Hh-60 Pilot Mqf 51-105

Front 1

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

Back 1

A. True

Front 2

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
A. reducing fuel flow
B. shutting off all fuel flow followed by an automatic restart.
C. shutting off all fuel flow with no possible restart until maintenance corrective action
D. through TGT limiting

Back 2

C. shutting off all fuel flow with no possible restart until maintenance corrective action

Front 3

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
A. Engine Overspeed Protection System, Ng
B. Engine Overspeed Protection System, TGT
C. Automatic TGT Limiting System, TGT
D. Automatic TGT Limiting System, Ng

Back 3

C. Automatic TGT Limiting System, TGT

Front 4

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

Back 4

A. True

Front 5

Flight Controls
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
A. left lateral cyclic input
B. right lateral cyclic input
C. increased tail rotor pitch
D. both A and C

Back 5

D. both A and C

Front 6

Fuel
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
A. 45%
B. 48%
C. 55%
D. 58%

Back 6

D. 58%

Front 7

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
A. 0° C
B. 0° F
C. 4°C
D. 4° F

Back 7

A. 0° C

Front 8

General
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
A. searchlight
B. tail position light
C. position lights
D. FLIR

Back 8

A. searchlight

Front 9

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
A. SQ/CC
B. WG/CC
C. MAJCOM/A3 (NGB: NGB/A3)
D. ACC/A3T (NGB: NGB/A3T)

Back 9

C. MAJCOM/A3 (NGB: NGB/A3)

Front 10

60(118). The Aircraft Commander is responsible for all of the following except_________.
Ref: AFI 11-2HH60V3 05 Jan 2011 Para: 2.1
A. Approving deviations from AFI 11-2HH-60V3 during routine mission accomplishment.
B. Ensuring aircraft security when away from home station.
C. Responsible for the welfare of the crew and the safe accomplishment of the mission.
D. The final authority for asking for and accepting waivers affecting the crew or mission.

Back 10

A. Approving deviations from AFI 11-2HH-60V3 during routine mission accomplishment.

Front 11

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

Back 11

A. True

Front 12

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
A. SQ/CC
B. OG/CC
C. Wing/CC
D. MAJCOM/DO

Back 12

B. OG/CC

Front 13

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
B. wait for the system to automatically turn back on
C. turn the PITOT HEAT switch OFF
D. both A and C

Back 13

A. WINDSHIELD ANTI-ICE PILOT, CTR, and COPILOT switches must be placed OFF and then ON

Front 14

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
A. 300, 300
B. 400, 300
C. 400, 250
D. 400, 400

Back 14

C. 400, 250

Front 15

65(97). A PIC may deviate from any flight rule only when ________.
Ref: AFI 11-202, Vol 3, General Flight Rules Para: 1.7
A. an in-flight emergency requires immediate action
B. deviation is required to protect lives
C. when safety of flight dictates
D. all of the above

Back 15

D. all of the above

Front 16

66(98). The following are approved types of flight logs _______.
Ref: AFI 11-202, Vol 3, General Flight Rules Para: 2.5
A. AF Form 70
B. navigator's flight log
C. lead command approved computer-generated flight log
D. all of the above

Back 16

D. all of the above

Front 17

General Operating Procedures
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
A. right
B. left
C. the slower (more maneuverable) aircraft has the right of way
D. the faster (less maneuverable) aircraft has the right of way

Back 17

A. right

Front 18

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
A. to the destination
B. until obtaining an IFR clearance
C. to a suitable landing location
D. all of the above

Back 18

D. all of the above

Front 19

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
A. day ½ SM clear of clouds
B. night 1 SM clear of clouds
C. both A and B
D. none of the above

Back 19

C. both A and B

Front 20

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
A. SQ/CC
B. SQ/DO
C. Aircraft Commander
D. Cabin NCOIC

Back 20

C. Aircraft Commander

Front 21

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
A. 0; -5
B. 10; 4
C. 13; 0
D. 21; 10

Back 21

B. 10; 4

Front 22

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
A. immediately shut down the engine
B. run engine at idle until pressure is within limits
C. make an AF Form 781 write-up
D. both A and C

Back 22

B. run engine at idle until pressure is within limits

Front 23

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
A. slightly advance the throttle, if engine oil pressure caution light extinguishes, oil pressure is acceptable
B. rapidly advance the throttle to fly, if engine oil pressure caution light extinguishes, oil pressure is acceptable
C. no action required, it is acceptable to fly with the engine oil pressure caution light illuminated
D. immediately move the throttle to the OFF position

Back 23

A. slightly advance the throttle, if engine oil pressure caution light extinguishes, oil pressure is acceptable

Front 24

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. 3 to 4
B. 5 to 10
C. 8 to 12
D. 15 to 20

Back 24

C. 8 to 12

Front 25

Hyd
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
A. #1 TAIL ROTOR SERVO, BOOST SERVO OFF, SAS OFF
B. #1 and #2 RSVR LOW, #2 TAIL ROTOR SERVO ON, BACKUP PUMP ON
C. BACKUP RSVR LOW
D. all of the above

Back 25

C. BACKUP RSVR LOW

Front 26

Instrument
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

Back 26

A. True

Front 27

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
B. 250 ft/NM
C. 300 ft/NM
D. none of the above

Back 27

A. 200 ft/NM

Front 28

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.
B. a ceiling 400 ft above, and a visibility of at least 1 SM above, the lowest compatible published landing minimum.
C. 700/1
D. A or C, whichever is higher

Back 28

A. a ceiling 200 ft. above, and a visibility of at least 1 SM above, the lowest compatible published landing minimum.

Front 29

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. 30 minutes
B. 45 minutes
C. 50 minutes
D. 1 hour

Back 29

D. 1 hour

Front 30

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
A. thunderstorm
B. rain/snow shower
C. both A and B
D. none of the above

Back 30

C. both A and B

Front 31

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
A. an IMC departure under IFR is not authorized
B. helicopters may take off using max climb and charted obstacle avoidance
C. an IFR departure to VMC conditions is authorized
D. radar vectors at MEA are required

Back 31

A. an IMC departure under IFR is not authorized

Front 32

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
A. in VMC conditions only
B. when an IP/EP is at a set of controls
C. both A and B
D. never

Back 32

D. never

Front 33

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"
B. "100 feet above DH"
C. "Land" at DH if the runway environment is in sight and the aircraft is in a position for a normal landing
D. "Go-around" at DH if the runway environment is not in sight or if the aircraft is not in a position for a normal landing.

Back 33

A. "500 feet above DH"

Front 34

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. 5, 10, 100
B. 5, 20, 100
C. 10, 10, 100
D. 10, 20, 100

Back 34

C. 10, 10, 100

Front 35

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
A. 0+/-5; 0 to +3
B. 0 to +3; 0+/-5
C. 0+/-3; 0 to +3
D. 0 to +5; 0+/-5

Back 35

A. 0+/-5; 0 to +3

Front 36

91(99). Flights conducted in IMC require ________.
Ref: AFI 11-202, Vol 3, General Flight Rules Para: 2.15.2
A. operative pitot heat
B. operational anti-icing and/or deicing equipment
C. A and B
D. none of the above

Back 36

C. A and B

Front 37

Landing Gear
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. the transponder is turned to STBY for 15 seconds before removing power
B. the Mode 4 power switch is left in the ON position while AC power is removed
C. no action required, the Mode 4 codes are only erased by the ZERO function
D. specifically held with the HOLD function

Back 37

D. specifically held with the HOLD function

Front 38

Limits
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. 34, 30, 45
B. 20, 25, 30
C. 45, 50, 55
D. 43, 30, 51

Back 38

D. 43, 30, 51

Front 39

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
A. 110; 120
B. 95; 101
C. 100; 107
D. 100; 110

Back 39

A. 110; 120

Front 40

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
A. 25
B. 35
C. 45
D. 55

Back 40

C. 45

Front 41

96(38). Avoid operation in the ______________ Nf ranges.
Ref: 1H-60(H)G-1 Chng 7 01 Jun 2011 Pg: 5-2 Chap: 5
A. 0%-50% and 80%-90%
B. 20%-40% and 60%-90%
C. 30%-50% and 70%-80%
D. 35%-45% and 65%-85%

Back 41

B. 20%-40% and 60%-90%

Front 42

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
A. 20 to 40; 180
B. 20 to 40; 50
C. 30 to 50; 180
D. 30 to 50; 50

Back 42

C. 30 to 50; 180

Front 43

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
A. 100
B. 120
C. 130
D. 145

Back 43

C. 130

Front 44

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
A. 25 KIAS
B. 45 KIAS
C. 85 KIAS
D. 105 KIAS

Back 44

B. 45 KIAS

Front 45

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
B. 120 KIAS
C. 130 KIAS
D. 145 KIAS

Back 45

A. 100 KIAS

Front 46

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
A. 100 KIAS
B. 120 KIAS
C. 130 KIAS
D. 145 KIAS

Back 46

D. 145 KIAS

Front 47

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

Back 47

A. True

Front 48

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. 15 deg C
B. 21 deg C
C. 33 deg C
D. 43 deg C

Back 48

B. 21 deg C

Front 49

MISSION PLANNING/FLIGHT PREPARATION
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) / 1000/2 (Night Unaided)
B. 700/1 (Day) / 700/2,(NVG) / 1000/3 (Night Unaided)
C. 700/1 (Day and NVG) / 1000/2 (Night Unaided)
D. 700/1 (Day) / 700/2 (NVG) / 1500/3 (Night Unaided)

Back 49

B. 700/1 (Day) / 700/2,(NVG) / 1000/3 (Night Unaided)

Front 50

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
B. published approach minimums (ceiling and visibility), but no less than 1/4 mile (RVR 1200) at the departure airfield.
C. equal to or higher than published approach visibility minimums at the destination
D. equal to or higher than published ceiling and visibility minimums at the destination

Back 50

A. published approach minimums (ceiling and visibility), but no less then 1/2 mile (RVR 2400) at the departure airfield