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Ryanair
Ryanair’s Boeing 737 NG initial type rating
400 actual type rating technical exam questions. Certain questions are purposefully “incorrect” since they appear this way in the actual exam. Primarily Boeing 737 NG 700/800 questions but also relevant regarding Boeing 737 NG variants. Many airlines use these exact questions in their final technical examinations.
- AIRPLANE GENERALquestion 1 to 36 (36)
- AIR SYSTEMSquestion 37 to 78 (42)
- ANTI-ICE, RAINquestion 79 to 93 (15)
- AUTOMATIC FLIGHTquestion 94 to 117 (24)
- COMMUNICATIONquestion 118 to 124 (7)
- ELECTRICALquestion 125 to 160 (36)
- ENGINES & APUquestion 161 to 198 (38)
- FIRE PROTECTIONquestion 199 to 219 (21)
- FLIGHT CONTROLSquestion 220 to 251 (32)
- FLIGHT INSTRUMENTS, DISPLAYSquestion 252 to 279 (28)
- FLIGHT MANAGEMENT & NAVIGATIONquestion 280 to 313 (34)
- FUELquestion 314 to 335 (22)
- HYDRAULICSquestion 334 to 359 (24)
- LANDING GEARquestion 360 to 372 (13)
- WARNING SYSTEMSquestion 373 to 400 (28)
Ryanair’s Boeing 737 NG initial type rating
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- Incorrect
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Question 1 of 167
1. Question
Category: Airplane generalWhat is the wingtip height of blended wing aircraft?
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Question 2 of 167
2. Question
Category: Airplane generalThe operation of the overwing exit locks is dependent on:
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Question 3 of 167
3. Question
Category: Airplane generalActivated at 14,000 feet, the passenger oxygen masks drop down from the stowage:
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Question 4 of 167
4. Question
Category: Airplane generalWhen are the NO SMOKING signs illuminated?
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Question 5 of 167
5. Question
Category: Airplane generalThe aircraft is on ground and the Flight Recorder Switch is on NORMAL:
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Question 6 of 167
6. Question
Category: Airplane generalWhat happens if you reject takeoff at 100 knots with Autobrakes in RTO?
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Question 7 of 167
7. Question
Category: Airplane generalWhat are the 737-800s maximum latitude certifications:
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Question 8 of 167
8. Question
Category: Airplane generalWhat is the minimum pavement width for a 180 degrees turn?
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Question 9 of 167
9. Question
Category: Airplane generalThe aircraft is on the ground and the Flight Recorder Switch is in NORMAL:
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Question 10 of 167
10. Question
Category: Air systemsThe APU is capable of supplying bleed air conditioning packs:
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Question 11 of 167
11. Question
Category: Air systemsZONE TEMP amber light illumination for CONT CAB indicates:
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Question 12 of 167
12. Question
Category: Air systemsThe maximum differential pressure is:
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Question 13 of 167
13. Question
Category: Air systemsIllumination of an amber COWL ANTI ICE light indicates:
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Question 14 of 167
14. Question
Category: Air systemsWhen does the amber DUAL BLEED Light illuminate?
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Question 15 of 167
15. Question
Category: Air systemsAfter normal engine start, what should be done if the DUAL BLEED light is illuminated:
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Question 16 of 167
16. Question
Category: Air systemsFollowing an unpressurised takeoff, when is the first engine Bleed Switch positioned to ON?
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Question 17 of 167
17. Question
Category: Air systemsWhich systems use engine bleed air for operation?
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Question 18 of 167
18. Question
Category: Air systemsWhat happens when the WING-BODY OVHT TEST Switch is pressed?
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Question 19 of 167
19. Question
Category: Air systemsIf all TEMPERATURE ZONE SELECTORS are positioned to OFF:
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Question 20 of 167
20. Question
Category: Air systemsAn illuminated BLEED TRIP OFF light indicates
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Question 21 of 167
21. Question
Category: Air systemsIn flight with both PACK switched in HIGH:
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Question 22 of 167
22. Question
Category: Air systemsDuring single pack operation with TRIM AIR selected OFF:
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Question 23 of 167
23. Question
Category: Air systemsDuring descent, the pressurization descent mode is activated when:
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Question 24 of 167
24. Question
Category: Air systemsThe amber DUAL BLEED light is illuminated before starting engines. What should you do?
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Question 25 of 167
25. Question
Category: Air systemsWhat is the position of the isolation valve when the ISOLATION VALVE Switch is in AUTO?
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Question 26 of 167
26. Question
Category: Air systemsA panel failure of the Flight Altitude (FLT ALT) Indicator may result in the following indication:
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Question 27 of 167
27. Question
Category: Air systemsThe position indicator of the outflow valves show the position of the valve:
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Question 28 of 167
28. Question
Category: Air systemsWhere are the bleed trip sensors installed?
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Question 29 of 167
29. Question
Category: Air systemsThe Recirculation Fan:
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Question 30 of 167
30. Question
Category: Air systemsThe ISOLATION VALVE switch is set to AUTO, both engine bleeds are ON and both pack switches are in AUTO. The isolation valve:
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Question 31 of 167
31. Question
Category: Air systemsIllumination of the amber BLEED TRIP OFF light indicates what valve has automatically closed?
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Question 32 of 167
32. Question
Category: Air systemsWhile making a no engine bleed air take off and an engine failure occurs, when should the bleed air switches be positioned to ON?
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Question 33 of 167
33. Question
Category: Air systemsThe wing-body overheat light comes on. What is the related master caution warning?
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Question 34 of 167
34. Question
Category: Air systemsRefer to the Cabin/Flight Altitude placard. At cruise altitude FL290, the cabin altitude should read:
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Question 35 of 167
35. Question
Category: Air systemsCruising at FL370. The motorised Overboard Exhaust valve will open in flight if:
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Question 36 of 167
36. Question
Category: Air systemsIn the PACK fail non-normal procedure, the crew selects a warmer temperature in order to:
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Question 37 of 167
37. Question
Category: Air systemsThe ram air system deflector doors:
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Question 38 of 167
38. Question
Category: Air systemsThe amber OFF SCHEDULE DESCENT Light illuminates. What does that indicate?
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Question 39 of 167
39. Question
Category: Air systemsWhat is the differential pressure the pressure controller maintains above 37,000 ft?
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Question 40 of 167
40. Question
Category: Air systemsWhat is the primary source of conditioned air to the cockpit?
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Question 41 of 167
41. Question
Category: Air systemsWhat systems need pneumatic power for operation?
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Question 42 of 167
42. Question
Category: Air systemsDue to a malfunction you are required to return to the airport of departure. To avoid the OFF SCHED DESCENT warning, you reset the FLT ALT. What can you expect?
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Question 43 of 167
43. Question
Category: Air systemsWarm air from the E&E bay is:
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Question 44 of 167
44. Question
Category: Air systemsIn MANUAL pressurization mode, the outflow valve is driven by?
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Question 45 of 167
45. Question
Category: Air systemsA WING BODY OVERHEAT light indicates:
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Question 46 of 167
46. Question
Category: Air systemsWhich systems use engine bleed air for operation?
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Question 47 of 167
47. Question
Category: Air systemsWhat is the position of the Engine Bleed Air Switches during the secure scan flow on the parking checklist:
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Question 48 of 167
48. Question
Category: Air systemsThe right primary pack control fails. The right pack:
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Question 49 of 167
49. Question
Category: Air systemsThe BLEED TRIP OFF light:
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Question 50 of 167
50. Question
Category: Air systemsIn the PACK TRIP OFF non-normal procedure, the crew selects a warmer temperature in order to:
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Question 51 of 167
51. Question
Category: Air systemsA DUCT OVERHEAT light only cause:
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Question 52 of 167
52. Question
Category: Airplane generalThe Cockpit Voice Recorder (CVR) can be erased:
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Question 53 of 167
53. Question
Category: Airplane generalWhat statement is correct about the flight crew oxygen mask in the EMERGENCY position:
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Question 54 of 167
54. Question
Category: Airplane generalWhen the passenger service unit (PSU) is activated, how long can it supply oxygen?
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Question 55 of 167
55. Question
Category: Airplane generalEmergency exit light can be activated from:
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Question 56 of 167
56. Question
Category: Airplane generalIn AUTO, the FASTEN BELTS and RETURN TO SEAT signs:
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Question 57 of 167
57. Question
Category: Airplane generalOperation of the airstairs from the exterior panel with the switch to STANDBY:
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Question 58 of 167
58. Question
Category: Airplane generalThe operation of the over-wing emergency exits depends on:
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Question 59 of 167
59. Question
Category: Airplane generalWhere are the logo lights installed?
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Question 60 of 167
60. Question
Category: Airplane generalAt what cabin altitude is the passenger oxygen system automatically activated?
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Question 61 of 167
61. Question
Category: Airplane generalWhere do you read the flight crew oxygen pressure?
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Question 62 of 167
62. Question
Category: Airplane generalThe Auto position of the Cockpit Voice Recorder (CVR) On/Auto switch:
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Question 63 of 167
63. Question
Category: Airplane generalIf a landing is made with RTO selected:
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Question 64 of 167
64. Question
Category: Airplane generalThe wing span is (-800):
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Question 65 of 167
65. Question
Category: Airplane generalWhen the PASS OXY ON Light is illuminated, what does this indicate?
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Question 66 of 167
66. Question
Category: Airplane generalThe flight crew oxygen system uses auto pressure breathing masks / regulators with pressure breathing starting at:
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Question 67 of 167
67. Question
Category: Airplane generalIllumination of the PSEU fault light on the aft overhead panel will indicate:
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Question 68 of 167
68. Question
Category: Airplane generalThe flight crew oxygen may be as high as:
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Question 69 of 167
69. Question
Category: Airplane generalWhat could cause the amber ANTISKID INOP Light to illuminate?
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Question 70 of 167
70. Question
Category: Airplane generalExtending the airstairs using the exterior system:
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Question 71 of 167
71. Question
Category: Airplane generalThe ISFD is an emergency source of altitude, heading, attitude and airspeed. In case of total electrical failure it is powered by its own battery for:
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Question 72 of 167
72. Question
Category: Airplane generalThe EMERGENCY EXIT LIGHTS Switch in the ARMED position:
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Question 73 of 167
73. Question
Category: Airplane generalThe Flight Crew oxygen pressure can be:
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Question 74 of 167
74. Question
Category: Airplane generalThe Cockpit Voice Recorder uses four independent channels to record flight deck audio for a maximum of:
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Question 75 of 167
75. Question
Category: Airplane generalThe wing-span of the 737-800 is:
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Question 76 of 167
76. Question
Category: Airplane generalDo not attempt to make a turn away from an obstacle within:
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Question 77 of 167
77. Question
Category: Airplane generalFor RVSM operation, the maximum allowable altitude display difference for sea level, between the Captain and F/Os on the ground is?
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Question 78 of 167
78. Question
Category: Airplane generalPushing the ATTEND call switch:
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Question 79 of 167
79. Question
Category: Anti-ice, rainPositioning the WING ANTI-ICE switch to ON in flight:
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Question 80 of 167
80. Question
Category: Anti-ice, rainDual angle-airflow sensors (alpha vanes) provide angle-of-attack information to the stall warning system, autothrottle, autopilot and autoslats are anti-iced:
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Question 81 of 167
81. Question
Category: Anti-ice, rainWhen operating on standby power:
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Question 82 of 167
82. Question
Category: Anti-ice, rainWhich are not heated?
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Question 83 of 167
83. Question
Category: Anti-ice, rainPositioning the ENG ANTI-ICE switch to ON in flight:
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Question 84 of 167
84. Question
Category: Anti-ice, rainThe aircraft experiences a loss of both engine driven generators. Which one is true?
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Question 85 of 167
85. Question
Category: Anti-ice, rainAll window heat is selected ON. The green window heat ON light for the Right Side Window extinguishes. The likely reason is:
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Question 86 of 167
86. Question
Category: Anti-ice, rainThe R ELEV PITOT Light is illuminated and PROBE HEAT switches are ON. What does this indicate?
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Question 87 of 167
87. Question
Category: Anti-ice, rainThe window heat PWR TEST:
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Question 88 of 167
88. Question
Category: Anti-ice, rainThe wing anti-ice system provides bleed air to:
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Question 89 of 167
89. Question
Category: Anti-ice, rainThe alpha vanes provide angle-of-attack information to the stall warning system, auto throttle, auto pilot, auto slats and are anti-iced:
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Question 90 of 167
90. Question
Category: Anti-ice, rainWhich window(s) are heated with the LEFT FWD WINDOW HEAT switch ON?
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Question 91 of 167
91. Question
Category: Anti-ice, rainWhat is the maximum airspeed limit according MEL, when WINDOW HEAT is inoperative for window nr 4?
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Question 92 of 167
92. Question
Category: Anti-ice, rainRefer to the thermal anti-ice (TAI) CDS indication. TAI is shown above each N1 indicator:
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Question 93 of 167
93. Question
Category: Anti-ice, rainWing anti-ice
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Question 94 of 167
94. Question
Category: CommunicationTo receive NAV and ADF voice and range audio:
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Question 95 of 167
95. Question
Category: CommunicationAntenna switching from tail antenna to nose antenna occurs when:
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Question 96 of 167
96. Question
Category: CommunicationWhen the Audio System is operating in the degraded mode:
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Question 97 of 167
97. Question
Category: CommunicationOn the ground, for primary ATC communication:
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Question 98 of 167
98. Question
Category: CommunicationIn degraded mode, what are the combinations for transmission and reception at the degraded station?
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Question 99 of 167
99. Question
Category: CommunicationPushing VHF TEST switch on the radio tuning panel:
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Question 100 of 167
100. Question
Category: CommunicationWhen the Captains audio control panel is operating in degraded mode:
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Question 101 of 167
101. Question
Category: Automatic FlightThe Automatic Flight System (AFS) consists of:
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Question 102 of 167
102. Question
Category: Automatic FlightThe Air Data Inertial Reference System (ADIRS) produces the following flight data:
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Question 103 of 167
103. Question
Category: Automatic FlightDuring AUTO LAND, at which radio altitude should the flare mode be engaged?
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Question 104 of 167
104. Question
Category: Automatic FlightWhen control wheel pressure is released during CWS roll operation, the aircraft will roll wings level when the bank angle is:
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Question 105 of 167
105. Question
Category: Automatic FlightWhat is the latest altitude (AGL) CMD that can be selected on the second autopilot to execute a dual channel A/P approach?
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Question 106 of 167
106. Question
Category: Automatic FlightWhich is the correct mode on the FMA? Condition: After takeoff, A/P engaged, before flaps up. (Thrust: Roll: Pitch)
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Question 107 of 167
107. Question
Category: Automatic FlightHow many independent Flight Control Computers (FCCs) are there in the Autopilot Director System (AFDS)?
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Question 108 of 167
108. Question
Category: Automatic FlightNormally, N1 limits and target N1 values are provided to the A/T by the:
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Question 109 of 167
109. Question
Category: Automatic FlightDuring an ILS approach below 1,000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert:
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Question 110 of 167
110. Question
Category: Automatic FlightWhich A/T modes permit manual thrust changes without A/T interference?
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Question 111 of 167
111. Question
Category: Automatic FlightWhich mode must be armed before the second autopilot can be selected during a dual channel A/P approach?
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Question 112 of 167
112. Question
Category: Automatic FlightIn normal operation, what provides the A/T system with N1 limit values?
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Question 113 of 167
113. Question
Category: Automatic FlightUnder speed limiting (flashing A) appears:
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Question 114 of 167
114. Question
Category: Automatic FlightWhich of the following occurs when a TO/GA switch is pressed once below 2000 feet radio altitude for an automatic go-around from an ILS channel A/P approach and FLARE armed?
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Question 115 of 167
115. Question
Category: Automatic FlightWhat happens with the IAS/MACH display on the MCP if SPD INTV switch is pushed during VNAV operation:
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Question 116 of 167
116. Question
Category: Automatic FlightAt what altitude will both A/Ps automatically disengage if FLARE is not armed during an ILS dual channel approach:
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Question 117 of 167
117. Question
Category: Automatic FlightWhat pitch mode is annunciated in the FMA after takeoff when the autopilot is first engaged in CMD?
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Question 118 of 167
118. Question
Category: Automatic FlightTwo independent radio altimeters provide radio altitude to the respective FCCs. With one radio altimeter inoperative:
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Question 119 of 167
119. Question
Category: Automatic FlightLNAV will automatically disengage:
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Question 120 of 167
120. Question
Category: Automatic FlightAfter a normal take-off, what pitch command can you expect from the F/D?
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Question 121 of 167
121. Question
Category: Automatic FlightIf the autopilot ALT HOLD mode is manually overridden with control column pressure, which of the following occurs?
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Question 122 of 167
122. Question
Category: Automatic FlightThe autopilot disengages if FLARE mode is not armed by:
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Question 123 of 167
123. Question
Category: Automatic FlightAfter lift-off, the A/T remains in THR HLD until:
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Question 124 of 167
124. Question
Category: Automatic FlightWith VNAV engaged, the AFDS pitch and A/T modes are commanded by the:
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Question 125 of 167
125. Question
Category: ElectricalThe TR Unit light will illuminate in flight if:
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Question 126 of 167
126. Question
Category: ElectricalWhich bus supplies electrical power to the auxiliary battery charger:
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Question 127 of 167
127. Question
Category: ElectricalNormal DC indications are:
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Question 128 of 167
128. Question
Category: ElectricalOne basic principle of operation for the 737 electrical system is:
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Question 129 of 167
129. Question
Category: ElectricalWhen AC power is not available, the main battery energizes the hot battery and:
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Question 130 of 167
130. Question
Category: ElectricalIf ON DC on left IRS mode selector unit comes ON steady it means:
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Question 131 of 167
131. Question
Category: ElectricalHow are the Engine Bleed Air valves powered?
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Question 132 of 167
132. Question
Category: ElectricalDuring primary charge cycle operation, battry voltage can be as high as:
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Question 133 of 167
133. Question
Category: ElectricalWith the STANDBY POWER switch in the AUTO position, loss of both engine driven generators and APU generator will result in that AC standby bus is powered by battery through static inverter, and DC standby bus is powered by battery…
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Question 134 of 167
134. Question
Category: ElectricalA take off is performed with the APU powering both transfer buses:
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Question 135 of 167
135. Question
Category: ElectricalOn the ground, with the BATTERY switch OFF and STANDBY POWER Switch in BAT, the switched hot battery bus is:
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Question 136 of 167
136. Question
Category: ElectricalBlue illumination of APU GEN OFF BUS means:
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Question 137 of 167
137. Question
Category: ElectricalThe ELEC light will illuminate in flight if:
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Question 138 of 167
138. Question
Category: ElectricalThe left IRS is electrically powered from:
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Question 139 of 167
139. Question
Category: ElectricalThe cross bus tie relay automatically opens at glide slope capture to:
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Question 140 of 167
140. Question
Category: ElectricalElectrical power to start the APU comes from:
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Question 141 of 167
141. Question
Category: ElectricalIllumination of the BAT DISCHARGE light indicates:
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Question 142 of 167
142. Question
Category: ElectricalIllumination of the STANDBY POWER OFF lights indicates:
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Question 143 of 167
143. Question
Category: ElectricalWhen the STANDBY POWER Switch is OFF:
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Question 144 of 167
144. Question
Category: ElectricalAs part of the preflight procedure, you are about to test the STALL warning. For this to be possible, an AC source must have powered the Aircraft for a minimum of approximately:
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Question 145 of 167
145. Question
Category: ElectricalIf the APU is the only source of electrical power:
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Question 146 of 167
146. Question
Category: ElectricalThe TRs (Transformer rectifier) converts:
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Question 147 of 167
147. Question
Category: ElectricalGalley busses are powered from:
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Question 148 of 167
148. Question
Category: ElectricalThe AC Standby Bus is powered by:
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Question 149 of 167
149. Question
Category: ElectricalWith normal power source on the buses, placing the battery switch to OFF will remove power from:
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Question 150 of 167
150. Question
Category: ElectricalThe right IRS is electrically powered from:
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Question 151 of 167
151. Question
Category: ElectricalIllumination of the GND POWER AVAILABLE light indicates:
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Question 152 of 167
152. Question
Category: ElectricalMoving the battery switch to OFF automatically shuts down the APU:
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Question 153 of 167
153. Question
Category: ElectricalThe blue APU GEN BUS light will illuminate:
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Question 154 of 167
154. Question
Category: ElectricalThe GROUND POWER AVAILABLE light will extinguish when:
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Question 155 of 167
155. Question
Category: ElectricalSwitching the CAB/UTIL switch OFF removes all 115v AC from the gally busses and:
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Question 156 of 167
156. Question
Category: ElectricalIllumination of the STANDBY POWER OFF lights indicates:
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Question 157 of 167
157. Question
Category: ElectricalThe cross bus tie relay:
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Question 158 of 167
158. Question
Category: ElectricalWhen the aircraft batteries are the only source of power:
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Question 159 of 167
159. Question
Category: ElectricalFor ground service, a ground service switch is placed:
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Question 160 of 167
160. Question
Category: ElectricalOn the ground, the TR UNIT amber light illuminates if:
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Question 161 of 167
161. Question
The APU may be used as a pneumatic source up to:
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Question 162 of 167
162. Question
Once the thrust reverse auto-stow circuit is activated:
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Question 163 of 167
163. Question
During battery start, when does the EEC start to operate?
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Question 164 of 167
164. Question
During engine start, the maximum time allowance for EGT indication after start lever is moved to idle is:
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Question 165 of 167
165. Question
If a crossfeed start is required during in flight starting, the X-BLEED START indication will be displayed above:
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Question 166 of 167
166. Question
During a normal engine start:
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Question 167 of 167
167. Question
When the EEC is not powered, following engine indications are displayed directly from the engine sensors:
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