _____
TASKS PERFOR INSPECTOR
MECHANIC NAME
LICENSE No
SIGN.
NAME
LICENSE N
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS DATA
AIRCRAFT
ENGINE
PROPE PROP
MODEL / TYPE SERIAL NUMBER TOTAL TIME TIME SINCE O/H REMANENTE REGISTRATION Nº TIPO INSPECCION
1.
FECHA DE INICIO FECHA TERMINO DESCRIPTION
1 0 0
ENGINE RUN – UP Engine temperatures and pressures.
X
R I I
S P C
MECH.
2. Static rpm. X Magneto drop; note particularly any difference between the drop on 3. X the two magnetos. 4. Engine response to changes in power. X
X
5. Any unusual engine noises.
6. Propeller response through pitch range. X Fuel tank selector or shut-off valve; operate engine on each each tank and 7. X off positions long enough to make mak e sure the valve functions properly. 8. Idling speed and mixture; proper idle cut-off. X
X
9. Ammeter. 10. Suction gage.
Sign up to vote on this title
Useful
11. Fuel flow indicator.
ENGINE COMPARTMENT.- NOTE: Remove engine cowling,
X
Not useful X
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS DESCRIPTION
1 0 0
R I I
S P C
4. Entire engine assembly for cleanliness. X 5. Induction air box for internal cleanliness, cracks, and security; air valve and doors for operation and sealing; controls for security and X 3 operation. If installed Filter element BA6108 replace every 100 hours. 6. Cold air and hot air flexible flexible hoses for security, kinks, holes, chafing, X and burnt spots. 7. Engine baffles for security, sealing, cracks, metal deformation, and X attachment of sealing strips. 8. Cylinders for security, security, cracks, broken cooling fins; rocker box covers X and push rod housings for security, oil leaks, cracks, and dents. 9. Crankcase, oil pan, reduction gear housing, and accessory section for security, oil leaks, safetying; front crankshaft seal for oil X leakage. 10. All lines and hoses for security, leaks, cracks, dents, kinks, X corrosion, hose deterioration, and hafing. Intake system for security, leaks, deteriorated hoses, and loose or 11. corroded clamps, manifold drains for proper operation, drain lines X and hoses for security, leaks, and chafing. Exhaust system for security, leaks, cracks, and burned – out spots. 12. X Refer to paragraph 12-74. Ignition harness for security, chafing, burning, defective insulation, 13. X and loose or broken terminals. Spark plugs for proper gap, cleanliness, and evidence of reliable 14. X operation. (Also see paragraph 12-40.) Compresion check , SB 03-3 Crankcase and vacuum system breather lines for security, 15. X obstructions, corrosion, cracks, and chafing. All electrical wiring wiring in the engine compartment for security, 16. X chafing, defective insulation, and loose or broken terminals Signengine up to vote on this title Engine shock mounts for security, safetying, deterioration; Useful of XNot useful 21. mount for cracks, corrosion, dents, bends, and evidence overheating; ground straps for security, corrosion, fraying of braided straps, and cracking of metal straps. Cabin heater valve and door for proper operation, sealing, cracks,
MECH.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS
DESCRIPTION
23.
24.
25. 27.
Starter for security, oil leaks, tight electrical connections; engagement engagem ent lever for f or proper rigging and return spring tension, Every Every 200 hours, check starter brushes for sufficient length, length, binding; binding; brush leads for fraying, chafing; commutator for glaze, pits, grooves, high high mica, and cleanliness. Generator for security and oil leaks if generator is fastened to accessory case; drive belt for cuts, fraying, and excessive wear; electrical electri cal connections conne ctions for security. Every Every 200 hours, check generator brushes for sufficient length, binding; brush leads for fraying, chafing; commutator for glaze, pits, grooves, high mica, and cleanliness. Voltage regulator for security and tight electrical connections. Every Every 200 hours, check contact points for discoloration, pits, and corrosion. Bendix – Scintilla Magnetos. a. Breaker compartment for dirt and grease. b. Breaker points for security, pits, burns and carbon deposits. c. Cam followers for correct lubrication. d. Ventilator screens for cleanliness and security. e. Magnetos for correct internal timing, timing to engine, and security of attachment.
1 0 0
R I I
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X
4
X
5
X
6
X
8 28. Slick (formerly Case) Magnetos.(If installed) X a. Magnetos for correct timing to engine engine and and security security of attachment. Note As long as slick magneto timing is correct, the magnetos need by checked internally only al 500 hours intervals. Check the following items whenever a magneto is disassembled. b. Breaker points for security, pits, burns, and carbon Sign up to vote on this title deposits. c. Cam oilier pad for correct lubrication. Useful Not useful d. Ventilator screens for cleanliness and security. e. Carbon brush for excessive wear. The brush should protrude a minimum of 1/32” from the Shaft.
MECH.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS DESCRIPCION
1 0 0
R I I
S P C
35. Engine cowling for cleanliness, cleanliness, proper fit, security, security, cracks, dents, cuts, tears, loose or broken hinges, defective latches or fasteners, X and deteriorated paint. PROPELLER 1. Fixed- pitch propeller for track, nicks, cracks, corrosion, bends, X dents, security and proper safetying. 5. Spinner and Spinner and spinner bulkhead for cracks, dents, alignment, security, and condition of paint. FUEL SYSTEM 1. Fuel strainer for internal cleanliness, security, leaks, and safetying; X drain valve and control for proper rigging, operation, leaks and security. 3. Fuel tank sump drains for water water and sediment, leaks, leaks, security, security, and safetying, quick drain valves for proper operation. X 4. Under side side of wings for evidence evidence of fuel leaks; leaks; rubber fuel cells cells for X loose fasteners attaching upper surface of win; fuel tank filler cap placards for legibility; caps for leaks and security. NOTE : At engine overhaul periods (or approximately 1000 hrs) drain all fuel and inspect interior of rubber fuel cells for checks and cracks, and the area around the filler opening for visible defects. On metal fuel tanks, remove the wing skin above the tanks and check for deformed metal, chaffing, condition of straps and rubber pads, and security. On rubber or metal tanks, check outlet screens for contamination. These are coarse screens, designed to filter out larger foreign particles. 5. Fuel vents for obstructions, operation operation of check valve, leaks, security, X Sign up to vote on this title and proper position of vent behind wing strut. Useful 6. Fuel selector valve, or shut-off valve, for proper operation, security, Not useful leaks, positive detent positions, and legibility and correct indexing indexing of X placard.
MECH.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND ITEMS ESPECIALS ESPECIALS DESCRIPCION
1 0 0
R I I
S P C
13. Fuel quantity indicating indicating system operational operational test is required every 12 months. Refer to Section 16 for detailed accomplishment X 9 instructions. 14. Carburetor fuel bowl drain, drain, drain fuel from carburetor and check for fuel contaminants Refer Refer to Cessna Service Bulletin Bulletin SEB99-19, X 10 Engine Carburetor Fuel Inspection (or latest revision) for detailed accomplishment instructions. LANDING GEAR 1. Brakes for proper operation, sponginess, failure to hold pressure, X and fluid level. 2. Master cylinders, brake lines, lines, and hoses for security, security, leaks, cracks, dents, and chafing. X 3. Brake linings for wear, cleanliness, chips, cracks, and security. X 4. Brake discs for scoring, warping, excessive wear,and wear,and loose loose or X broken brake clips. 5. Wheel Wh eel and brake assembly for cracks, dents, corrosion, leaks, loose bolts, defective paint, freedom of moving parts, and excessive wear. wear. X 6. Axles for security, security, cleanliness, cleanliness, cracks, bends, detective threads, X axle nuts for proper adjustment and safetying. 7. At the first 100 hour inspection and at 500 hours intervals intervals thereafter, thereafter, remove wheel bearings and inspect for cleanliness, rust, cracks, X RII 12 pits, scoring, brinelling, discoloration, excessive wear, and lubrication. 8. Main landing gear spring struts for security, cracks, bends, deep X scratches, dents, chipped paint, and security of steps. 9. Tires for proper inflation, sufficient tread cleanliness, cuts, blisters, X breaks, and uneven wear. 10. Tail wheel for lubrication, security, cracks; tire for proper inflation, Sign up to vote on this title cuts sufficient tread, breaks, and blisters; tailwheel spring, steering X Useful and anti-swivel mechanism for security, proper operation, crack, Not useful frayed cables, and worn links. 11. Nose gear shock strut for proper servicing, servicing, leaks, cleanliness, X
MECH.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS DESCRIPCION 1. 2.
3. 4. 5. 6.
7. 8.
9.
1 0 0
R I I
S P C
AIRFRAME Pitot and static ports for obstructions ; pitot and static lines for security, X cracks, kinks, chafing, and moisture ; pitot and static systems for leaks ; pitot tube for alignment. Aircraft exterior for cracks, metal distortion, broken spot welds, loose or missing rivets, screws, and bolts, corrosion, condition of paint, and any other apparent damage or defects. Especially check wing and X empennage tips for damage. Aircraft structure for corrosion, cracks, metal distortion, loose or X missing rivets, screws, and bolts, and evidence of excessive loads. Windows and windshield for cleanliness, proper attachment, sealing, X crazing, cracks, deep scratches, and discoloration. Door and window hinges and latches for lubrication, alignment, proper X operation, cracks, distortion, binding, and security. Seat Installation : a. For ease for movement, positive locking, security. b. Upholstery for rips, tears, holes, and cleanliness. c. Seat stops. X d. Seat rails for security, cracks, and damage. e. Seat structure for cracks, bends and bends. f. Reel type secondary seat stops, make sure the manual lock operates correctly. Safety belts for security, proper latching, cuts, tears, fraying, and X broken stitching ; attaching parts for cracks, deformed metal, and excessive wear. Control column for security, binding, cracks, looseness, and restricted travel ; bearings, sprockets, and pulleys for cleanli ness, lubrications, binding, security, and exessive wear ; cables and chains for security, RII title Sign up and to voteXon this clealiness, corrosion, fraying, binding, broken links, misalignment ; turnbuckles for safetying, bellcranks for f orUseful cracks, c racks, Not useful distortion, and binding. Control wheels for alignment, binding, security, bent tube, and X excessive wear ; control lock for proper operation and availability.
MECH.
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS 14. Defrosting, heating, and ventilating systems for proper operation, security, chafing, and deterioration ; controls for proper rigging, X binding, and security ; ram air inlets for obstructions. 15. Cabin upholstery and trim for cleanliness, rips, tears, holes, and secrity ; sunvisors for security and proper operation ; ash trays for X cleanliness and security.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND ITEMS ESPECIALS ESPECIALS DESCRIPCION 16. 17. 18. 19. 20. 21. 22.
23. 24 25.
26. 27. 28. 29.
1 0 0
R I I
S P C
Area beneath floor for cleanliness, cleanliness, chafing and security of lines, hoses, and electrical wires ; control cables for fouling. X Stall warning horn and light for proper operation and security. X Electrical switches, circuit breakers, and fuses for security, security, proper functioning, correct rating, and legibility of placarding ; wiring for X security, securit y, proper insulation, in sulation, and chafing ; spare fuses for availability. availability. Instrument and cabin lights lights for proper operation, security, and X cleanliness ; instrument light rheostat for proper functioning. Radios and and radio controls for proper operation and security. security. X Radio components in in the aft fuselage for security, security, proper shock mounting, cracked or deformed mounting brackets, and X cleanliness. Battery for servicing, servicing, security, security, and corroded terminals ; battery cables for fo r condition of terminals, t erminals, security, and defective insulation ; 1 battery box for cracks, corrosion, damaged mounting brackets, X and security, vent line for corrosion, security and obstructions. Firewall for proper sealing, sealing, security of grommets and shields, cracks, dents, wrinkles, loose or missing rivets, screws, or bolts, X and evidence of excessive loads. Emergency Locator Transmiter. (Refer: Seccion 16 del S/M D1381-13 and Installation Installa tion and Operation Manual Document Nº IM-450). X Radio antennas for cleanliness, security, security, proper connections, corrosion, and cracked insulators ; external loop housing for security, secur ity, cleanliness, cleanlines s, cracks, crack s, loose or or missing screws, sealing, and X obstructed drain hole. Navigation lights, landing lights, and rotating beacon for proper operation, security, cleanliness, and cracked glass. X Stall warning sensing unit for freedom of vane, security, security, cleanlines cleanliness, s, X and proper operation. Pitot and stall warning heaters for proper operation. X Aileron Control System : direction of movement when operated from X a. Ailerons for correct direction the cabin. Sign up to vote on this title crcks, X b. Pulleys for security, cleanliness, binding, misalignment,, Useful Not useful crcked or deformed pulley brackets, and chipped or broken flanges. c. Cables for cleanliness, security of terminals, corrosion, fraying, X RII
MECH.
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS correct tension, and safetying of turnbuckles.
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS DESCRIPCION c. Bellcranks and push-pull rods for cleanliness, lubrication, security, binding, cracks, and distortion. d. Fairleads and cable guards for security and excessive wear. e. Flap system for correct rigging and proper travel. f. Flap control lever for security, proper operation of latch, lubrication, and binding ; flap decal f or legibility. 32. Flaps for security of attachment, smooth operation, binding rollers, rollers, cracked, bent, or loose trcks, corrosion, and skin or structural damage. 33. Elevator control system : a. Elevators for corr ect direction of movement when operated operated from the cabin. b. Pulleys for security, cleanliness, binding, misalignment, cracks, cracked or deformed pulley brackets, and chipped or broken flanges. c. Cables for cleanliness, security of terminals, corrosion, fraying, correct tension, and safetying of turnbuckles. d. Bellcranks and push-pull rods for cleanliness, lubrication, security, binding, cracks, and distortiton. f or security and excessive wear. e. Fairleads and cable guards for
1 0 0 X
35.
S P C
MECH.
X X X
RII
X X X X
RII
X X
f. Elevator downspring system for security and proper operation. X Where the attachment to the push-pull tube is adjustable, check that the downspring system applies load to the elevator as it reaches the streamlined position (with stabilizer leading edge full down). g. Elevator system for correct rigging and proper travel. X 34.
R I I
RII
Elevators for security of attachment, smooth operation, security of Sign up toe. voteXon this title balance weights, cracks, corrosion, and skin or structural damage. damag Elevator or stabilizer trim control system : Useful Not useful a. Elevator trim tab or stabilizer for correct direction of movement X when operated from the cabin.
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS DESCRIPCION g. – Trim tab or stabilizer actuators for security cleanliness, lubrication proper operation, corrosion, cracks, and excessive wear. h. – Trim control system for correct rigging and proper travel.
1 0 0 X
R I I
X
RII
36.
Movable stabilizer or elevator trim tab for security of attachment, X smooth opeation, cracks, corrosion, and skin or structural damage.
37
Rudder Control System : a- Rudder for correct directin of movement when operated from X the cabin. b- Rudder pedal assembly for binding, cleanliness, lubrication, X security, cracks, bent linkage, and excessive wear. c- Pulleys for security, cleanliness, binding, misalignment, cracks, X cracked or deformed pulley brackets, and chipped or broken flanges. d- Cables for cleanliness, security of terminals, coros ion, fraying, X correct tension on closed systems, and safetying safetying of turnbuckles. e- Fairleads and cable uards for f or security and excessive wear.
X
f- Rudder system for crrect rigging and proper travel.
X
S P C
RII
RII
38
Rudder for security of attachment, sooth operation, security of X balance weight, crack s, corrosion, and skin or structural damage. damage.
39.
Rudder trim control system: X a. Trim control wheel for lubrication, cleanliness, security, binding, and proper operation. b. Position indicator for proper operation, correct indexing, legible X markings, and security. Sign up to vote on this title Useful XNot useful c. Bungee for cleanliness, security, proper operation,excessive wear, and correct safetying.
d. Chain for cleanliness, proper tension, broken or damaged X
MECH.
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS puntos: 29a, 31e, 33a, 35a, 37a.
INSPECTION SHEET 100 HOURS AND AND ITEMS ESPECIALS
PAPER REQUIREMENTS 1. 2. 3.
MECH
SERVICE BULLETINS/AIRWORTHINES DIRECTIVES Check that all applicable a pplicable Cessna Service Bulletins and Supplier Supplier Service Bulletins Bulletins are complied with. A compliance record shall be filled every inspection. Check that all applicable applicable Airworthiness Directives, Normas Técnicas Complementarias and RAP´s are complied with. Ensure all all Maintenance Maintenance Record Entries required required by RAP´s are completed completed before returning the airplane to service. After the inspection has been completed, com pleted, an engine RUN UP should again be performed to determine that any discrepancies or abnormalities have been corrected.
DATE OF COMPLETION ____ / ____ / _____
TASKS PERFOR INSPECTOR
MECHANIC NAME
LICENSE No
SIGN.
NAME
LICENSE N
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 100 HORAS CESSNA 172B : ITEMS ESPECIALS ITEM
DESCRIPTION SPECIAL ITEMS
1
Check level of electrolyte every 25 hours (or at least every 30 days)
2
Change engine oil, and replace oil filter every 50 hours.See Section 2 paragraph 2-1
3
Service filter, see paragraph 2-15. Replace filter element BA-6108 each 100 hours.
4
STARTER: Every 200 hours, check starter brushes for sufficient length, binding; bru for fraying, chafing; commutator for glaze, pits, grooves, high mica, and cleanliness.
5
GENERATOR: Every 200 hours, check generator brushes for sufficient length, bindi leads for fraying, chafing; commutator for glaze, pits, grooves, high mica, and cleanl
6
VOLTAJE REGULATOR: Every 200 hours, check contact points for discoloration, pi corrosion.
7
STARTING VIBRATOR: Every 500 hours, check vibrator contact points for discolora and corrosion.
8
Slick (formerly Case) Magnetos: check internally at 5 00 hours intervals.
9
Every 12 months. Refer to Section 16 for detailed accomplishment instructions.
10
up to vote on this title Engine carburetor fuel inspection, every 12 monthsSign (SEB99-19). Useful Not useful
11
The fuel injection nozzles must be cleaned at 300-hour intervals or more frequently stains are found.
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 1000 HORAS
FORMATO DE INSPECCIONES ESPECIALES DE 1000 HORAS Sign up to vote on this title
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 1000 HORAS CESSNA 172B INSPECTIONS SPECIALS 1000 HOURS DATE
AIRCRAFT
ENGINE
PROP
MODEL TYPE SERIAL NUMBER TOTAL TIME TIME NEXT CUMPL. REGISTRATION Nº
FECHA DE INICIO
TIPO INSPECCION
FECHA DE TERMINO
R I I
DESCRIPTION Drain all fuel and inspect interi or of rubber fuel cells for checks and cracks, and the area around the filler opening for visible defects. On metal fuel tanks, remove the wing skin above th e tanks and check for deformed metal, 1 chaffing, condition of straps and rubber pads, and security. On rubber or metal tanks, check outlet screens for contamination. These are coarse screens, designed to filter out larger foreign particles. Magnetic compass for security, fluid di scoloration, leaks, lighting and proper proper operation. Accuracy of the compass on all cardinal headings should be checked whenever equipment replacement, replacement, modification, or relocation might 2 cause compass deviation, and at engine overhaul periods (or approximately approximately 1000 hours). Compensate the compass and record deviation on the compass correction card.
S P C
MECH.
1000 Hrs
1000 Hrs
Seat and interiors, inspect Upholstery for condition. 1000 Hrs
3
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Painting of the aircraft, inspect for condition and presence of corrosion. Useful
4
Not useful 1000 Hrs
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Cessna 172
CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE INSPECCION DE 1000 HORAS
CESSNA 172B INSPECTIONS SPECIALS 1000 HOURS (Contiuacio
R I I
DESCRIPTION
9
BOLTS IN CRITICAL AREAS for: Correct torque in accordance with torque values given in the chart in Section 1, when installed or when RII visual Inspection indicates the need for a torque check.
DATE OF COMPLETION:
MECH.
1000 Hrs
______ /_____ /______
TASK PERFORMED BY: MECHANIC NAME
S P C
INSPECTOR LIC.
SIGNATU RE
NAME
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LIC
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE CORROSION PREVENCION Y CONTROL DE LA CORROSION
NOTA: Para el cumplimiento del Control de prevención y Programa de Corrosio refiérase al Manual Supplemenal Inspection Document (SID´s), presentados por s en el anexo “B”.
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE CORROSION
REGISTRO DE CUMPLIMIENTO DE CONTROL DE CORROSIO MODELO
Nº
FECHA INSPECCION
SERIE
CUMPLIDO
MATRICULA
PROXIMO CUMPLIMIENTO
REALIZADO POR
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE DOBLE COMANDO
FORMATO DE INSTALACIÓN DEL COMANDO Y PEDALES CESSNA 17 DATOS
AERONAVE
MODELO/TIPO: NUMERO DE SERIE: TIEMPO TOTAL: T.U.R.M. : MATRICULA: FECHA: I. PROCEDIMIENTOS PROCEDIMI ENTOS PARA LA INSTALACION DEL COMANDO: La instalación del comando, será realizada de acuerdo con la Memoria Técnica Técnica aprobada aprobada por la DGAC, Manual de Servicios P/N D138-1-13, D138- 1-13, sección 6 párrafo 6-10 figura 6-1 y sección 10 párrafo 10-5 y figura 10-3, AC43.13-1B y lo establecido en la RAP 135.113(b). Mem oria Técnica). 1. PASOS DE INSTALACION DEL COMANDO: (Ref. figura 6 y 3 de la Memoria a) Retirar del Panel de Instrumentos el Cover Cover Plate, con sus respectivos tornillos de sujeción, (Fig. 03 de Memoria Técnica). b) Instalar el comando en F.S. 6.0, instalar BOLT P/N AN3-10A, que une el Tubo de Control con la junta Universal Universal y el Support-control Support-control Tube RH Attaching Parts, del Panel de Instrumentos. c) Remover Placard del Panel de Instrumentos “DOBLE COMANDO REMOVIDO”.
2. PASOS DE INSTALACION DE PEDALES: (Ref. figura 7 y 5 de la Memoria Técnica) a) Remover Registro del Mecanismo de los Pedales, confeccionada confeccionada según lo indicado en la figura 5 de la Memoria Técnica. b) Instalar los pedales en F.S. 6.5, instalar instalar 02 pernos P/N AN3-11A, del ARM RUDDER BAR y 02 pines P/N MS20392-2C15 del LINK-DUAL BRAKES. Chequear la operación de los pedales y verificar el correcto recorrido por libertad de movimiento del timón timón de dirección. Sign up to vote on this title LIBERACION DE MANTENIMIENTO Useful Not useful Certifico que la Instalación del comando com ando y pedales ha sido realizada de acuerdo con los procedim la Memoria Técnica aprobada, realizándose prueba operacional por correcto recorrido y libertad d
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Cessna 172
CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE DOBLE COMANDO
FORMATO DE RETIRO DEL COMANDO Y PEDALES CESSNA 172B DATOS AERONAVE MODELO/TIPO: NUMERO DE SERIE: TIEMPO TOTAL: T.U.R.M. : MATRICULA: FECHA: I. PROCEDIMIENTOS PROCEDIMI ENTOS PARA EL RETIRO DEL COMANDO: La remoción del comando, será realizada de acuerdo con la Memoria Técnica aprobada por la DGAC, Manual de Servicio N/P D138-1-13 sección 6, párrafo 6-10 figura 6-1 y sección 10 parrafo 10- 4, figura 10-3, AC43.13-1B y lo establecido en la RAP 135.113(b). 1. PASOS DE REMOCION DEL COMANDO: (Ref. figura 2 y 3 de la Memoria Técnica) a) Remover el comando instalado en F.S. 6.0, por retiro del BOLT P/N AN3-10ª, que une el Tubo de Control con la junta Universal y el Support-control Tube RH Attaching parts instalado en el Panel de Instrumentos. b) Instalar Cover Plate, en el panel de Instrumento con sus respectivos tornillos de sujeción, (Fig. 03 de Memoria Técnica). c) Instalar placard en el Panel de Instrumentos cerca del timón de doble comando removido, indicando “DOBLE COMANDO REMOVIDO”.
2. PASOS DE REMOCION DE PEDALES: (Ref. figura 4 y 5 de la Memoria Técnica) a) Remover los pedales instalados en F.S. F.S. 6.5, por retiro de 02 pernos P/N AN3-11ª, AN3-11ª, del ARM RUDDER BAR y 02 pines P/N MS20392-2C15 del LINK-DUAL BRAKES. b) Instalar tapa de registro confeccionada según lo lo indicado en la figura 4 de la Memoria Técnica. Chequear la operación del comando y verificar el correcto Sign uprecorrido to vote onpor thislibertad title de movimiento de los elevadores y alerones. Useful Not useful Chequear la operación de los pedales, pedales, y verificar el correcto recorrido por libertad de movimiento del timón de dirección.
MEC
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APR PARA LA AERONAVE CESSNA 172B
CAPITULO II. FORMATO DE DOBLE COMANDO
PAGINA EN BLANCO DEJADO INTENCIONALMENTE
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B O CAPITULO III. OVERHAUL/ REEMPLAZO E INSPECCION
CAPITULO III OVERHAUL Y REEMPLAZO
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B O CAPITULO III. OVERHAUL/ REEMPLAZO E INSPECCION
TIEMPO LIMITE OVERHAUL / REEMPLA REEMPLAZO/INSPECION ZO/INSPECION Todos los componentes compon entes incluídos incluíd os en esta carta deberán inspeccionarse según s el capitulo correspondiente del Manual de Mantenimiento y serán overhau reemplazados según como sea necesario durante los periodos de mantenimien indicados. El tiempo utilizado para los TBO de los componentes, es el tiempo empleado de o del motor desde el arranque, hasta el apagado en el pre sente vuelo, es decir, la del tacómetro / horómetro de la aeronave antes del arranque y después del apa cada vuelo. Ref. NTC-SDA-007-2002 y Oficio Circular Nº 021-2008-MTC/12.04 COMPONENTE MOTOR CONTINENTAL O-300 SERIES HÉLICE, Mc CAULEY CARBURADOR ALTERNADOR MAGNETOS BENDIX S-20 ARRANCADOR VACUUM SYSTEM FILTER
E.L.T. SATELITAL ME406 (BATTERY) FILTRO DE INDUCCION DE AIRE (ELEMENTO P/N BA-6108) ELEVATOR TRIM ACTUATOR
VIDA/ LIMITE 1,800 Hrs. 12 Años 2000 Hrs. 6 Años
ACCION Overhaul Overhaul
OBSERVAC
S.I.L. 98
S.B. Mc C 137AE 1,800 Hrs. Overhaul S.I.L. 12 Años S.B.97 1,800 Hrs. S.I.L. 98 12 Años Overhaul S.B.97 1,800 Hrs. Master Servic X-4200 04 Años Overhaul SB-643 1800 Hrs S.I.L. 98 12 Años Overhaul S.B.97 S/M D138 Replace 500 Hrs. Sección 2 Maintenance ME406 and Replace 05 Año HM ELT D138 100 Hrs/ Sign up to vote on this title S/M Replace 1 año Sec.2-1 Useful Not useful S/M D138 1000 Hrs. Overhaul 03 Años Sección 2
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B O CAPITULO III. OVERHAUL/ REEMPLAZO E INSPECCION
CARTA DE OVERHAUL / REEMPLAZO DE COMPONENTES (Continuacion) COMPONENTE RESTRAINT ASSEMBLY PILOT, COPILOT AND PASSENGER SEATS. VACUUM RELIEF/REGULATOR VALVE FILTER EXTINGUISHER HAND
Aircraft Structure
VIDA/ LIMITE
ACCION
10 Años
Replace
N/A
N/A
05 Años
Replace
30,000 hrs
Replace
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OBSERVA
S/M D138 Sección No Vacuum (Only Air V
Opera
TR7 D138
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B O CAPITULO III. OVERHAUL/ REEMPLAZO E INSPECCION TIEMPO LIMITE DE OVERHAUL / REEMPLAZOS /INSPECCION VIDA/ LIMITE
ACCION
REFER
SID Operation 1
100 hrs 12 month
Visual
TR7 D1
SID Operation 2
24 month
Visual
TR7 D1
SID Operation 3
35 month
Visual
TR7 D1
SID Operation 4
36 month
Visual
TR7 D1
SID Operation 5
48 month
Visual
TR7 D1
SID Operation 6
60 month
Visual
TR7 D1
SID Operation 7
1,000 hrs. 3 Years
VISUAL, EDDY CURRENT, IF REQUIRED FOR CONFIRMATION
SID Operation 8
3,000 hrs. 5 Years
Visual
SID Operation 9
3,000 hrs. 5 Years
VISUAL AND EDDY CURRENT
SID Operation 10
VISUAL AND At Engine MAGNETIC OverhaulSign up toPARTICLE vote on this title
COMPONENTE
SID Operation 11
10 Years
Useful
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Visual
TR7 D1
TR7 D1
TR7 D1
TR7 D1
TR7 D1
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Cessna 172
CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B O CAPITULO III. OVERHAUL/ REEMPLAZO E INSPECCION
TIEMPO LIMITE DE OVERHAUL / REEMPLAZOS /INSPECCION VIDA/ LIMITE
ACCION
REFER
SID Operation 16
500 hrs. 5 Years
Visual
TR7 D1
SID Operation 17
1,000 hrs. 5 Years
Visual
TR7 D1
SID Operation 18
10 Years
Visual
TR7 D1
SID Operation 19
5 Years
Visual
TR7 D1
COMPONENTE
SID Operation 20
20,000 hrs. 10 Years
SID Operation 21
1,000 hrs. 5 Years
SID Operation 22
2,000 hrs. 5 Years
SID Operation 23 SID Operation 24 SID Operation 25
2,000 hrs. Visual 5 Years 1,000 hrs. Visual 3 Years 100 hrs. Visual 1 YearsSign up to vote on this title
SID Operation 26
VISUAL WITH EDDY CURRENT IF NEEDED. VISUAL WITH EDDY CURRENT IF NEEDED. VISUAL WITH EDDY CURRENT IF NEEDED.
2,500 hrs. 5 Years
Useful
TR7 D1
TR7 D1
TR7 D1
TR7 D1
TR7 D1 TR7
D1
Not useful
Visual and Boroscope
TR7 D1
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CURSO JEPPSEN
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B O CAPITULO III. OVERHAUL/ REEMPLAZO E INSPECCION
PAGINA INTENCIONALMENTE DEJADA EN BLANCO
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B IV. ANEXO “A”
ANEXO “A”
CONTINUED AIRWORTHINESS PROGRAM (C PRESENTADO EN UN VOLUMEN POR SEPARADO Sign up to vote on this title
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PROGRAMA DE MANTENIMIENTO APRO PARA LA AERONAVE CESSNA 172B IV. ANEXO “A”
ANEXO “B”
SUPPLEMENTAL INSPECTION DOCUMENT ( PRESENTADO EN UN VOLUMEN POR SEPARADO Sign up to vote on this title
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