LEARJET 60-60XR AEROCIVIL

(1) Each Phase Inspection is contained within one of four hourly or calendar driven inspection intervals?. (a) Perform each subsequent A-Phase inspection every 300 hours or 12 months, whichever occurs. (b) Perform each subsequent A-Phase inspection every 300 hours or 24 months, whichever occurs. (c) Perform each subsequent A-Phase inspection every 300 hours or 36 months, whichever occurs. (d) Perform each subsequent A-Phase inspection every 300 hours or 48 months, whichever occurs.

(2) Inspections controlled by Hours may be accomplished within a period of beginning?. (a) At or before 600 Total Aircraft Hours or 12 months from the original Certificate of Airworthiness. (b) At or before 600 Total Aircraft Hours or 24 months from the original Certificate of Airworthiness. (c) At or before 600 Total Aircraft Hours or 36 months from the original Certificate of Airworthiness. (d) At or before 600 Total Aircraft Hours or 48 months from the original Certificate of Airworthiness.

(3) Inspections controlled by landings or cycles may be accomplished within a period of beginning?. (a) Perform each subsequent B-Phase inspection every 300 hours or 12 months, whichever occurs. (b) Perform each subsequent B-Phase inspection every 600 hours or 24 months, whichever occurs. (c) Perform each subsequent B-Phase inspection every 900 hours or 36 months, whichever occurs. (d) Perform each subsequent B-Phase inspection every 1200 hours or 48 months, whichever occurs.

(4) Inspections controlled by Hours may be accomplished within a period of beginning?. (a) At or before 1200 Total Aircraft Hours or 12 months from the original Certificate of Airworthiness. (b) At or before 1200 Total Aircraft Hours or 24 months from the original Certificate of Airworthiness. (c) At or before 1200 Total Aircraft Hours or 36 months from the original Certificate of Airworthiness. (d) At or before 1200 Total Aircraft Hours or 48 months from the original Certificate of Airworthiness.

(5). The following is a list of all scheduled inspections contained in the Learjet Inspection Program and the overhaul interval for each inspection is true?. (a) Landing Inspection - Due Every 2,000 Landings. b) Landing Inspection - Due Every 3,000 Landings. (c) Landing Inspection - Due Every 4,000 Landings. (d) Landing Inspection - Due Every 6,000 Landings.

(6). The following is a list of all scheduled inspections contained in the Learjet Inspection Program and the major landing gear interval for each inspection is true?. (a) Major Landing Inspection - Due Every 2,000 Landings. (b) Major Landing Inspection - Due Every 3,000 Landings. (c) Major Landing Inspection - Due Every 4,000 Landings. (d) Major Landing Inspection - Due Every 6,000 Landings.

(7). The following is a list of all scheduled inspections contained in the Learjet Inspection Program and the overhaul interval for each inspection is true?. (a) 12,000 Hour Airframe Inspection - Initial Due at first 12,000 Hours/Repeat Due Every12.000Hours. (b) 12,000 Hour Airframe Inspection - Initial Due at first 12,000 Hours/Repeat Due Every 6,000 cycle. (c) 12,000 Hour Airframe Inspection - Initial Due at first 12,000 Hours/Repeat Due Every 12,000 Hours. (d) 12,000 Hour Airframe Inspection - Initial Due at first 12,000 Hours/Repeat Due Every 12,000 cycle.

(8). The following is a list of all scheduled inspections contained in the Learjet Inspection Program and the overhaul interval for each inspection. (a) Phases A1, A2, A3, A4, A5, and A6 - Each A-Phase Due Every 300 Hours or 12 Months. (b) Phases B1, B2, B3, B4, B5, and B6 - Each B-Phase Due Every 300 Hours or 24 Months. (c) Phases C1, C2, C3, C4, C5, and C6 - Each C-Phase Due Every 300 Hours or 48 Months. (d) Phases D1, D2, D3, D4, D5, and D6 - Each D-Phase Due Every 300 Hours or 96 Months.

(9). The following is a list of all scheduled inspections contained in the Learjet Inspection Program and the overhaul interval for each inspection. (a) Phases A1, A2, A3, A4, A5, and A6 - Each A-Phase Due Every 600 Hours or 12 Months. b) Phases B1, B2, B3, B4, B5, and B6 - Each B-Phase Due Every 600 Hours or 24 Months. (c) Phases C1, C2, C3, C4, C5, and C6 - Each C-Phase Due Every 600 Hours or 48 Months. d) Phases D1, D2, D3, D4, D5, and D6 - Each D-Phase Due Every 600 Hours or 96 Months.

10. The following is a list of all scheduled inspections contained in the Learjet Inspection Program and the overhaul interval for each inspection. (a) Phases A1, A2, A3, A4, A5, and A6 - Each A-Phase Due Every 1200 Hours or 12 Months. (b) Phases B1, B2, B3, B4, B5, and B6 - Each B-Phase Due Every 1200 Hours or 24 Months. (c) Phases C1, C2, C3, C4, C5, and C6 - Each C-Phase Due Every 1200 Hours or 48 Months. (d) Phases D1, D2, D3, D4, D5, and D6 - Each D-Phase Due Every 1200 Hours or 96 Months.

11.The following specifies the Allowable Inspection Tolerances for Learjet scheduled inspections: (a) Inspections controlled by calendar time may be accomplished within a period beginning 2 weeks before and ending no later than 2 weeks after the inspection due date. (b) Inspections controlled by calendar time may be accomplished within a period beginning 3weeks before and ending no later than 3 weeks after the inspection due date. (c) Inspections controlled by calendar time may be accomplished within a period beginning 4 weeks before and ending no later than 4 weeks after the inspection due date. (d) )Inspections controlled by calendar time may be accomplished within a period beginning 6 weeks before and ending no later than 6 weeks after the inspection due date.

12. The following specifies the Allowable Inspection Tolerances for Learjet scheduled inspections: (a) ) Inspections controlled by flight hours may be accomplished within a period beginning 40 flighthours before and ending no later than 40 flight hours after the inspection due time. (b) Inspections controlled by flight hours may be accomplished within a period beginning 25 flighthours before and ending no later than 25 flight hours after the inspection due time. (c) ) Inspections controlled by flight hours may be accomplished within a period beginning 10 flighthours before and ending no later than 10 flight hours after the inspection due time. (d) ) Inspections controlled by flight hours may be accomplished within a period beginning 50 flighthours before and ending no later than 50 flight hours after the inspection due time. (See.

13. The following specifies the Allowable Inspection Tolerances for Learjet scheduled inspections: (a) Inspections controlled by landings or cycles may be accomplished within a period beginning 5 landings or cycles before and ending no later than 5 landings or cycles after the inspection due. (b) Inspections controlled by landings or cycles may be accomplished within a period beginning 10 landings or cycles before and ending no later than 10 landings or cycles after the inspection due. (c) Inspections controlled by landings or cycles may be accomplished within a period beginning 25landings or cycles before and ending no later than 25 landings or cycles after the inspection due. (d) Inspections controlled by landings or cycles may be accomplished within a period beginning 50 landings or cycles before and ending no later than 50 landings or cycles after the inspection due.

14 Which is the major zone 200?. (a) Empennage, FS 378.05 to FS 708.22. (b) Right Wing. (c) Landing Gear and related systems. (d) Fuselage, FS 99.57 to FS 378.05.

15 Which is the major zone 600?. (a) Empennage, FS 378.05 to FS 708.22. (b) Right Wing. (c) Landing Gear and related systems. (d) Fuselage, FS 99.57 to FS 378.05.

16 Which is the major zone 700?. (a) Empennage, FS 378.05 to FS 708.22. (b) Right Wing. (c) Landing Gear and related systems. (d) Fuselage, FS 99.57 to FS 378.05.

17 Which is the major zone 300?. (a) Empennage, FS 378.05 to FS 708.22. (b) Right Wing. c) Landing Gear and related systems. (d) Fuselage, FS 99.57 to FS 378.05.

18 Fuselage station is a horizontal reference designation measuring from?. (a) Fuselage length. FS 12.77 is the reference point at nose of aircraft. (b) Fuselage length. FS 12.77 is the reference point at door of aircraft. (c) Fuselage length. FS 12.77 is the reference point at nose landing gear of aircraft. (d) Fuselage length. FS 12.77 is the reference point at aft bulk head of aircraft.

19 Water line is a vertical reference designation measured parallel to the ground. (a) At the bottom centerline of the outer skin from Frame 32 (FS 124.39) to Frame 27 Fwd. (FS 381.07). (b) At the bottom centerline of the outer skin from Frame 24 (FS 124.39) to Frame 27 Fwd. (FS 381.07). (c) At the bottom centerline of the outer skin from Frame 16 (FS 124.39) to Frame 27 Fwd. (FS 381.07). (d) At the bottom centerline of the outer skin from Frame 8 (FS 124.39) to Frame 27 Fwd. (FS 381.07).

20 Where is the major pressured area?. (a) Empennage, FS 378.05 to FS 708.22. (b) Fuselage, FS 99.57 to FS 356.61. (c) Fuselage, FS 99.57 to FS 378.05. (d) Fuselage, FS 99.57 to FS 465.28.

21 The location of fwd engine beam support is ?. (a) Empennage, FS 378.05 to FS 708.22. (b) Right Wing. (c) WL 65.93 at aircraft Center Line. (d) Fuselage, FS 99.57.

22 The location of level point support on Learjet 60 XR is ?. (a).Fuselage, Frame 41. (b) Fuselage, Frame 40. (c) Fuselage, Frame 30. (d) Fuselage, Frame 25.

23 The location of level point support on Learjet 60 is ?. (a).Fuselage, Frame 41. (b) Fuselage, Frame 40. (c) Fuselage, Frame 30. (d) Fuselage, Frame 25.

24 When you Taxing or towing the airplane, ensure that?. (a).Emergency Exit/Baggage door and lower passenger/crew door are close and latched. (b) Baggage door open. (c) Lower passenger/crew door are close and latched. (d) Lower passenger/crew door are open.

25 When pouching airplane backward, ensure that?. (a). All braking with the towing vehicle. (b) Ensure the battery switches are off to avoid damage to the electric nose steering actuator. (c) Emergency Exit/Baggage door and lower passenger/crew door are close and latched. (d) a ,b and c are correct.

26 When pouching airplane backward, with power on, ensure that?. (a). Ensure the battery switches are off. (b) Ensure the battery switches are on. (c) Ensure the battery switches are on, pull both AC/DC nose steer CB. (d) Nothing happened.

27 The maximum turning radius for the nose wheel steering system is?. (a) 15º either side of center. (b) 30º either side of center. (c) 45º either side of center. (d) 60º either side of center.

27 The controls gust lock ?. (a) Should be installed anytime the airplane is parked. (b) Should be installed anytime the airplane is on fly. (c) Should be installed anytime the airplane is exposed to wind. (d) a and c are correct.

28 Where is located the aircraft identification plate?. (a) The aircraft identification plate is on the LH lower outer portion of the tail cone. (b) The aircraft identification plate is on the RH lower outer portion of the tail cone. (c) The aircraft identification plate is on the LH upper outer portion of the tail cone. (d) The aircraft identification plate is on the RH upper outer portion of the tail cone.

29 The identification plate, supplies?. (a) Color of the plane. (b) Owner name. (c) Model number, serial number, type certificate date and production certificate. (d) Company name.

30 The controls gust lock ?. (a) Should be installed anytime the airplane is parked. (b) Should be installed anytime the airplane is on fly. (c) Should be installed anytime the airplane is exposed to wind. (d) a and c are correct.

31 Where is located the Cabin Control Blower on the Learjet 60 XR ?. (a). Pilot side main panel. (b) Copilot side main panel. (c) Copilot climate panel. (d) Environmental panel RH panel.

32 When the thermo switch close to operate the fan?. (a) The thermo switch close at 90+/- 5 F°. (b) The thermo switch close at 100+/- 5 F°. (c) The thermo switch close at 80+/- 5 F°. (d) The thermo switch close at 110+/- 5 F.

33 The air circulation system consists of a cabin blower, a cockpit blower, and a cockpit blower control box assembly. The air circulation system can be used in conjunction with the auxiliary heaters or the evaporators to heat or cool the circulated air. Is true or false?. (a) True. (b) False.

34 When the thermo switch open to operate the fan?. (a) The thermo switch open at 110+/- 5 F°. (b) The thermo switch open at 100+/- 5 F°. (c) The thermo switch open at 90+/- 5 F°. (d) The thermo switch open at 70+/- 5 F°.

35 Where are located on the Learjet 60 XR the Avionics cooling Fan?. (a) Nose section. (b) Under the floorboards and exhausted under the glare shield. (c) Fw main cabin. (d) Tail cone.

36 Where are located on the Learjet 60 XR the primary outflow valve?. (a) Nose section. (b) Under the floorboards and exhausted under the glare shield. (c) Lower right side of the forward pressure bulkhead. (d) Tail cone.

37 When the thermo switch close to operate the instrument cooling fan?. (a) .70°F. (b) 80F°. (c) 90F°. (d) 100F°.

38 When the FAULT illuminates on pressurization control panel, in auto mode and PRESS SYS Light illuminate on annunciator panel at high altitude?. (a) 9500 ft. (b) 10500 ft. (c) 12500 ft. (d) 14500 ft.

39 When the pressure light illuminates on annunciator panel in MANUAL mode at high altitude?. (a). 9500 ft. (b) 10500 ft. (c) 12500 ft. (d) 14500 ft.

40 When the pressure light illuminates on annunciator panel in MANUAL mode at high altitude?. (a). 9500 ft. (b) 10500 ft. (c) 12500 ft. (d) 14500 ft.

41 When the Oxigen mask deployment?. (a). 9500 ft. (b) 10500 ft. (c) 12500 ft. (d) 14500 ft +/- 250ft.

42 When the temperature in tail cone baggage compartment drops below to ---- both baggage thermostat switches Close. (a). 25°F. (b) 30F°. (c) 35F°. (d) 40F°.

43 When the temperature in tail cone baggage compartment rises above to ---- both baggage thermostat switches Open?. (a). 25°F. (b) 30F°. (c) 35F°. (d) 50F°.

44 What is the major zone 400?. (a) Empennage, FS 378.05 to FS 708.22. (b) Engines. (c) Landing Gear and related systems. (d) Fuselage, FS 99.57 to FS 378.05.

45 What refrigerant use the Learjet 60 XR ?. (a) Water. (b) R-134. (c) R-12. (d) Oil.

46 Cuales son las dimensiones de la aeronave Learjet 60 XR. (a) 60 Ft, alto 18 Ft, distancia entre alas 43 Ft 10 In. (b) largo 58 Ft 8 ½ In, alto 14 Ft 7 In, distancia entre alas 43 Ft 10 In. (c) largo 58 Ft 8 ½ In, alto 14 Ft 7 In, largo 58 Ft 8 ½ In, alto 18 Ft, distancia entre alas 43 Ft 10 In. (d) largo distancia entre alas 45 Ft 10 In.

47 De cuantas fases se componen los chequeos de mantenimiento?. (a) 30. (b) 24. (c) 27. (d) 28.

48 En el sistema eléctrico de la aeronave Learjet 60 XR si se encuentran los inverter fuera de fase ocurre lo siguiente. (a) El último digito del EPM (External power monitor) se convierte en una letra C de color ámbar. (b) ámbar Se enciende una letra C de color en la PFD o MFD. (c) Se enciende una luz ámbar con la letra C en el System Test. (d) Se enciende una luz ámbar con la letra C en el Panel de Control Eléctrico.

49 El sistema eléctrico AC derecho NO está relacionado con ?. (a) Windshield. (b) Nosewheel steering. (c) Spoilers. (d) Mach trim.

50 Cuantas baterías de emergencia pueden estar instaladas en la aeronave. (a) 3. (b) 2o3. (c) 3o4. (d) 2.

51 El sensor de sobre temperatura y relays se abre a cuantos amperios y como cierra. (a) 600 amperios y cierra automáticamente. (b) 700 amperios y cierra automáticamente. (c) 700 amperios y se debe resetear. (d) 600 amperios y se debe resetear.

52. Cual es la ubicación del ajuste de los pedales de piloto y copiloto. (a) En los pedales. (b) En el pedestal. (c) En los extremos del sub panel de piloto y copiloto. (d) En el panel de cb’s.

53 Cual es la presión para la ruptura del disco indicador de sobrepresión de oxigeno. (a) 2700 a 3000 psi. (b) 2600 a 2900 psi. (c) 3000 a 3200 psi. (d) 2900 a 3200 psi.

54 Los elementos de sensación de ubicados calentamiento están en __ y el rango de sensación es de __: (a) Sección central, 255°C. b) Sección inferior cono de cola, 275°C. (c) Cono de cola, 255°C. (d) Sección de nariz, 275°C.

55 El máximo recorrido del Trim Tab es: (a) 8 +/- 1° arriba y abajo. (b) 9 +/- 1° arriba y abajo. (c) 8 + 1° arriba, -2° abajo. (d) 9 + 1° arriba, -2° abajo.

56 Cuando el radio altímetro que mas falla con el. (a) TCAS y Air Data computer. (b) TCAS y Multifuntional Fligt Display. (c) TCAS y IVS. (d) TCAS y TAWS.

57 Cual es el rango de operación del radio altímetro. (a) 0 a 3200 pies. (b) 0 a 3200 pies. (c) 0 a 2500 pies. (d) 0 a 25000 pies.

58 Coloque Falso o verdadero, para que un operador realice operación RVSM se requiere únicamente que la aeronave esté certificada para dicha operación. (a) Verdadero. (b) Falso.

59 De las siguientes inspecciones RVSM cual debe ser realizado con una periodicidad de 12 mese,. (a) Prueba de alineación de los tubos pitot. (b) Inspección de tolerancia de la puerta del compartimiento de avionica. (c) Chequeo funcional del Air Data System. (d) Descarte de los tubos pitot.

60 El APR (Automatic Performance Reserve) cuanto tiempo está limitado. (a) 8 minutos cada vez que es usado. (b) 5 minutos durante toda la vida del motor. (c) 8 minutos durante toda la vida del motor. (d) 5 minutos cada vez que es usado.

61 El conjunto de rotor del motor está soportado por 4 rodamientos principales así: (a) N1 rodamientos 1 y 4, N2 rodamientos 2 y 3. (b) N1 rodamientos 2 y 4, N2 rodamientos 1 y 3. (c) N1 rodamientos 1 y 2, N2 rodamientos 3 y 4. (d) N1 rodamientos 1 y 3, N2 rodamientos 2 y 4.

62 En la sincronización de los motores cual es el motor maestro. (a) Cualquiera puede ser maestro. (b) El motor que tiene el menor N1. (c) El motor con el más alto trim. (d) El motor que tiene el mayor N1.

63 Cual es el tiempo de extensión y retracción del reversible. (a) 1.7 y 4.2 segundos. (b) 2.3 y 4.2 segundos. (c) 2.3 y 2.8 segundos. (d) 1.68 y 2.43 segundos.

64 Donde se encuentra localizado el ELT del Learjet 60XR?. (a) Seccion fuselaje de cola RH. (b) Bodega de carga. (c) Seccion de nariz. d) Seccion fuselaje de cola LH.

65 Que motors se encuntran instalados en el Learjet 60XR?. (a) PT6A-67D. (b) PW JT5D5. (c) JT5. (d) PW 305A.

66 Que fluido hidraulico usa el sistema del Learjet 60 XR ?. (a) MIL-H_5606. (b) Skydrol. (c) Aeroshell 500. (d) MIL-G-!7.

67 Cual es la descriccion mas adecuada para los motores del Learjet 60 XR??. (a) Un compresor axial de tres etapas y una rueda de turbine libre. (b) a lightweight two-spool turbofan engine, featuring a full-length annular bypass duct. (c) Un motor tuebo eje. (d) Un motor jet.

68 Donde se encuentra instalado el generador arranque de la aeronave?. (a) En el montante del motor,parte superior. (b) En la caja de reduccion del Motor. (c) En la parte delantera inferior del compresor en cada motor. (d) En el fuselaje.

69 El equipo de Avionica del Learjet 60 XR es ?. (a) Honnywell 3000. (b) Collins Proline 4. (c) Collins Proline 21. (d) KLN King.

70 Cuando se opera el modo primario del piloto automatico que sistema queda desabiltado?. (a) Yaw Damper. (b) Trust Reverser. (c) Estabilizador Horizontal. (d) Rudder.