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Archive > EP 14March2016 > Flashcards

EP 14March2016 Flashcards

1
Q

What is the over consideration during any emergency?

A
  1. Maintain Aircraft Control
  2. Analyze the Situation
  3. Take Appropriate Action

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2
Q

What does the term “LAND/DITCH IMMEDIATELY” mean?

A

Execute the landing or ditching without delay due to the seriousness of the malfunction

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3
Q

What is the primary consideration during a “LAND/DITCH IMMEDIATELY”?

A

Survival of the occupants of the aircraft

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4
Q

During a “LAND/DITCH IMMEDIATELY” what is not a consideration?

A

Loss of the airframe

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5
Q

What does the term “LAND AS SOON AS POSSIBLE” mean?

A

Executing a landing at the first site at which a safe landing can be made

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6
Q

What does “LAND AS SOON AS PRACTICABLE” mean?

A

Extended flight is not recommended but landing site and duration of flight is at the discretion of the PIC

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7
Q

What does the term “ABORT MISSION” mean?

A

Aircraft shall not proceed on its assigned mission and should return to its desired recovery base

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8
Q

Can the crew continue on a mission after an EP that ends with “ABORT MISSION”?

A

Yes as long as the gain clearly outweighs the risk for a short additional duration

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9
Q

What does the term “CONTINUE FLIGHT AS APPROPRIATE” mean?

A

PIC should consider mission urgency and the impact of the malfunction on safe aircraft operation when determining whether to proceed on the assigned mission

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10
Q

What does the circuit breaker term “CHECK” mean?

A

Note the status of the affected circuit breaker

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11
Q

What does the circuit breaker term “CHECK/RESET” mean?

A

Ensure that affected circuit breaker is in

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12
Q

How many times can you reset a Circuit Breaker?

A

Once

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13
Q

What does the circuit breaker term “CYCLE” mean?

A

Pull affected circuit breaker, wait 15 seconds, and reset affected circuit breaker

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14
Q

What does the circuit breaker term “PULL” mean?

A

Manually open affected circuit breaker

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15
Q

What EP as two or more of the following:

  1. Complete loss of MGB lubrication
  2. Yaw kicks, abnormal MGB noises, or unusually high power requirements
  3. MGB CHIP on the VEMD CAUTION/FUEL page?
A

MGB Failure imminent

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16
Q

What is the EP for MGB Failure Imminent?

A
  1. 200-foot Checklist-complete
  2. Land/Ditch Immediately

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17
Q

How long can you fly without MGB oil?

A

Approximately 25 minutes

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18
Q

What is the airspeed required for MGB Overheat?

A

120 KIAS minimum

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19
Q

What EP symptom is:

  1. MGB FIRE warning light illuminated and possible symptoms of
  2. Illumination of MGB related warning caution light
  3. Loss of XMSN OIL pressure and/or rise in temperature
  4. Drop in fuel or hydraulic pressure
  5. Electrical system malfunctions?
A

MGB fire

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20
Q

What is the corrective action for MGB Fire?

A
  1. Attempt to confirm presence of fire (alert crew)
  2. 200-foot checklist-Complete
    If fire confirmed:
  3. Land/Ditch immediately
    If fire NOT confirmed:
  4. Land as soon as possible

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21
Q

What inflight EP symptoms are:

  1. Engine “FIRE” warning light illuminated
  2. Red warning light illuminated on the corresponding EFSL
  3. Flames and/or smoke coming from engine compartment
  4. Electrical system system malfuctions?
A

Engine compartment fire inflight

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22
Q

What is the corrective action for engine compartment fire inflight?

A
  1. Attempt to confirm presence of fire (alert crew)
  2. Single-Engine flight profile-establish
    If fire confirmed:
  3. FCS (affected engine)-Confirm; IDLE, Confirm; off
  4. EFSL (affected engine)-Confirm; Off
  5. Boost pumps (affected engine)-off
  6. Pri Fire extinguisher button (affected engine)-Confirm; Push
    7.Sec fire extinguisher button (affected engine)- push
  7. 200-foot checklist-complete
    If fire still persists:
    Land/Ditch immediately
    If fire no longer evident:
    Land as soon as possible
    If fire not confirmed:
  8. Land as soon as practicable

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23
Q

What EP on-deck has symptoms of:

  1. Engine FIRE warning light illuminate
  2. Possible hand or voice signals form ground crew
  3. Red warning light illuminated on the corresponding EFSL?
A

Engine compartment fire on deck

1H-65D-1
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24
Q

What is the corrective action for engine compartment fire on deck?

A
  1. Attempt to confirm presence of fire (alert crew)
  2. FCSs-both off
  3. EFSLs-both off
  4. Boost pumps-all off
    If fire confirmed:
  5. Pri fire extinguished button (affected engine)-confirm; push
  6. Sec Fire extinguisher button (affected engine)Push
    7.Emergency electrical cutoff-off
  7. Rotor brake-on
    9.Evacuate aircraft

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25
Q

What EP has symptoms of:

  1. Smoke/fumes/sparks originating from a single component inside the cabin
  2. Smoke/fumes/sparks originating from an unknown component inside the cabin?
A

Internal fire (cabin, Electrical, and/or avionics)

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26
Q

What is the corrective action for an Internal fire (cabin, electrical, and/or avionics)?

A
  1. Designate crew member to fight fire
  2. Affected equipment-off
  3. Circuit breakers-pull (for affected circuits)
  4. Rack blower circuit breaker-pull
  5. Heat/cool switches-off
  6. Ram air, doors, and CP window-closed
  7. 200-foot check list complete
    If electrical or avionics fire persists:
  8. Emergency electrical cutoff-off
    If electrical or avionics fire persists:
  9. Land/Ditch immediately
    If first goes out:
    10: Land as soon as possible

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27
Q

What is the corrective action for “Smoke and fume elimination”?

A
  1. Heat/cool switches-off
  2. Ram air, cabin sliding door, and CP window-open
  3. Land as soon as practicable

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28
Q

What is the best radio to use if there is fuel fumes in the cabin?

A

COMM 1

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29
Q

What EP symptoms are:

  1. TOT rises rapidly after FCS has been placed in the OFF position
  2. TOT does not decrease within 10 seconds after FCS has been placed in the OFF position?
A

Engine post-shutdown fire

1H-65D-1
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30
Q

How long does it take for the FADEC to shut down the engine with the solenoid valve fails?

A

5 to 6 seconds

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31
Q

What is the corrective action for engine post-shutdown fire?

A
  1. FADEC control switch-check off
  2. Boost pumps-check off
  3. EFSL (affected engine)-off
    If High TOT still evident after 10 seconds:
  4. Crank button-depress until TOT decreases
    IF TOT continues to rise or does not decease:
  5. Emergency electrical cutoff-off
  6. Rotor brake-on
  7. Evacuate aircraft

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32
Q

When planning an approach and landing with a medium or high frequency vibrations or abnormal noise from the tail section what should be considered?

A

A possible loss of tail rotor thrust

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33
Q

What EP symptoms are:

  1. Known or suspected aircraft damage
  2. Abnormal vibrations?
A

Known or suspected damage/abnormal vibrations

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34
Q

What is the best speed to reduce vibration and improve flight characteristics?

A

75-100 KIAS

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35
Q

What is corrective actions for known or suspected aircraft damage/abnormal vibrations?

A
  1. 200-foot checklist-complete
    If severe vibrations and/or drastically altered flight characteristics:
  2. Land/ditch immediately
    If moderate vibrations:
  3. Land as soon as possible
    If slight vibrations or unknown origin or suspected:
  4. Land as soon as practicable

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36
Q

For loss of tail rotor thrust what speed is need so that the lateral and vertical fin can maintain balance flight?

A

120-125 KIAS

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37
Q

When are the 4 times that 30-sec OEI automatically selected by the FADEC?

A

Major FADEC failure
BACKUP mode selected on one engine
N1 difference between the two engines is >6%
There is an engine failure

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38
Q

When is 2 minute OEI LO automatically selected by FADEC?

A

TRNG switch is in IDLE, and either engine is degraded

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39
Q

What is the airspeed for minimum power required?

A

70-75 KIAS

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40
Q

What is the term for the basic procedures that should be followed in the event of any suspected engine malfunction?

A

THE BIG 4

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41
Q

What is THE BIG 4?

A
  1. NR
  2. Airspeed/Altitude
  3. Wheels/Floats
  4. Analyze

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42
Q

What EP has symptoms:

  1. “ENG # CHIP” warning light illuminated
  2. ENGINE CHIP annunciation on the VEMD CAUTION/FUEL page?
A

Engine Chip Detected

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43
Q

What is the corrective action for Engine Chip Detected?

A
  1. Complete THE BIG 4
  2. FCS (affected engine)Confirm; idle
    If abnormal idle indications:
  3. FCS (affected engine)-confirm; off

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44
Q

During an engine chip EP what can be done on landing if more power is need?

A

Affected engine can be brought back to flight

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45
Q

What EP symptoms:

  1. “DIF Na” warning light illuminated
  2. DIF Na aural warning
  3. Possible NR droop
  4. Low NR horn
  5. OEI GOV Mode on VEMD
  6. N1 difference between engines is great than 6%
A

N1 divergence/partial power loss

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46
Q

What is the corrective action for N1 Divergence/partial power loss?

A
  1. Complete THE BIG 4

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47
Q

When will CHECK TRQ appear on the VEMD?

A

When the torque differential between the engines is greater then 7.5%

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48
Q

What EP has symptoms of:

  1. “FADEC # FAIL” caution light illuminated
  2. Engine status light
  3. OEI GOV Mode page displayed
  4. Affected engine will not respond to collective movement du to fuel flow metering being frozen at the at the rate present when the FADEC failed?
A

Major FADEC/Governor failure (LEVEL 3)

1H-65D-1
Page 3-35

49
Q

What is the corrective action for Major FADEC/Governor Failure (LEVEL 3)?

A
  1. Complete THE BIG 4
  2. TRNG switch-FLT
  3. FADEC backup switch (affected engine)confirm; backup

1H-65D-1
Page 3-35

50
Q

Why should the collective not be reduced before the FADEC backup switch is selected?

A

Could result in an over speed condition

1H-65D-1
Page 3-35

51
Q

When can the FADEC backup switch not be used?

A

When an engine is at TRNG IDLE

1H-65D-1
Page 3-35

52
Q

When will the automatically cancel Training Mode?

A

In the event of a Level 2 or Level 3 FADEC failure

1H-65D-1
Page 3-35

53
Q 
What EP has the symptoms:
1."GOV" caution light illuminated
Possible Symptoms:
2."FLI DEGR" annunciation of he VEMD
3. TRQ, TOT, or N1 value missing with TRQ, TOT, or N1 label in boldface yellow type
4. One or bothVEMD screens off or failed
5. NO BING annunciation on ÇDU
6. LAANE 1/2 FAILED> PRESS OFF 1/2
7. CROSS TALK FAILED>PRESS OFF 1/2
8. STAT page FAIL line: BARO?
A

Minor FADEC/Governor failure (LEVEL 2)

1H-65D-1
Page 3-36

54
Q

What is the corrective actin for Minor FADEC/Governor Failure (level 2)

A
  1. Complete THE BIG 4

1H-65D-1
Page 3-36

55
Q

What is the cruise airspeed for an engine over heat?

A

120 KIAS Minimum

1H-65D-1
Page 3-37

56
Q

Before doing an inflight engine restart how long should you wait with FCS in the off position?

A

30 sec

1H-65D-1
Page 3-38

57
Q

What is the corrective action for EMERGENCY SHUTDOWN PROCEDURE ONDECK?

A
  1. EFSL-both off
  2. ELECTRICAL CUTOFF-off
  3. Rotor brake-on
  4. Evacuate Aircraft

1H-65D-1
Page 3-39

58
Q

When should the pilot shut down the engine during a start?

A

TOT 750 degrees C

1H-65D-1
Page 3-39

59
Q

When will the FADEC automicatilly shut down the engine during the start?

A

TOT 840 degrees C

1H-65D-1
Page 3-39

60
Q

What is the target Airspeed for an autorotation?

A

75-105

1H-65D-1
Page 3-42

61
Q

Doing an autorotation closer to 75 KIAS give you what kind of aircraft performance?

A

Max endurance

1H-65D-1
Page 3-42

62
Q

Doing an autorotation at 105 KIAS will give the aircraft what kind of performance?

A

Max range

1H-65D-1
Page 3-42

63
Q

What EP has the possible symptoms of:

  1. “BATT TEMP” warning light illuminated
  2. Smoke and/or fumes from radome or vent
  3. Noise from radome
A

Battery over temperature/thermal runaway

1H-65D-1
Page 3-52

64
Q

What are the corrective actions for Battery over temperature/thermal runaway

A
  1. Batt relay switches-both off
  2. Land as soon as practicable

1H-65D-1
Page 3-52

65
Q

Will securing the BAT RELAY switches stop or reverse a battery over-temperature/thermal runaway?

A

No

1H-65D-1
Page 3-52

66
Q

Can the T/R power the DC bus with the battery switches secured?

A

No

1H-65D-1
Page 3-53

67
Q

Why should CO2 never be used in the battery compartment to effect cooling of displace the explosive gases?

A

Static electricity generated by CO2 can ignite the hydrogen/oxygen gases

1H-65D-1
Page 3-53

68
Q

How many times can you reset a boost pump circuit breaker?

A

0

1H-65D-1
Page 3-56

69
Q

Above what must all boost pumps be on?

A

8,000ft MSL

1H-65D-1
Page 3-56

70
Q

How long should you wait before hovering or landing after jettisoning fuel?

A

1 minute

1H-65D-1
Page 3-59

71
Q

How long should you be in a normal straight and level attitude and a constant airspeed before starting the IN-AIR alignment for the EGIs?

A

2 minutes

1H-65D-1
Page 3-74

72
Q

What info from the MDL is stored in the CDUs?

A

Reversionary site database, Mission Identifier database,
GPS almanac data, and Magnetic variation tables

1H-65D-1
Page 3-77

73
Q

What info from the MDL is not stored in the CDU’s?

A

Primary site database and flight plans

1H-65D-1
Page 3-77

74
Q

Dual MFD failure will result in a loss of what in the RADALT system?

A

Low altitude warning tones and visual indications (I.E., 40 and 200-foot)

1H-65D-1
Page 3-79

75
Q

What EP has the symptoms of:

  1. Complete loss of audio (all stations)
  2. All ICS and transmit functions inoperative
  3. Constant squeal or heard in headset?
A

Audio System Failure

1H-65D-1
Page 3-83

76
Q

When reading the Red Book what must be read first?

A

Title of the emergency

1H-65D-1
Page 3-5

77
Q

What is the corrective action for Audio System failure?

A
  1. Pilot and Copilot audio Bypass switches-bypass

1H-65D-1
Page 3-83

78
Q

In audio bypass what can the pilot transmit on?

A

COMM 1

1H-65D-1
Page 3-83

79
Q

In audio bypass what can the Copilot transmit on?

A

COMM 2

1H-65D-1
Page 3-83

80
Q

In audio bypass what can the FM transmit on?

A

No transmit capability

1H-65D-1
Page 3-83

81
Q

What EP has the symptoms of:

  1. “HEATERO/HEAT warning light illuminated
  2. ECS circuit breaker popped on Copilot panel
A

Heater Overheat

1H-65D-1
Page 3-89

82
Q

What is the corrective action for Heater Overheat?

A
  1. Heat Switch-off

1H-65D-1
Page 3-89

83
Q

Before egressing how long should you wait after landing?

A

8-10 Seconds

1H-65D-1
Page 3-103

84
Q

When ever possible where should you muster after egressing on land or water?

A

Up wind

1H-65D-1
Page 3-103

85
Q

Where should you muster after egressing on a ship?

A

Forward part of the ship

1H-65D-1
Page 3-103

86
Q

What EP has the symptoms of:

  1. Severe Vibration of unknown origin.
  2. insufficient power or control authority to maintain flight
  3. Other confirmed emergency procedure leading to land/ditch immediately?
A

Land/Ditch immediately

1H-65D-1
Page 3-108

87
Q

What is the corrective action for Land/Ditch Immediately?

A
  1. Crew and Passengers-alerted
  2. Wheels/floats-as required
  3. Land/Ditch
  4. EFSLs-both off
  5. Emergency Electrical cutoff-as required
  6. Rotor brake (land only)-on
  7. Emergency egress-execute

1H-65D-1
Page 3-108

88
Q

What is the corrective action for Emergency Egress?

A
  1. Wait
  2. Hold
  3. Jettison
  4. Cords
  5. Harness
  6. Egress
  7. Inflate

1H-65D-1
Page 3-109

89
Q

What EP symptoms are:

1. Cabin Sliding door does not fully open or will not secure in the closed position?

A

Malfunctioning cabin sliding door

1H-65D-1
Page 3-110

90
Q

What is the corrective action for Malfunctioning cabin sliding door?

A
  1. FM-remain secured to aircraft

1H-65D-1
Page 3-110

91
Q

What FD Mode can be used to get your out of an unusual attitude?

A

GA

1H-65D-1
Page 3-111

92
Q

What EP has the symptoms of:

1.Any unintentional, undesirable, or unsafe aircraft attitude?

A

Unusual attitude recovery

1H-65D-1
Page 3-111

93
Q

What is the corrective action for an Unusual Attitude Recovery?

A
  1. Level the wings
  2. Nose on the horizon
  3. Center the ball
  4. Power-adjust to maintain level flight

1H-65D-1
Page 3-111

94
Q

How should the pilot’s and copilot’s door be opened if using or going to be using the floats?

A

Jettisoned

1H-65D-1
Page 3-103

95
Q

What EP has the symptoms:

  1. Hoist cable fouled or caught ondeck or ground items
  2. Hoist cable visibly damaged
A

HOIST CABLE FOULED/DAMAGED

1H-65D-1
Page 3-95

96
Q

What is the corrective action for Hoist Cable Fouled/Damaged?

A

If injury or damage is imminent:
1. Announce “Cable Fouled.”
2. Activate host shear switch while announcing “Shear, Shear, Shear” (PF/PM/FM).
3. Once cable is clear, announce “Cable is away” (FM)
If conditions permit:
1. Pay out slack in cable
2. Advice PF.
3. Direct the vessel’s crew to free the cable.
4. If unable to free the cable or the cable is damaged, and situation permits, cut the cable utilizing cable cutters and announce “Cable is Away” (FM)
5.If mission urgency dictates a continued hoist, assemble the quick splice and complete the hoist with remaining cable length

1H-65D-1
Page 3-95

97
Q

What are the 2 caution about using the quick splice on the hoist?

A
  1. Unlikely the UP-LIMIT switch will actuate
  2. Sever damage to the hoist or cable may result if the quick splice is run to the UP-LIMIT switch

1H-65D-1
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98
Q

What EP has the symptom:

1. Hoist fails to respond to flight mechanic inputs?

A

Hoist Failure

1H-65D-1
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99
Q

What will cause the normal electrical power to be removed from the hoist?

A

Secondary hydraulic isolate condition

1H-65D-1
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100
Q

What are the corrective actions for a hoist failure?

A
  1. Announce “Hoist Failure” and advise the PF “Committed” or “Not Committed.”
    If committed:
  2. Check the cable and drum for fouling.
  3. Activate Emergency hoist power and continue the hoist
    If hoist power is not restored:
  4. Activate manual override and continue hoist
    If hoist fails to respond to manual override with no personnel in rescue device:
  5. Retrieve the rescue device if practicable
    If unable to retrieve rescue device:
  6. Cut cable with cable cutter or shear..
  7. Once cable is clear, announce “Cable is away.”
    If not committed:
  8. Abort the hoist

1H-65D-1
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101
Q

What are the warning and cautions with using manual override on the host?

A
  1. No Up-Limit switch
  2. Closed step 1 valve after hoist do to hoist creep

1H-65D-1
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102
Q

What EP has the symptom:

1. Hoist boom does not respond to electrical control inputs

A

Hoist Boom Failure

1H-65D-1
Page 3-97

103
Q

What is the corrective action for Hoist Boom Failure?

A
  1. Announce “Boom Failure”
  2. Hoist Master switch - check crew position
  3. Hoist act control and hoist act power circuit breaker (2) - cycle
    If boom is not in the fully stowed position and does not respond to electrical control inputs:
  4. Hoist act circuit breakers (2) - pull
  5. Hoist operator pendant - disconnect
  6. Manual crank - install
  7. Manually crank boom to stowed position
  8. Manual crank - remove
    If unable to move boom:
  9. Continue Flight as appropriate

1H-65D-1
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104
Q

What is the important thing to know about Boom Stow and Boom in-out during a boom failure?

A

Boom Stow works regardless of the MASTER or emergency switch position

1H-65D-1
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105
Q

What EP has the symptom:

1. Hoist cable extends/retracts without crew input

A

Hoist Electrical Runaway

1H-65D-1
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106
Q

What is the corrective action for Hoist Electrical runaway?

A
  1. Secure Hoist Power at the hoist control panel only
  2. Announce “Hoist Runaway” and advise the PF “Committed” or “Not Committed”
    If committed to the hoist or mission urgency dictates:
  3. activate manual override and continue the hoist.
    If not committed to the hoist
  4. Abort the hoist

1H-65D-1
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107
Q

Why do we not secure the hoist at the cockpit hoist master switch during a hoist electrical runaway?

A

Shear capabilities will be lost

1H-65D-1
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108
Q

What EP has the symptom:

1. PF and/or FM unable to listen and/or talk during a hoist?

A

Lost Communications during hoisting operations

1H-65D-1
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109
Q

What is the corrective action for Lost Communications during hoisting operations?

A
  1. FM Tap the PF and give hold signal
  2. Announce “ICS Failure” and advise the PF “Committed” or “Not Committed”
    If committed:
  3. Communicate by vocal commands and continue hoist
    Once hoist is completed:
  4. FM - Ensure hot mic is selected, Helmets properly connected: attempt Hot Mic ICS Comms.
    If communications are not restored:
  5. Press push-to-talk switch - attempt normal comms
    If communications are still no restored:
  6. Audio control panel - select altn and attempt comms (ALL CALL and HOT MIC are inoperative in ALTN)
    If communications are still not restored:
  7. Abort mission
    If not committed:
  8. Abort Hoist

1H-65D-1
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110
Q

What is the corrective action for Lost RS Day?

A
  1. Mark and Record position
  2. Transition and establish Right Orbit
  3. Look and Listen for RS signal
  4. When Visual - Resume hover position
    If these procedures fail to relocate RS:
  5. Complete leaving RS on scene procedure

1H-65D-1
Page 3-100

111
Q

What is the corrective action for Lost RS night?

A
  1. Mark and record position
    2.Flash landing/hover light
  2. Look and listen for RS signal
  3. When visual - cease flashing light
    If these procedures fail to relocate RS:
  4. Complete leaving RS on scene procedure

1H-65D-1
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112
Q

What EP has the symptom:

RS signals In Trouble, Need assistance

A

Emergency recovery of RS

1H-65D-1
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113
Q

When there is a hazard to the RS what do you do?

A

Place the rescue device or bare hook between the RS and the hazard

1H-65D-1
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114
Q

When is a rescue brief not required?

A

During emergency recovery of the RS

1H-65D-1
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115
Q

What is the corrective action for emergency recovery of RS?

A
  1. Rescue Basket - If rigged and empty
  2. Bare Hoist hook - if basket not readily available
  3. With the assistance of the FM, the RS shall enter the cabin backwards

1H-65D-1
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116
Q

What is the corrective action for RS falls through ice with Hoist cable attached`?

A
  1. RS - extract out of the ice hole by rolling out, or pulling out with the ice awls or hoist cable.
  2. Establish a hover. FM conns helo into position so that the RS may be hoisted out of the hole

1H-65D-1
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117
Q

What is the corrective action for RS falls through ice without hoist cable attached?

A
  1. RS - extract out of the ice hole by rolling out, or pulling out with the ice awls.
    If the RS is unable to extract:
  2. Complete emergency recovery of the RS

1H-65D-1
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118
Q

What is the corrective action for Emergency breakaway of disembarked RS on ice?

A
  1. On pre briefed frequency PF announce, “Breakaway, Breakaway, Breakaway.”
  2. Activate Hoist/shear switch while announcing “Shear, Shear, Shear” on pre briefed frequency.
  3. Once cable is clear, announce “Cable Away.”
  4. Complete leaving RS onscene Procedures

1H-65D-1
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119
Q

What is the corrective action for leaving RS onscene?

A
  1. Mark and record position
  2. Deploy lighted raft
  3. Deploy DMB
  4. Notify Opcen or other Rescue Resource

1H-65D-1
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Archive (12 decks)

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