HH-60G Plt QUAL MQF 2015_Cards.txt

  1. 1(10). With the SAS/FPS computer, is required for turn coordination to disengage and transition to heading hold.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-69 Chap: 1




    C. airspeed less than 60 KIAS
  2. 2(11). If the Ground BITE check (AFCC) is inadvertently initiated,________.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-70 Chap: 1 Para: WARNING




    C. do not takeoff for approximately 2 minutes to ensure FPS authority has been reenabled
  3. 3(12). Flight near high power RF emitters such as microwave antennas or shipboard radar may cause uncommanded AFCS and/or stabilator inputs.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-79 Chap: 1 Para: NOTE
    A. True
    B. False
    A. True
  4. 4(172). If _______ of the stabilator check fails, do not fly the helicopter.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-20 WARNING Chap: 2




    B. any part
  5. 5(9). With the AFCC,______is required for turn coordination to disengage and transition to heading hold.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-69 Chap: 1




    D. all of the above
  6. 6(151). Do not conduct hoist training with the hoist operator's intercom inoperative.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.2.4

    A. True
    B. False
    A. True
  7. 7(153). For live hoist training, hoist riders will not be lifted higher than _____ feet over terrain, obstacles, or water; but may be lifted up to ____ feet to meet
    unique training requirements with concurrence of both the Aircraft Commander and Team Leader.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.2.2




    A. 25, 50
  8. 8(154). ______ determine eligibility of personnel authorized to ride the hoist during training.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.2.1




    D. Unit Commanders
  9. 9(176). Once the tankers assume _______, the ______ will be responsible for all navigation, weather avoidance, and position reporting.
    Ref: ATP-56(B) Pg: 2-3 Chap: Part 3 Para: 204 b.




    D. formation lead, tankers
  10. 10(177). Overt ______ may cause excessive glare during NVG join ups.
    Ref: ATP-56(B) Pg: 4-2 Chap: Part 3 Para: 403 b. (2) NOTE




    B. anti-collision lights
  11. 11(179). During HAAR Formation Option 2 (Trail), the helicopter flight separates into two elements in trail. Standard spacing between helicopter
    elements is ____; however, it may be as little as _____ and should be determined based on mission requirements such as number of receivers, terrain,
    forecast visibility, and light conditions.
    Ref: ATP-56(B) Pg: 3-1 Chap: Part 3 Para: 303 a.




    B. 2nm, 0.5nm
  12. 12(180). If visual and electronic contact are lost after the tanker is within 3 NM of the receiver, the tanker will immediately call "CONTACT LOST",
    establish a minimum _____ foot vertical separation and _____ of the track heading.
    Ref: ATP-56(B) Pg: 4-3 Chap: Part 3 Para: 405 a. (1) (a) (i-iii




    C. 500/turn 45 degrees right
  13. 13(181). Under no circumstances should the pilot stare at the _____ as this will result in poor aircraft control and may result in spatial disorientation.
    Ref: ATP-56(B) Pg: 2-4 Chap: Part 3 Para: 206 b. WARNING




    D. drogue
  14. 14(182). Wing/prop turbulence can cause uncontrolled settling. If this occurs while connected to the drogue, disconnect immediately.
    Ref: ATP-56(B) Pg: 2-3 Chap: Part 3 Para: 206 b. WARNING

    A. True
    B. False
    A. True
  15. 15(183). A counter-clockwise rotating drogue could result in partial or complete unthreading of the probe nozzle.
    Ref: ATP-56(B) Pg: 2-5 Chap: Part 3 Para: 206 b. CAUTION

    A. True
    B. False
    B. False
  16. 16(184). Lengths of pod hoses vary between _____ and _____ depending on the system and use; 24 m (80 ft) is typical of an integral system hose.
    Ref: ATP-56(B) Pg: 3-2 Chap: Part 1 Para: 302 c. (1)




    B. 15 m (50 ft)/27 m (90 ft)
  17. 17(185). If a crossover is required, the receiver pilot will move to the outside of the tanker wing tip, _____ feet aft of the horizontal
    stabilizer and increase altitude a minimum of _____ feet above the tanker's vertical stabilizer.
    Ref: ATP-56(B) Pg: 2-3 Chap: Part 3 Para: 205




    A. 100/50
  18. 18(186). Due to distraction and the difficulty of maintaining lateral separation, two receivers will not disconnect or fly in the _____ position simultaneously.
    Ref: ATP-56(B) Pg: 2-7 Chap: Part 3 Para: 208 b. WARNING




    A. astern
  19. 19(187). The ARCP (HAAR ONLY) is defined as _____.
    Ref: ATP-56(B) Pg: 1A-2 Chap: Part 1 Para: Terms and Definition




    D. normally the earliest point the tanker can pass abeam the receiver during join-up
  20. 20(188). When conducting RV procedures, both the receivers and the tankers should plan to arrive at the ARCP on time; however,
    if a deviation is required, receivers should arrive at the ARCP _____ and tankers should arrive at the ARCP _____.
    Ref: ATP-56(B) Pg: 2-2 Chap: Part 3 Para: 203 b.




    A. earlier (no more than 1 minute)/later (no more than 1 minute)
  21. 21(189). Disconnect is approximately _____feet above the contact position.
    Ref: ATP-56(B) Pg: 2-5 Chap: Part 3 Para: 207




    A. 5 - 10
  22. 22(190). One White light from the tanker indicates _____ to the receiver.
    Ref: ATP-56(B) Pg: 5A-4 Chap: Part 3 Para: Table 5A-4




    C. "proceed to observation"
  23. 23(191). The AAR Abort Point is defined as _____.
    Ref: ATP-56(B) Pg: 1A-2 Chap: Part 1 Para: Terms and Definition




    D. a planned point along the receiver track at which the receiver must divert, if he is not in contact receiving fuel
  24. 24(192)._____ is the minimum acceptable equipment for conducting electronic RV (HAAR).
    Ref: ATP-56(B) Pg: 2-1 Chap: Part 3 Para: 202 b.




    D. all of the above are acceptable minimum equipment
  25. 25(193)._____ is the command given by the tanker to receiver, either verbally or by signal, instructing receiver to disengage from tanker refueling equipment.
    Ref: ATP-56(B) Pg: 1A-6 Chap: Part 1 Para: Terms and Definition




    C. "Disconnect"
  26. 26(194). During a "Tobaggan" procedure, the rate of descent is between _____ and _____ feet per minute and this should be used
    unless tanker or receiver requests otherwise.
    Ref: ATP-56(B) Pg: 1A-13 Chap: Part 1 Para: Terms and Definition




    D. 300/500
  27. 27(195). A planned geographic point prior to the RVCP to which tankers and receivers time independently to effect an arrival at the RVCT is the _____.
    Ref: ATP-56(B) Pg: 1A-11 Part 1 Chap: Part 1 Para: Terms and Definition




    A. RVIP
  28. 28(196). The Observation Position is defined as a position to the left or right of the tanker, _____ of the wingtip and slightly above and ____ the tanker horizontal stabilizer.
    Ref: ATP-56(B) Pg: 1A-8 Chap: Part 1 Para: Terms and Definition




    A. outboard, behind
  29. 29(197). Emission Option ______ (Emission Out) is defined as: No emitters will be used unless specifically authorized by the plan that the HAAR is supporting (ATO, SPINS, Rules of Engagement (ROE), Operations plan, Safe Passage procedures, or other mission directive).
    Ref: ATP-56(B) Pg: 5A-1 Chap: Part 3 Para: Figure 5A-1




    B. 4
  30. 30(198).______ is defined as: Any and all emitters are authorized, ie full RT for training purposes adding any timing that would affect the RV.
    Ref: ATP-56(B) Pg: 5A-1 Chap: Part 3 Para: Figure 5A-1




    B. Emission Option 1 - (HAAR)
  31. 31(199). Emission Option _____ (Silent R/T) is defined as: Radio silent operations including formation, RV and HAAR. The use of other emitters is
    authorized unless specifically prohibited.
    Ref: ATP-56(B) Pg: 5A-1 Chap: Part 3 Para: Figure 5A-1




    D. 3 (HAAR)
  32. 32(200). A _____ is made when the probe engages the drogue.
    Ref: ATP-56(B) Pg: 1A-5 Chap: Part 1 Para: Terms and Definition




    B. Contact
  33. 33(4). During Aerial Refueling if the OVERFLOW indicator on the fuel management panel illuminates, the following corrective action should be taken ____.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-37 Chap: 1




    C. hold the MAIN switch to SHUTOFF
  34. 34(5). The probe valve can be opened to on-load fuel through a retracted probe with the helicopter on the ground by _____.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-48 Chap: 1




    B. activation of the left WOW switch
  35. 35(2). The FUEL PUMP switch should be at APU BOOST for all APU operations.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-15 Chap: 1

    A. True
    B. False
    A. True
  36. 36(46). The following corrective action should be accomplished in order to recover from a vortex ring state.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 6-2 Chap: 6




    D. both A and C
  37. 37(6). If the APU generator is the sole source of AC power all equipment may be operated except
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-50 Chap: 1 Para: NOTE




    C. both A and B
  38. 38(7). When the #1 AC generator is inoperative and BACKUP PUMP PWR circuit breaker is out for any reason, _____ must be shut off
    before resetting the circuit breaker.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-51 Chap: 1 Para: CAUTION




    A. BACKUP PUMP switch
  39. 39(16). The crash axe is located ______.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-95 Chap: 1




    A. AG's console
  40. 40(173). A boost servo malfunction _____ be accompanied by illumination of the BOOST SERVO OFF caution light.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-37 NOTE Chap: 3




    C. may or may not
  41. 41(174). Weapon Systems Emergencies: A _____ is the complete failure of the weapon to fire. This is not dangerous,
    but must be treated as a malfunction in the firing mechanism or a faulty round.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-53 Chap: 3




    D. misfire
  42. 42(26). Loss of DC primary power will result in the engine anti-ice and engine inlet anti-ice valves failing to the _____ position.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-15 Chap: 3 Para: WARNING




    A. open
  43. 43(27). During autorotations, pitch attitudes from a hover attitude to _____ degrees nose-up at the point of touchdown normally result in a safe landing.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-22 Chap: 3




    B. 25
  44. 44(28). Do not respond to ENG OUT audio and warning lights until checking _____.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-24 Chap: 3 Para: WARNING




    D. both A and B
  45. 45(29). If AC electrical power is not available, only the _____ engine compartment has fire protection. Additionally only the _____ fire bottle is capable of being discharged.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-23 Chap: 3 Para: WARNING




    C. #1; reserve
  46. 46(30). The minimum rotor speed for a single-engine go-around is _____ % Nr.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-26 Chap: 3




    A. 95
  47. 47(31). If the airspeed fault advisory light is illuminated, continued flight above _____ KIAS with the stabilator in the AUTO mode is unsafe.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-33 Chap: 3 Para: WARNING




    D. 70
  48. 48(32). _____ is the first step for both #1 or #2 FUEL PRESS CAUTION LIGHT and #1 or #2 FUEL FLTR BYPASS CAUTION LIGHT ON checklist.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-34 Chap: 3




    B. Fuel Selector (affected engine) - Select alternate tank. (DIR or XFD)
  49. 49(33). _____ should be done when #1 RSVR LOW and #1 HYD PUMP caution lights illuminate with BACKUP PUMP ON advisory light on, followed by
    BACKUP RSVR LOW caution light on.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-36 Chap: 3




    B. SVO OFF switch - 1st STG
  50. 50(34). _____ is the first step of the BOOST SERVO MALFUNCTION checklist.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-37 Chap: 3




    C. BOOST switch - OFF
  51. 51(35). If tail rotor control is lost, do not use aerodynamic braking to slow the helicopter after touchdown.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 3-52 Chap: 3 Para: WARNING

    A. True
    B. False
    A. True
  52. 52(1). The HMU provides Ng overspeed protection, _____ if Ng reaches 110% +/- 2.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-3 Chap: 1




    C. shutting off all fuel flow with no possible restart until maintenance corrective action
  53. 53(169). With the throttle in ECU/DEC LOCKOUT, _____ is deactivated and the _____ must be manually controlled.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-10 Chap: 1




    B. Automatic TGT Limiting System, TGT
  54. 54(18). If ENG INLET ANTI-ICE ON light goes on with ENG ANTI-ICE NO. 1 and NO. 2 switches in the OFF position,
    it indicates that heat is being applied to that engine and a malfunction exists.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-113 Chap: 1

    A. True
    B. False
    A. True
  55. 55(8). Which of the following functions does the mixing unit provide as a result of increased collective?
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-62 Chap: 1




    D. both A and C
  56. 56(170). Auxiliary Tanks: If the 200 Gallon Internal Auxiliary Fuel Tank contains more than ____ of its total fuel capacity,
    the lower cargo rings structure securing the left and right restraint beams may fail on impact with the ground, causing the tank to dislodge.
    This causes an increase in the probability and severity of injury.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-31 WARNING Chap: 1




    D. 58%
  57. 57(3). When using fuel without icing inhibitor, avoid flying at altitudes where indicated OAT is below _____ to preclude fuel system icing.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-27 Chap: 1 Para: CAUTION




    D. 0°C
  58. 58(110). Helicopters equipped with a _____ that provides sufficient light for a landing may substitute that for an operable landing light.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 5.20.5




    B. searchlight
  59. 59(117). Deviations from AFI 11-2HH-60V3 require specific approval of the _____ unless an urgent requirement or an aircraft emergency dictates otherwise.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 1.3




    D. MAJCOM/A3 (NGB: NGB/A3)
  60. 60(118). The Aircraft Commander is responsible for all of the following except ______.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 2.1




    B. Approving deviations from AFI 11-2HH-60V3 during routine mission accomplishment.
  61. 61(119). Passengers will not be carried on flights involving practice emergency procedure training.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 2.7.1

    A. True
    B. False
    A. True
  62. 62(120). Concerning MEP, unless otherwise stated in MAJCOM supplements to AFI 11-401, _____ or equivalent with
    Operational Control (OPCON) is the approving authority.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 2.8.1




    B. OG/CC
  63. 63(17). When WINDSHIELD ANTI-ICE switch is on, and there is windshield ice build up, it indicates that the monitor has turned off the system,
    the following corrective action should be taken ______.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-113 Chap: 1




    A. WINDSHIELD ANTI-ICE PILOT, CTR, and COPILOT switches must be placed OFF and then ON
  64. 64(171). Maintain positive control of the engine cowling/work platform when opening and closing. Do not lean on vertical arm of cowling.
    Do not exceed _____ pounds of total weight on platform. Individual on platform will not exceed ______ pounds.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-6 WARNING Chap: 2




    D. 400, 250
  65. 65(97). A PIC may deviate from any flight rule only when ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 1.7




    D. all of the above
  66. 66(98). The following are approved types of flight logs ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 2.5




    D. all of the above
  67. 67(100). When two aircraft are approaching head-on, each shall alter course to the ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 5.7.3




    D. right
  68. 68(109). If weather prevents continued flight under VFR on the planned route, the PIC will alter the route of flight as necessary,
    so as to continue operations under VFR ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 7.1.3




    D. all of the above
  69. 69(111). Avoid thunderstorm activity by any means available by at least _____ laterally below FL 230.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 5.26.3.1




    B. 10 NM
  70. 70(112). Helicopters operating in class G airspace below 1200 ft AGL adhere to the following cloud clearance and visibility ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: TABLE 7.1




    C. both A and B
  71. 71(163). The final responsibility regarding equipment required for a mission rests with the _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.18.3




    D. Aircraft Commander
  72. 72(47). When visible moisture is present, pitot heat, engine anti-ice, blade de-ice and windshield anti-ice should be
    turned on when at or below _____ degrees C. These systems must be turned on at or below ______ degrees C.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 7-1 Chap: 7




    C. 10; 4
  73. 73(48). If high engine oil pressure is observed during initial start in cold weather, accomplish the following ______.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 7-4 Chap: 7




    B. run engine at idle until pressure is within limits
  74. 74(49). During hot weather ground operations if engine oil pressure falls into the red gauge range and/or the engine oil
    pressure caution light comes on when the throttle is in IDLE, accomplish the following ______.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 7-5 Chap: 7




    D. slightly advance the throttle, if engine oil pressure caution light extinguishes, oil pressure is acceptable
  75. 75(50). During salt water operations, the rate of salt build up in engines is greatest in winds of ______knots.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 7-11 Chap: 7




    A. 8 to 12
  76. 76(14). In flight which of the following caution/advisory lights will indicate a hydraulic leak test was attempted ______.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-84 Chap: 1




    C. BACKUP RSVR LOW
  77. 77(102). Helicopter pilots must use the published visibility minimums for "Copter Only" approaches as published.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.6.4

    A. True
    B. False
    A. True
  78. 78(104). The required climb gradient for a selected IFR departure is ______ (if a higher gradient is not published) to the appropriate minimum IFR altitude.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.12.10.4




    A. 200 ft/NM
  79. 79(105). For an airport to qualify as an alternate, the worst forecasted prevailing weather conditions (ETA +/- 1 hour) must meet or exceed ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.8.1.2




    A. a ceiling 200 ft. above, and a visibility of at least 1 SM above, the lowest compatible published landing minimum.
  80. 80(106). For an airfield without a Published Instrument Approach Procedure to qualify as an alternate, the forecast weather
    for the ETA (+/- ______ ) must permit a VFR descent from the MIA to a VFR approach and landing.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.8.2




    A. 1 hour
  81. 81(107). Pilots may select an airport as an alternate that includes a temporary condition in the forecast if the condition is due to _____.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.8



    C. both A and B
  82. 82(108). For airports without a published instrument approach, pilots may not ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.5.2




    A. file IFR to the airport
  83. 83(113). For IFR takeoff minimums for training flights, weather must be equal to or higher than ______.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.3.2.1




    B. the published approach minimums (ceiling and visibility)
  84. 84(114). If unable to meet or exceed the required IFR departure climb gradient, a VMC climb to the IFR MEA or a
    VFR departure are authorized as a last resort for mission accomplishment.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.12.10.3

    A. True
    B. False
    A. True
  85. 85(115). If the airport does not have an authorized IFR departure method, then ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.12.9




    D. an IMC departure under IFR is not authorized
  86. 86(116). The term "Radar contact" by a controller means the aircraft has been identified on radar, but does not mean that
    terrain and obstruction clearance responsibility has transferred to the controller.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.12.6.3

    A. True
    B. False
    A. True
  87. 87(148). The use of a hood or other artificial vision-restricting device is authorized ______.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 5.1.1




    D. never
  88. 88(149). For precision instrument approach procedures, all of the following are required PNF calls except ______.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 5.2.3




    A. "500 feet above DH"
  89. 89(150). Any crewmember will announce heading deviations of _____ degrees, airspeed deviations of _____ knots, or when altitude deviation exceeds _____ feet.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 5.2.5




    A. 10, 10, 100
  90. 90(19). After about a 2 minute warm up, the radar altimeter altitude pointer will be _____ feet, and the digital readout will be _____ feet.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-557 Chap: 1




    B. 0+/-5; 0 to +3
  91. 91(99). Flights conducted in IMC require ______.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 2.15.2




    C. A and B
  92. 92(15). If the helicopter has become airborne (the WOW switch has cycled) the Mode 4 codes will be lost if power is removed unless _____.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-84 Chap: 1




    A. specifically held with the HOLD function
  93. 93(175). To prevent APU overheating, APU operation at an OAT of ____ degrees Celsius and above with engine and rotor operating, is limited to _____ minutes.
    With engine and rotor not operating, the APU may be operated continuously up to an OAT of ____ degrees Celsius.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-15 Chap: 5




    A. 43, 30, 51
  94. 94(36). Maximum allowable Nr for normal operations and emergency procedures training is ______%. Maximum allowable Nr for functional check flights is _____%.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-1 Chap: 5




    C. 110; 120
  95. 95(37). The maximum wind velocity, from any direction, for rotor start or stop is ______ KIAS.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-1 Chap: 5




    D. 45
  96. 96(38). Avoid operation in the _____ and _____ Nf ranges.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-2 Chap: 5




    A. 20%-40% and 60%-90%
  97. 97(39). Routine rotor brake stops shall be done between _____% Nr, and should be limited to ____ psi.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-7 Chap: 5




    B. 30 to 50; 180
  98. 98(40). The maximum airspeed with one engine inoperative is _____ KIAS.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-9 Chap: 5




    B. 130
  99. 99(41). _____ is the sideward/rearward flight limit into the wind, when combined with wind speed.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-9 Chap: 5




    D. 45 KIAS
  100. 100(42). _____ is the maximum airspeed to extend either searchlight.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-10 Chap: 5




    A. 100 KIAS
  101. 101(43). The maximum airspeed authorized with cabin doors open, with soundproofing removed aft of station 379 or with
    soundproofing retention kit installed is _____.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-10 Chap: 5




    D. 145 KIAS
  102. 102(44). The cabin heater should be turned off before starting descents in icing conditions.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-15 Chap: 5

    A. True
    B. False
    A. True
  103. 103(45). The blade deicing system shall not be operated at an OAT above ______.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-15 Chap: 5




    A. 21 deg C
  104. 104(121). The VFR weather training minimums are ______and IAW AFI 11-202 for night practice emergency procedures.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.3.1.1-3.3.1.2




    A. 700/1 (Day) / 700/2,(NVG) / 1000/3 (Night Unaided)
  105. 105(122). IFR Takeoff Minimums for training flights require weather equal to or higher than _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.3.2.1




    A. published approach minimums (ceiling and visibility), but no less then 1/2 mile (RVR 2400) at the departure airfield
  106. 106(123). An IFR departure alternate airfield for operational flights _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.3.2.2

    A. should be within 60 minutes flight time
    B. must have prevailing weather equal to or better than the lowest published approach ceiling and visibility minimum (no lower than 1200 RVR),
    and forecast to remain so for 1 hour after the time you expect to arrive
    C. is not required if visibility at the departure point is at or above the published visibility minimums required for the appropriate aircraft
    category for an available approach
    D. all of the above
    D. all of the above
  107. 107(124). For instrument flight planning purposes, when _____ criterion is used, or when destination weather information may be unreliable,
    fuel requirements for descent, approach, and missed approach will be _____ pounds. Ensure sufficient fuel remains to arrive at the alternate with appropriate reserves.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.5.2




    C. visibility-only, 500
  108. 108(125). Minimum en route altitude for unaided night navigation is 500 feet AHO within 5 NM for _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.10.2




    C. both A and B
  109. 109(126). Helicopter crewmembers will wear survival vest/Load Bearing Vest (LBV) on all flights departing the local traffic pattern.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.12.2

    A. True
    B. False
  110. 110(127). A new or corrected DD Form 365-4, Weight and Balance Form F, need not be recomputed provided the initial takeoff gross weight (item 16)
    is not changed by more than ____pounds.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.17.3




    B. 500
  111. 111(128). Malfunctions of the Enhanced Fuel Quantity Indicating (EFQI) system should not affect main fuel quantity indications and do not restrict
    the crew from flying the aircraft. However, if mission requirements dictate the use of auxiliary fuel with a malfunction in the EFQI then _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.23.2




    D. Both A and B
  112. 112(92). If an alternate is required, fuel for approach and missed approach must be included in the total flight plan fuel when _____.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 2.4.3.1




    C. visibility only weather criteria is used
  113. 113(93). Regarding helicopter operations, the required visibility minimum may be reduced to _____ of the published visibility minimums for category A aircraft.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.6.4




    B. one-half
  114. 114(94). Regardless of weather, pilots must designate an alternate on all IFR flight plans when filing to a destination where _____.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.7.2




    D. all of the above
  115. 115(129). Passengers will not occupy a seat with access to a set of flight controls.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.3

    A. True
    B. False
    A. True
  116. 116(130). Aircraft will avoid taxi obstructions by ______feet without wing walkers and by ____feet with wing walkers.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.8.1




    D. 25, 10
  117. 117(131). The maximum hover taxi speed is _____, or as required when directed by ATC (N/A for air taxi).
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.8.3




    B. 15 KGS
  118. 118(132). The maximum ground taxi speed is ____ KGS, or as required when directed by ATC.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.8.4




    A. 10
  119. 119(133). During rotor turning crew changes, the new crew will review _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.9.3




    A. aircraft forms, weight and balance, asterisk item before takeoff items and TOLD
  120. 120(134). If the aircraft commander becomes doubtful of the helicopter's airworthiness or encounters hazardous weather conditions, a ____ should be accomplished.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.13




    A. precautionary landing
  121. 121(135). In addition to flight manual prohibited maneuvers, all of the following maneuvers will not be practiced in the aircraft except ____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.1




    C. throttle reduction on a single engine
  122. 122(137). Accomplish all emergency procedures to _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.5




    D. all of the above
  123. 123(138). Marginal power and maximum performance takeoffs will be terminated when clear of the simulated obstacle and above
    safe single engine airspeed (or _____ KIAS if safe single engine airspeed is not available).
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.6 - 4.20.3.7




    B. 80
  124. 124(139). When practicing a rolling takeoff, simulate max power _____percent below hover power.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.8



    D. 10
  125. 125(140). Initiate practice steep approaches at ____, _____, and a _____degree apparent angle.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.11




    A. 300 feet AGL, 50 knots KGS, 45
  126. 126(141). The maximum rate of descent on a steep approach is _____feet a minute.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.11




    A. 800
  127. 127(142). The maximum touchdown speed for a practice roll-on landing is _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.12




    B. 60 KGS
  128. 128(143). When reducing torque available on the simulated failed engine, initiation of practice single-engine
    emergencies will not be lower than _____ feet AGL, _____ KIAS.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.13




    B. 300 / 80
  129. 129(144). Practice single-engine emergencies may be initiated below 300 feet AGL and 80 KIAS so long as torque available is
    limited on both engines versus reducing torque available on the simulated failed engine by actual throttle manipulation.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.13

    A. True
    B. False
    A. True
  130. 130(145). The following simulated single-engine maneuvers will be practiced by simulating a limited torque available on both
    engines versus reducing torque by actual throttle manipulation _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.13.1




    C. A and B
  131. 131(147). Practice autorotations will terminate and a power recovery will be initiated at the first indications of ______.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.18.1




    D. all of the above
  132. 132(155). For restricted visibility approaches, when the anticipated power margin is _____or less, a second
    aircrew member will reconfirm power computations using flight manual performance charts or the CDU Calculator Page.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.15.5




    C. 10%
  133. 133(156). For restricted visibility approaches training, power available must be equal to or greater than _________.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.15.4.1




    C. OGE hover power + 5%
  134. 134(157). For water operations training, power available must be equal to or greater than _______________.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.15.3.1




    A. OGE hover power + 5%
  135. 135(158). When landing to a surface area smaller than your rotor diameter, such as a pinnacle or ridgeline, power for ____ hover must be available.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.15.2.3




    A. an OGE
  136. 136(159). Do not initiate fuel dumping except for life and death rescue missions, operational missions, MAJCOM exercises and emergencies.
    Except during emergencies, or operational deeds dictate due to inability to climb due to threats or weather, fuel will not be dumped
    below 3,000 feet AGL or over agricultural/populated areas.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.14

    A. True
    B. False
    A. True
  137. 137(160). Do not taxi another aircraft within ___ feet of a refueling operation.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.12




    C. 50
  138. 138(161). Aircraft may be flown with one strobe light inoperative.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.7.1
    A. True
    B. False
    A. True
  139. 139(162).____ approval is required to remove the FE and AG seats. _____ may delegate this authority no lower than ____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.20.2




    C. OG/CC, OG/CC, SQ/CC
  140. 140(164). Conduct all operations at or above ____ above ground level (AGL) except when lower altitudes are required for takeoff, departure, arrival, landing, operational missions, training flights in approved areas or routes, or approved exercise missions.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.10




    D. 500 feet
  141. 141(165). For all flights, VFR or IFR, plan to arrive at destination with a ____-pound usable fuel reserve.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.5.3




    C. 500
  142. 142(166). Prior to each flight the aircraft commander will ensure all passengers are briefed IAW TO 1H- 60(H)G-1CL-1 and applicable MAJCOM guidance.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 3.2.3

    A. True
    B. False
    A. True
  143. 143(51). Aircraft energy is the combination of airspeed (kinetic energy) and altitude (potential energy) at any time during flight.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-1 Chap: 14 Para: 14.3.1

    A. True
    B. False
    A. True
  144. 144(52). Engine performance is affected by pressure altitude (PA) and outside air temperature, with ____ generally having the largest impact on power available.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-1 Chap: 14 Para: 14.3.2




    A. temperature
  145. 145(53). The lowest point of the total power required curve indicates the airspeed that normally determines the aircraft's
    level flight speed for VY, VBE, and minimum rate-of-descent speed for autorotation is referred to as the ____ speed.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-5 Chap: 14 Para: 14.3.4.4




    B. bucket
  146. 146(54). As gross weights and DA increase, the single-engine airspeed range _____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-5 Chap: 14 Para: 14.3.4.5



    A. narrows
  147. 147(55). For an HH-60G in a stabilized hover in a no-wind environment, the application of right pedal for a moderate-rate
    pedal turn will result in an approximate ____ change in torque.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-7 Chap: 14 Para: 14.3.6




    B. 5 % decrease
  148. 148(56). When hovering with a crosswind, the application of pedal to hold heading will result in power (required to hover)
    readings that will not match those estimated for a no-wind environment.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-10 Chap: 14 Para: 14.3.7

    A. True
    B. False
    A. True
  149. 149(57). As main rotor and tail rotor thrust are both increased to cushion the landing, the helicopter may exhibit a right
    lateral drift. This phenomenon is most noticeable just prior to touchdown during an approach to the ground and is known as .
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-11 Chap: 14 Para: 14.4.1




    A. translating tendency
  150. 150(58). If a loss of tail rotor effectiveness occurs, consider counteracting by _____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 14-11 Chap: 14 Para: 14.3.7.2.1




    D. all of the above
  151. 151(59). Excessive cyclic input and insufficient collective application may result in inadequate taxi speed and droop-stop pounding.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-3 Chap: 9 Para: 9.2.1.1.4

    A. True
    B. False
    A. True
  152. 152(60). Hover references off the nose of the helicopter (or using the probe on the pilot side) will help in detecting heading and
    sideward drift. If only one reference is available, attempt to position it at a ____ degree angle to the side.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-4 Chap: 9 Para: 9.2.2.1




    D. 45
  153. 153(61). The normal takeoff may be made from the ground or a hover. Target torque value for the normal takeoff is ____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-7 Chap: 9 Para: 9.3.1.1.1




    D. hover power +10 percent
  154. 154(62). Using more than ____degrees nose low when in close proximity to the ground can lead to difficulty during a single-engine or
    uncommanded stabilator movement emergency or result in inadvertent probe-to-ground contact.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-8 Chap: 9 Para: NOTE




    A. 10
  155. 155(63). For practice and simulated maximum performance takeoffs, use a target torque value of ____ or as specified by the IP/EP and a 100-foot vertical obstacle.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-8 Chap: 9 Para: 9.3.1.2.1




    B. OGE hover power + 5%
  156. 156(64). Maximum performance takeoff: As the aircraft clears the obstacle, adjust cyclic to obtain an accelerative attitude
    (e.g., approximately 5 to 10 degrees nose low) and allow the aircraft to crab into the wind while maintaining desired ground track.
    Once the aircraft is clear of the obstacle and above safe single-engine airspeed, or _____ if safe single-engine airspeed is not available,
    continue with normal takeoff procedures.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-9 Chap: 9 Para: 9.3.1.2.3




    B. 70-80 KIAS
  157. 157(65). The marginal power takeoff is made from the ground or a stabilized 10-foot hover. For practice or simulated marginal power
    takeoffs, use a target torque value of ____ and a 50-foot vertical obstacle.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-10 Chap: 9 Para: 9.3.1.3.1




    B. 10 ft hvr pwr
  158. 158(66). The ____ is used when power available is limited (e.g., high gross weights/high DA) and will not allow for the use of other types of takeoffs.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-11 Chap: 9 Para: 9.3.1.4.1




    D. rolling take-off
  159. 159(67). For practice rolling takeoffs, use a simulated maximum power available value of ____. For rolling takeoffs when power is actually limited,
    apply torque as necessary, up to maximum available power (without droop).
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-11 Chap: 9 Para: 9.3.1.4.1




    D. 10 percent less than 10-foot hover power
  160. 160(68). To begin a rolling take-off, place the cyclic forward of neutral so that the tip-path plane is slightly above the horizon. Increase the collective and release the brakes.
    Apply approximately ___ percent torque to accelerate the aircraft.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-11 Chap: 9 Para: 9.3.1.4.3




    A. 30 to 40
  161. 161(69). The normal approach uses a _____ degree apparent angle and is initiated at ____ KIAS and 300 feet AGL. The normal approach may terminate on the ground or in a hover.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-13 Chap: 9 Para: 9.4.3.1




    D. 30, 80
  162. 162(70). The steep approach is used when obstacles or terrain will not allow the use of other types of approaches. The steep approach uses a 45-degree apparent angle,
    is initiated at _____ and _____, and may terminate on the ground or in a hover.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-14 Chap: 9 Para: 9.4.4.1




    D. 50 KGS, 300 AGL
  163. 163(71). The shallow approach uses a 10-degree apparent angle and is initiated at 80 KIAS and 300 feet AGL. The shallow approach may terminate on the ground or in a hover.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-16 Chap: 9 Para: 9.4.5.1

    A. True
    B. False
    A. True
  164. 164(72). Aerodynamic braking is normally used when wheel-braking action may be inadequate due to the landing surface's size or surface or there is a concern that the
    aircraft's brakes may overheat. By using the aerodynamic forces of the main rotor system, the aircraft can be stopped or slowed down significantly in a relatively short distance.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-18 Chap: 9 Para: 9.4.6.1

    A. True
    B. False
    A. True
  165. 165(73). When executing a rolling landing, maintain airspeed ____ or above minimum safe single-engine airspeed, until the landing area can be reached in the
    event of a loss of power.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-19 Chap: 9 Para: 9.4.6.3




    D. between 60 to 80 KIAS
  166. 166(74). During a Boost/SAS malfunction, a well-executed ____ approach requires little maneuvering to terminate. Whatever approach angle is selected,
    ensure slow, smooth collective inputs at termination.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-22 Chap: 9 Para: 9.5 NOTE



    B. Steep
  167. 167(75). During a stabilator malfunction, in order to provide a normal deceleration, sight picture, and landing attitude, the stabilator is slewed full down below ____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-24 Chap: 9 Para: 9.5.3.3.5.1




    A. 40 KIAS
  168. 168(76). With the Stab set at zero degrees, the aircraft will take more time and distance to decelerate. The nose of the aircraft will pitch up several degrees higher than normal during the deceleration (particularly on short final), perhaps making forward visibility difficult.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-25 Chap: 9 Para: 9.5.3.3.5.2

    A. True
    B. False
    A. True
  169. 169(77). When a throttle is dragged to simulate a single-engine failure, consider dragging the throttle on the ____ engine in the event of inadvertent shutdown.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-26 Chap: 9 Para: 9.5.4 NOTE




    C. weaker (e.g., lower engine torque factor [ETF])
  170. 170(78). During practice emergency DEC operations, the PNF pulls the throttle downward out of the FLY detent and smartly/swiftly advances it full forward to LOCKOUT,
    then smartly/swiftly reduces it to _____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-26 Chap: 9 Para: 9.5.5.2.1




    A. an intermediate position between IDLE and FLY (the six o'clock position is recommended)
  171. 171(79). For autorotations, any crewmember noting an out of parameter condition or adverse trend should announce the condition/trend and/or direct a ____, as necessary.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-29 Chap: 9 Para: 9.5.6 NOTE




    A. go around
  172. 172(80). Some actual autorotations might require a near-zero ground speed, such as landing in/on ____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-30 Chap: 9 Para: 9.5.6.4.4




    D. all of the above
  173. 173(81). Allowing the aircraft attitude to pitch up during initiation of practice autorotations can result in ______.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-31 Chap: 9 Para: 9.5.6.5




    A. loss of airspeed throughout the maneuver
  174. 174(82). During performance of practice autorotations, initiating the wake-up while leveling the aircraft may not allow sufficient time for the engines to respond and may result in rotor droop and/or inadvertent landing.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 9-32 Chap: 9 Para: 9.5.6 CAUTION

    A. True
    B. False
    A. True
  175. 175(83). During brownout/whiteout operations and _____ wind conditions, extreme caution must be exercised due to the potential of near-zero visibility conditions.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-19 Chap: 10 Para: 10.21




    D. both A and B
  176. 176(84). Flying the high recon at approximately _____ should provide a reasonable compromise between providing a familiar sight picture and margin above hazards/obstacles, while being low enough to provide good viewing/analysis of the landing area.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-26 Chap: 10 Para: 10.26.2.1




    A. 300 feet above site elevation
  177. 177(85). Light and variable wind conditions could result in a tailwind component on final approach, significantly increasing power requirements.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-3 Chap: 10 Para: 10.5.2

    A. True
    B. False
    A. True
  178. 178(86). High DA, clear skies, and vegetation can cause a bubble effect on mountaintops that can result in surface temperatures of ____
    degrees warmer than the same elevation outside the bubble.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-4 Chap: 10 Para: 10.6.1.2




    A. several
  179. 179(87). A common problem associated with steep approaches over barriers is that translational lift may be lost when the helicopter is possibly ____ AGL.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-9 Chap: 10 Para: 10.9.1.3




    B. 100-200 feet
  180. 180(88). Use of IR lighting in brownout or whiteout conditions can seriously degrade visibility. When these conditions are anticipated, IR lighting, if used, should be _____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 8-1 Chap: 8 Para: 8.2 CAUTION




    C. dimmed to the lowest level necessary to safely accomplish the landing
  181. 181(89). During formulation of approach plans during remote area reconnaissance, a normal approach may prove advantageous because it provides a familiar _____.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-9 Chap: 10 Para: 10.9.1.1




    D. all of the above
  182. 182(90). The _____ is a proactive, pre-emptive action taken when external conditions warn of a deteriorating condition.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-10 Chap: 10 Para: 10.9.3




    A. go-around
  183. 183(91). The ____ is a reactive maneuver performed because of malfunction or because the PF failed to notice a deteriorating condition.
    Ref: AFTTP 3-3.HH-60G (28 Oct 2011) Pg: 10-10 Chap: 10 Para: 10.9.3




    B. escape
  184. 184(168). Failure to wait the full ____ minutes for APU cool down may result in the APU failing to start.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-15 NOTE Chap: 1




    C. 30
  185. 185(20). If the APU does not start, you should wait _____ before attempting a restart.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-13 Chap: 2 Para: CAUTION




    A. 2 minutes
  186. 186(21). Monitor main fuel quantity during probe extension and retraction to ensure no more than the normal _____ pound changes occur in total main fuel quantity.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-21 Chap: 2 Para: CAUTION




    D. 20 to 30
  187. 187(22). Due to the danger to personnel of electromagnetic fields radiating from the SATCOM antenna, no personnel should be on top of the aircraft when transmitting.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-22 Chap: 2 Para: WARNING

    A. True
    B. False
    A. True
  188. 188(25). With the BACKUP HYDRAULIC PUMP as the sole source of hydraulic pressure for either the #1 or
    #2 TAIL SERVO, do not ____ during shutdown.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-45 Chap: 2 Para: WARNING




    C. move the BACKUP HYD PUMP switch from AUTO
  189. 189(13). If the stabilator is slewed up using battery power, _____ to get a normal engagement of the automatic mode.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 1-80 Chap: 1




    C. it must be manually slewed back down
  190. 190(23). During the Engine HIT check, if TRQ is greater than 5% at 92% to 98% Nf, a torque stiction malfunction is possible _____.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-29 Chap: 2 Para: WARNING



    C. do not fly the aircraft
  191. 191(24). Do not place the MODE SEL switch to AUTO prior to moving the MAN AUX FLOW switches to NO FLOW.
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 2-31 Chap: 2 Para: CAUTION

    A. True
    B. False
    A. True
  192. 192(152). Recommended hoist altitude over water or vessels is the minimum altitude necessary to avoid salt spray and/or shipboard obstacles.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.2.3

    A. True
    B. False
    A. True
  193. 193(95). Designate an alternate, for the first point of intended landing if the worst weather is forecast to be less than _____.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.7.1.2




    D. B and C, whichever is higher
  194. 194(96). Which of the following is an authorized method of departing IFR?
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.12.3




    D. all of the above
  195. 195(101). Helicopters may fly in fixed-wing rectangular pattern if they maintain a compatible airspeed with the fixed-wing traffic.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 5.11.8.4

    A. True
    B. False
    A. True
  196. 196(103). On a diverse departure, track runway centerline to _____before turning on course.
    Ref: AFI 11-202, Vol 3, General Flight Rules Para: 8.12.7




    C. 400 feet above the departure end of the runway
  197. 197(136). Simulated hoist and gun emergencies may be performed at night with _____.
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.2



    A. concurrence of the aircraft commander
  198. 198(146). Boost/SAS-Off maneuvers can be initiated .
    Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 4.20.3.15




    C. on the ground, in straight and level flight with a minimum of 300 feet AGL and 80 KIAS
  199. 199(167). When performing hover operations with light and variable winds at high gross weight and/or in a high density altitude environment, _____ the power required computations
    Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 7-5 WARNING Chap: 7




    B. add a margin to
  200. 200(178). For EMCON 2 - 4 Aided HAAR, receivers will FLASH formation/position lights _____ seconds prior to movement for disconnect.
    Ref: ATP-56(B) Pg: 4-2 Chap: Part 3 Para: 403 c. (3)




    D. 5
Author
hvr4fun
ID
297819
Card Set
HH-60G Plt QUAL MQF 2015_Cards.txt
Description
Pilot MQF ACC, 301st Rescue Squadron 2015
Updated