test 9

Use AD 93-24-03 to answer this question. Known information: Beech Bonanza model E33, serial number CD1224, current aircraft total time 3,676 hours. The last recorded entry for this AD was at aircraft total time of 3,176 hours. At that time, the forward rudder spar was inspected in accordance with Beech service Bulletin No. 2333, Revision 1, No cracks were found at that time. During current inspection at 3,676 hours, cracks were found in the area of the upper hinge. What action should be taken concerning compliance with this AD?. reinspect the rudder forward spar for cracks in accordance with the instructions in Beech Service Bulletin No. 2333, Revision 1, at intervals not to exceed 500 hours time in service. since cracks were found only in the upper hinge area no further action is required by this AD. stop-drill the cracks and install an SMP upper-hinge reinforcement bracket in accordance with STC SA4899NM.

Use Airworthiness Directive (AD) AD 81-23-01 R1 to answer this question. Known Information: Beechcraft model 65-A88 serial number LP-34. Following the requirements of AD 81-23-01 R1, which of the following hardware is compatible for use with a used preload indicating washer?. A) FN22M-1414. B) LWB 22-14-31. C) VEP 220121-14-32.

Use Airworthiness Directive (AD) AD 90-01-06 to answer this question. Known Information: Enstrom Helicopter model F-28C-2 equipped with tail rotor gear box P/N 28-13500-1, incorporating a Boston gear XR-137-2YR. Installed gear box was placed in service, in new condition, at total time of 2,104 hours. During the last compliance with AD 90-01-06 at total time of 3,204 hours, five metal flakes of less than the AD specified size were noted in the gearbox oil. The gear box was flushed and reserviced. A test flight was conducted per the requirements of the AD. No further metal was found at that time. What action, if any, may be required during the annual inspection at 3,304 hours concerning this AD?. Replace the tail rotor gearbox. No further action is required at this time. If metal is found during the inspection, clean gearbox, reservice, and test fly. If metal reappears, replace gearbox.

Use Airworthiness Directive (AD) AD 82-11-05 to answer this question. Known Information: Bendix Magneto model D-2000 with blue identification plate, serial number 8121106. Time since new 2,002.5 hours, with 198.2 hours of operation in the preceding year. A review of aircraft records, prior to an annual inspection, revealed no compliance with AD 82-11-05. What action, if any, is required?. The blue identification plate found on the magneto indicates that it is a factory overhaul with AD compliance by the manufacturer. Compliance with AD will be by inspection and gear replacement. The magneto must be inspected per Bendix service bulletin number 617 within the next 50 hours time in service.

Use Airworthiness Directive (AD) 80-10-02 to answer this question. Known information: Messerschmitt-Bolkow-Blohm Model BO-105 helicopter with tail rotor blade grips P/N 105-31722 installed. While performing a progressive inspection on this helicopter, you note in the aircraft's records that the last compliance with AD 80- 10-02 was at an aircraft time of 5402 hours. The records further indicate that the tail rotor blade grips were replaced at an aircraft time of 4902. What action is required at this inspection with a time of 5502?. Compliance is required for paragraph (c) (1) (2). Compliance is required for paragraph (c). Compliance is required for paragraph (b) (d) (e).

Use Airworthiness Directive (AD) AD 82-06-12 to answer this question. Known Information: Air Tractor model AT-302, serial number 302-6521, equipped with 1-inch-thick (P/N 40007-2) main landing gear struts. On the effective date of AD 82-06-12, this aircraft had accumulated 703 hours and 897 landings. Which of the following actions would the AD require?. Within 500 landings, replace landing gear. Within 100 hours, inspect in accordance with paragraph (c). Within 20 hours, inspect in accordance with paragraph (c).

Use Airworthiness Directive (AD) AD 82-11-05 to answer this question. Known Information: Bendix Magneto model D-2000 with blue identification plate, serial number 8122206. Time since new 2,002.5 hours, with 198.2 hours of operation in the preceding year. A review of aircraft records, prior to an annual inspection, revealed no compliance with AD 82-11-05. What action, if any, is required?. Airworthiness directive does not apply by serial number. Compliance with AD will be by inspection and gear replacement. The magneto must be inspected per Bendix Service Bulletin number 617 within the next 50 hours time in service.

Use Airworthiness Directive (AD) AD 94-10-02 to answer this question. Known Information: Pratt & Whitney Canada (PWC) model PT6A-67D turboprop engine. Engine serial number PC-E114029, total time since new 1,572 hours at the effective date of AD 94-10-02, June 15, 1994. The maintenance record indicates the CT disk and blade assembly was debladed and inspected per the accomplishment instructions of PWC SB No. 14128, Revision 1, at 1,498 hours on December 16, 1992, in accordance with AD 92-27-19. When will the next deblading and inspection become due?. A) 1,548 horas. B) 1,622 horas. C) 1,748 horas.

Use Airworthiness Directive (AD) AD 95-13-08 to answer this question. Known Information: Pratt & Whitney Canada (PWC) model PT6A-67D turboprop engine. Engine serial number PC-E114029, total time since new 1,572 hours at receipt of AD 95-13-08. The maintenance record indicates the CT disk and blade assembly was debladed and inspected per the accomplishment instructions of PWC SB No. 14128, Revision 1, at 2,087 TIS hours on December 16, 1992, in accordance with AD 92-27-19. The aircraft now has 2,116 TIS. When will the next deblading and inspection become due?. 2,187 hours- 10 hours over due. 2,166 hours- due immediately. 2,137 hours- 21 hours to go.

Use Airworthiness Directive (AD) AD 93-24-03 to answer this question. Known Information: Beech Bonanza model E33, serial number CD1224, current aircraft total time 3,677 hours. The last recorded entry for this AD was at aircraft total time of 3,176 hours. At that time, the forward rudder spar was inspected in accordance with Beech Service Bulletin (SB) No. 2333, Revision 1. Following the inspection at that time, Supplemental Type Certificate (STC) SA4899NM was used to install SMP reinforcement bracket. What action is required at the current aircraft total time? La última entrada registrada para esta AD fue en un total de horas del avione de 3.176 horas. En ese momento, el mástil delantero del timón de profundidad fue inspeccionado de acuerdo con el Boletín de Servicio de beech (SB) No. 2333, Revisión 1. Después de la inspección en ese momento, el Certificado de Tipo Suplementario (STC) SA4899NM se utilizó para instalar el soporte SMP de refuerzo. ¿Qué medidas se requiere en la hora total actual del avión?. Reinspect in accordance with beech service bulletin SB No. 2333, revision 1. No further action is required by this AD. Replace rudder assembly with part number 33-630000-167.

Use Airworthiness Directive AD 80-15-12 to answer this question. Known Information: Agusta Helicopter model A109A, serial number 7162, having main rotor mast bearing inner race P/N 109-0404- 14 installed. What action is required at 200 hours time in service after the effective date of AD 80-15-12, if no evidence of oil leaks are found?. Install bearing race P/N 109-0404-14-15. Continue compliance with paragraph (d). Replace packing P/N 109-0406-68.

Use Airworthiness Directive AD 90-08-14 to answer this question. During the current annual inspection, aircraft records indicated AD 90-08-14 was last complied with at 1,500 hours. At that time, cracks were found in the wing forward spar carry-through web structure. One crack in the left forward bend radius, measuring .45 inch and one in the right aft bend radius measuring .40 inch, both were stop drilled. At this inspection, both cracks that were previously stop-drilled showed no additional cracking. However, another crack was found in the right aft web face that passes between two holes and extends another .78 inches. What action should be taken concerning compliance with this AD?. Stop-drill the additional crack and reinspect in 100 hours. Approve for return to service, and reinspect in the next 25 hours. Install beech P/N 58-4008 prior to further flight.

Use Airworthiness Directive AD 90-08-14 to answer this question. Known Information: Beechcraft model 56TC, serial number TG-28, aircraft total time 1,701.9 hours. During the current annual inspection, aircraft records indicated AD 90-08-14 was last complied with at 1,500.4 hours. At that time, cracks were found in the wing forward spar carry-through web structure. One crack in the left forward bend radius, measuring .45 inch and one in the right aft bend radius measuring .40 inch, both were stop drilled. At this inspection, both cracks that were previously stop-drilled showed no additional cracking. However, another crack was found in the right aft web face emanating from one huckbolt hole to another. What action should be taken concerning compliance with this AD?. Stop drill the additional crack and reinspect in 100 hours. Install kit P/N 58-4008 within the next 25 hours. Approve for return to service and reinspect within the next 100 hours.

How do we know the revisions to an Airworthiness Directive?. By the number at the bottom of the AD. In the first paragraph of the AD. In the AD number.

When, if ever, are manufacturer's service bulletins considered mandatory during an annual inspection?. When incorporated in the maintenance manual as required in 14 CFR part 21. Service bulletins are optional and never required at annual inspections. When incorporated in 14 CFR part 39.

Aeronaves, motores de aeronaves, hélices y palas de hélice y cubos están requeridos a ser marcados con ciertos datos de identificación. Un motor de aeronave requiere cual de los datos siguientes?(1) Nombre del fabricante.(2) Designación del modelo.(3) El número de serie del fabricante.(4) Número del certificado de tipo, en su caso.(5) Número del certificado de producción, en su caso.(6) La clasificación establecida para motores de las aeronaves. A) 1, 3, 4 y 6. B) 1, 2, 3, y 6. C) Todos los de arriba.

Aeronaves, motores de aeronaves, hélices y palas de hélice y cubos están requeridos a ser marcados con ciertos datos de identificación. Una hélice de paso requiere cual de los datos sigueintes?(1) Nombre del fabricante.(2) Designación del modelo.(3) El número de serie del fabricante.(4) Número del certificado de tipo, en su caso.(5) Número del certificado de producción, en su caso.(6) Numero de pieza (o equivalente). A) 1, 3, 4, y 6. B) 1, 2, 3, y 6. C) 1, 2, 3, 4, y 5.

Cual regulación en el 14 CFR establece las marcas de identificación requeridas en una aeronave civil de matrícula americana?. A) El 14 CFR parte 43. B) El 14 CFR parte 45. B) El 14 CFR parte 45.

En conjunto con la realizacion de de una inspeccion anual de una aeronave, usted determina que la aeronave no puede ser aprobada para su retorno a servicio debido a que uno de los siguientes elementos se encuentra ausente. ¿Cual elemento es ese?. A) Certificado de aeronavegabilidad. B) Los registros de la aeronave. C) Los datos de la matricula de la aeronave.

La aprobación de los fabricantes de piezas (PMA) que estan requeridas a ser marcadas con cierta información entre los cuales está el nombre y el modelo de cada producto con certificado tipo en el que la parte es elegible para su instalación. Cuando la información es tan extensiva que no es práctico marcarla en la pieza, una etiqueta adherida a la pieza o el contenedor de la pieza, la información puede ser: A) Incluida en un formulario FAA 337 para acompañar a la pieza y se completará en el momento de la instalación. B) Incluida en un catálogo de facil acceso. C) Incluidos en la hoja de datos del certificado de tipo original.

La aprobación de los fabricantes de piezas (PMA) que no tienen tiempos obligatorios de reemplazo, intervalos de inspección, o procedimiento especificos relacionado en la sección de limitaciones de aeronavegabilidad de un manual de mantenimiento del fabricante, o instrucciones para aeronavegabilidad continuada, no son requeridas a ser marcadas con qué información?. A) Las letras ¨FAA PMA¨. B) La marca. C) El numero de serie.

Piezas aeronáuticas, para lo cual se especifica un tiempo de reemplazo en la sección de limitaciones de aeronavegabilidad del manual de mantenimiento del fabricante, deberán ser marcadas con cual de la información siguiente ?(1) Nombre del fabricante.(2) designación del modelo.(3) Número de serie (o equivalente).(4) Número del certificado de tipo, en su caso.(5) Número del certificado de producción, en su caso.(6) Número de parte o pieza (o equivalente). A) 3 y 6. B) 1, 2 and 3. C) Todos los de arriba.

Una pequeña aeronave de matrícula americana construida por lo menos hace 30 años, de qué tamaño puede mostrar las marcas de registro?. A) 2 pulgadas. B) 12 pulgadas. C) Culquiera A o B.

¿Cuáles son los requisitos de altura de las marcas de registro de un Cessna del 1975 modelo 177RG repintado en 1994?. A) 2 pulgadas. B) 3 pulgadas. C) 12 pulgadas.

While reviewing an aircraft's records during an annual inspection, you notice three different FAA Forms 337 for the overhaul of the aircraft's engine. How long must these major repair records be retained? These records shall be retained. An transferred with the engine. For a period of 2 years after the work was performed. For a period of 1 year from the date of completion.

Each registered owner or operator of a large airplane, turbojet multiengine airplane, turbo propeller powered multiengine airplane and turbine-powered rotorcraft operated under 14 CFR Part 91, must elect one of the inspection programs of 14 CFR Section 91.409(e). However, one of these operators may additionally select an annual inspection. Which operator is it?. Large airplane. Multiengine turbo propeller airplane. Turbine rotorcraft.

Each registered owner or operator of an aircraft using a progressive inspection must designate a person to supervise or conduct the inspection. Which of the following could perform those duties?. A and P mechanic. Certificated airframe repair station. Both 1 and 2.

Each registered owner or operator of an aircraft using a progressive inspection must designate a person to supervise or conduct the inspection. Which of the following could perform those duties?. The aircraft manufacturer. Certificated airframe repair station. Both 1 and 2.

As the holder of an inspection authorization, you are approached by the owner of an aircraft that has recently been imported from a foreign country. The new owner wants to know when the aircraft will require an annual inspection. The aircraft's records indicate that the aircraft has been maintained under a French inspection program and that the last complete inspection under that program was four months earlier. The record further indicates that the aircraft entered the U.S. two months ago and was issued a U.S. standard airworthiness certificate at that time. When will the annual inspection be due?. in 8 calendar month. Immediately. In 10 calendar months.

When is an aircraft equipped for "Day VFR Only" operation, required to have it's altimeter tested and inspected in accordance with 14 CFR Part 43, Appendix E? Compliance with Appendix E. Not required. Required each 12 calendar months. Required each 24 calendar months.

Following a major repair that might appreciably change the flight characteristics of an aircraft, other than the maintenance record entry required by 14 CFR Section 43.9, what must be entered in the aircraft records?. The supplemental type certificate number. Record of flight test. FAA form 337.

Federal Aviation Regulations require certain information to be included in an aircraft's maintenance records for airworthiness directive compliance. Which of the following information would be part of a required record entry for the airworthiness directive?. Amendment number. Serial number of aircraft. Revision date.

Title 14 of the Code of Federal Regulations allow aircraft established on certain inspection programs to exceed an inspection interval by 10 hours while en route to a place where the inspection can be done. Which of the following may exceed the inspection interval by 10 hours?. An aircraft using a 100-hour inspection program. An aircraft using a progressive inspection program. Both 1 and 2.

The holder of an inspection authorization may supervise a progressive inspection on a turbine-powered rotorcraft weighing. 7,000 Lbs or less. 7,001 Lbs or more. Both 1 and 2.

The holder of an inspection authorization may supervise a progressive inspection on a turbine-powered rotorcraft weighting. 12,500 lbs or less. over 12,500 lbs. both 1 and 2.

The regulations require each registered owner or operator to maintain a record of Airworthiness Directives (AD). Listing all ADs pertinent to his or her moder. In a logbook for each airframe, engine, propeller, or rotor. Listing status of applicable ADs.

If an aircraft that has a separate record for airframe and engine receives a replacement engine between annual inspections, what action would be required?. An inspection as required by the manufacturer and a maintenance record entry. A 100-hour inspection of the engine followed by a flight test. Only the engine portion of the annual inspection with an entry in the engine´s record.

A Cessna 421B operated as a 14 CFR Part 91 airplane would have inspection conducted in accordance with. 14 CFR Part 43. Appendix D. 14 CFR Part 91, §91.409 (Inspections). 14 CFR Part 43, §43.16 (Airworthiness Limitations).

A rebuilt aircraft engine may be granted zero time by. The manufacturer. A certified powerplant mechanic. An A and P mechanic who holds an inspection authorization.

Which one of the following aircraft could require an annual inspection?. A small single-engine turboprop with a restricted airworthiness certificate. A rotorcraft with a provisional airworthiness certificate. A small multiengine turboprop aircraft with a standard airworthiness certificate.

Which one of the following aircraft could be maintained under an approved inspection program by the operator?. 30 seat large aircraft. 12 seat multi-engine turbine aircraft under commuter. Neither 1 or 2.

Which of the following is required to be installed on an airplane manufactured after July 18, 1978?. Shoulder harness for each front seat. An operacional emergency locator beacon. An equipment list showing the minimum equipment required for aircraft operations under specified conditions.

When may an authorized inspector (IA) perform an annual inspection on an aircraft?. 12 calendar months from the day the last annual inspection was performed. The IA may perform an annual inspection anytime the owner requests it. The IA may only perform an annual inspection only during the month the inspection is due.

When would data in aircraft maintenance manuals be considered approved data?. Aircraft maintenance manuals from the original manufacturer are always considered approved data. A manual or parts thereof become approved if the manufacturer assigns it's approval in the manual. When a manual includes an airworthiness limitations section, that section is considered approved data.

When, if ever, is the manufacturer's maintenance manual, or a section thereof, considered mandatory during an annual inspection?. They are required when part of an approved inspection program. They are required if made mandatory by the type certification program. Maintenance manuals are optional if an equivalent procedure is used.

How long must an FAA Form 337 for the overhaul of a reciprocating engine having a planetary propeller reduction gearing be retained?. It is retained in the engine records until the engine is removed from the airframe and replaced with a different engine or for 24 calendar months whichever occurs first. It is retained as a permanent document in the engine records or until the engine is zero timed. It is retained until the work is repeated or superseded by other work or for 1 year after the work is performed.

How long must an FAA Form 337 for the overhaul of a reciprocating engine having an integral supercharger be retained?. It is retained until the engine is removed from the airframe and replaced with a different engine. It is retained until the work is repeated or superseded by other work or for 1 year after the work is performed. It is retained as a permanent document in the engine records or until the engine is zero timed.

A 14 CFR Part 91 operator of a turbine-powered rotorcraft may elect to use which of the following inspection provisions?. An annual inspection. A Current inspection program recommended by the manufacturer. Either 1 or 2.

A 14 CFR Part 91 operator of a turbine-powered rotorcraft may elect to use which of the following inspection provision?. An annual inspection. An inspection program established by the operator and approved by the administrator. Either 1 or 2.

Certain persons are designated by the Administrator to represent the FAA in developing and approving technical data for alteration and repair of U.S.-certificated aircraft. These persons are known as. Designated aircraft maintenance inspectors. Designated engineering representatives. Designated airworthiness representatives.

A major repair is required in the fuselage of a corporate aircraft. A structural engineer has created a drawing of how to repair the damage. the technician should. fix the aircraft per the drawing and make a logbook entry. send the drawing to a structural Designated Engineering Representative (FAA-DER) for approval and then complete a 337 for FAA field approval. request an FAA Field approval from the local FSDO before doing the work on the aircraft.

When a repair station makes a major repair, the repair may be approved for return to service on an FAA Form 337, customer's work order, or tag attached to the product. 14 CFR Part 43, Appendix B, requires a maintenance release statement be printed on which of these documents?. FAA form 337. Tag attached to the product. Both A and B.

How long should an FAA Form 337 for a major alteration to an airframe be retained?. For one year or until the work is repeated or superceded. It becomes a part of of the permanent maintenance record and it is transferred with the aircraft when it is sold. For two years or until the work is repeated or superceded.

Who is responsible for keeping and maintaining the maintenance records for an aircraft operated under 14 CFR Part 91?. The pilot who flies the aircraft. The maintenance personnel who does the work. The owner or operator of the aircraft.