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EP's and Limits > EP's > Flashcards

EP's Flashcards

1
Q

Define:

LAND WITHOUT DELAY

A

a landing in which the primary consideration is continued control of the aircraft and survival of the occupants. It is meant to be more urgent than Land As Soon As Possible. The situation may not permit the aircrew to continue to maneuver the aircraft to a suitable landing area (e.g. open field). If maneuvering to an open area is not practical, then the crew must make the decision to land in an area that will have the least amount of negative impact on crew survivability. (e.g. Over dense forest, select an area with the smallest trees, in a mountainous area, choose an area with the least amount of slope).

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2
Q

Define:

LAND AS SOON AS POSSIBLE

A

landing at the nearest suitable landing area (e.g. open field) without delay. The primary consideration is to ensure the survival ofoccupants.

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3
Q

Define:

LAND AS SOON AS PRACTICABLE

A

landing at a suitable landing area.The primary consideration is the urgency of the emergency.

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4
Q

Define:

AUTOROTATE

A

adjusting the flight controls as necessary to establish

an autorotational descent and landing.

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5
Q

EMERG ENG SHUTDOWN

A

POWER lever (affected engine) — OFF.

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6
Q

Emergency Egress

A
  1. Helmet visors — Down.
  2. Area around helicopter — Clear of

personnel.

  1. CANOPY JETTISON handle — Turn 90°,

release, then push to jettison canopy.

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7
Q

Dual Engine Failure

A
  1. AUTOROTATE.
  2. CHOP button — Reset only if an engine

chop warning message is present.

Reset may be accomplished by either

crewmember.

  1. Wing Stores Jettison — As appropriate.
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8
Q

ABORT START PROCEDURES

A
  1. POWER lever — OFF.
  2. ENG START switch — IGN ORIDE for 30

seconds and TGT is below 540° C.

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9
Q

Single Engine Failure

A
  1. Airspeed — Adjust as appropriate.
  2. Wing Stores Jettison — As appropriate.
  3. LAND AS SOON AS PRACTICABLE.
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10
Q

Engine 1 or 2 Overspeed – NP Failed High.

A
  1. Collective — Adjust to maintain NR within limits.

If condition persists:

  1. POWER lever (affected engine) — Retard

to equalize torque.

  1. LAND AS SOON AS PRACTICABLE.
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11
Q

Low RPM Rotor – NP Failed Low.

A
  1. Collective — Adjust to maintain NR within limits.

If condition persists:

  1. POWER lever (affected engine) —LOCKOUT

and then retard to equalize torque output of both engines.

If manual control is not possible:

  1. POWER lever (affected engine) — IDLE.
  2. LAND AS SOON AS PRACTICABLE.
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12
Q

Engine Compressor Stall.

A
  1. Collective — Reduce.

If condition persists:

  1. POWER lever (affected engine) — Retard.

If TGT decreases and there is no further evidence of a

stall;

  1. POWER lever (affected engine) — FLY.

If stall condition recurs:

  1. POWER lever (affected engine) — IDLE.
  2. LAND AS SOON AS PRACTICABLE.
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13
Q

Loss of Tail Rotor Thrust in Cruise Flight.

Continued Flight Possible.

A
  1. Airspeed — 100 KTAS minimum (until 10

to 20 ft above touchdown).

  1. Wing Stores Jettison — As appropriate.
  2. POWER levers — Retard as necessary (5 to 10 ft above touchdown).
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14
Q

Loss of Tail Rotor Thrust in Cruise Flight.

Continued Flight Not Possible

A
  1. Collective reduce (compromise between

rate of turn and rate of descent).

  1. Wing Stores Jettison — As appropriate.
  2. Minimize rate of descent (10 to 20 feet above touchdown).
  3. POWER levers — OFF (5 to 10 feet above

touchdown).

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15
Q

Loss of Tail Rotor Thrust at Low Airspeed/Hover.

A
  1. Collective — Reduce (compromise

between rate of turn and rate of descent).

  1. Wing Stores Jettison — As appropriate.
  2. Minimize Rate of Descent — (10 to 20 ft

above touchdown).

  1. POWER levers — OFF (5 to 10 feet above

touchdown).

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16
Q

Tail Rotor Fixed Pitch Malfunction

(IGE turning left)

A

a reduction in the POWER levers coordinated with an increase in collective may slow or stop the rotation so that a controlled power on descent to landing can be accomplished.

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17
Q

Tail Rotor Fixed Pitch Malfunction

(IGE turning right)

A

If the aircraft has an uncontrolled turn to the right, reduce collective** to begin descent. **At approximately 5 to 10 ft

AGL, perform a hovering autorotation** **by CHOP button - Press or POWER** **Levers - OFF.

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18
Q

Tail Rotor Fixed Pitch Malfunction

(IGE not turning)

A

If the aircraft is not turning, a slight reduction in collective pitch will begin a descent. During the descent, a slight rotation to the left may be present; increasing collective just prior to touchdown should stop the rotation.

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19
Q

Tail Rotor Fixed Pitch Malfunction

(OGE little or no right rotation or left rotation)

A

If little or no right rotation or if left rotation is experienced and control can be maintained, the aircraft should be accelerated into forward flight and perform approach and landing appropriate to power setting and condition of flight at time of failure.

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20
Q

Tail Rotor Fixed Pitch Malfunction

(OGE cannot accelerate into forward flight)

A

If the aircraft cannot be accelerated into forward 􀃀ight, initiate a power-on descent. Collective should be adjusted so that an acceptable compromise between rate of turn and rate of descent is maintained. At approximately 5 to 10 ft above touchdown, perform a hovering autorotation by CHOP button - Press or POWER levers -OFF.

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21
Q

Main Transmission Input Drive Clutch Failure.

(In flight)

A
  1. POWER lever (affected engine) — IDLE.

If NP (affected engine) is below NR (indicating the clutch

is disengaged):

  1. EMERG ENG SHUTDOWN (affected engine).
  2. LAND AS SOON AS PRACTICABLE.

If NP (affected engine) does not drop below NR (indicating

the clutch has failed to disengage):

  1. LAND AS SOON AS POSSIBLE.
  2. EMERG ENG(S) SHUTDOWN (both engines

simultaneously).

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22
Q

Main Transmission Input Drive Clutch Failure.

(On ground)

A

(with indications that a clutch has failed to engage):

  1. EMERG ENG SHUTDOWN (affected engine only).
  2. Check NG is less than 10% (affected engine).
  3. Normal engine shutdown — Perform.

(with indications that a clutch has failed to disengage):

EMERG ENG(S) SHUTDOWN (both engines simultaneously).

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23
Q

Engine Fire

(In flight)

A
  1. EMERG ENG SHUTDOWN (affected engine) — when conditions permit.
  2. Illuminated ENG FIRE button — Press and RDY light illuminates.
  3. FIRE DISCH button(s) — Press.
  4. LAND AS SOON AS POSSIBLE.
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24
Q

Engine Fire

(On ground)

A
  1. EMERG ENG(S) SHUTDOWN.
  2. Illuminated ENG FIRE button — Press and RDY light illuminates.
  3. FIRE DISCH button(s) — Press.
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25
Q

APU Fire (On ground)

A
  1. APU — OFF.
  2. Illuminated APU FIRE button — Press and

RDY light illuminates.

  1. FIRE DISCH button(s) — Press.
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26
Q

APU Fire (In flight)

A
  1. Illuminated APU FIRE button — Press and

RDY light illuminates.

  1. FIRE DISCH button(s) — Press.
  2. LAND AS SOON AS POSSIBLE.
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27
Q

Deck Fire

A

LAND AS SOON AS POSSIBLE.

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28
Q

Fuselage Fire On Ground

A
  1. EMERG ENG(S) SHUTDOWN.
  2. APU — OFF (If applicable).
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29
Q

Electrical Fire In Flight

A
  1. GEN1 and GEN2 — OFF (SYS page).
  2. LAND AS SOON AS POSSIBLE.
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30
Q

Smoke and Fume Elimination

A
  1. Airspeed — Slow to 20 KTAS maximum.
  2. Canopy door (affected Crew Station) — Open to intermediate position.
  3. LAND AS SOON AS POSSIBLE.
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31
Q

Both Generators Fail/Complete Loss Of Electrical Power

A
  1. GEN 1 and GEN 2 — Reset Pilot GEN RST panel.

If condition persists:

  1. LAND AS SOON AS POSSIBLE.
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32
Q

Single Generator and Single RTRU Failure

A
  1. Affected GEN 1 or GEN 2 — Reset Pilot

GEN RST panel.

If condition persists:

  1. LAND AS SOON AS PRACTICABLE.
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33
Q

Dual TRU Failure (Transformer Rectifier 1 and Transformer Rectifier 2)

A

LAND AS SOON AS POSSIBLE.

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34
Q

Primary Hydraulic Pressure Low and Utility Hydraulic Pressure Low.

A
  1. EMERG HYD button — Press ON.
  2. LAND WITHOUT DELAY.
  3. EMERG ENG(S) SHUTDOWN.
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35
Q

Primary Hydraulic Pressure Low and Utility Hydraulic Level Low

A

LAND AS SOON AS POSSIBLE

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36
Q

EMERGENCY LANDING IN WOODED AREAS

(POWER OFF)

A

AUTOROTATE — Apply full collective to decay rotor RPM as helicopter settles.

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37
Q

DITCHING (POWER ON)

A
  1. Approach to hover.
  2. Canopies — JETTISON prior to entering

water.

  1. Pilot shoulder harness — Lock.
  2. CPG — Exit helicopter.
  3. Hover downwind to a safe distance.
  4. POWER levers — OFF.
  5. Perform hovering autorotation — Apply

full collective to decay RPM as helicopter

settles.

  1. Cyclic — Position in direction of roll.
  2. Exit when main rotor has stopped.
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38
Q

DITCHING (POWER OFF)

A
  1. AUTOROTATE — Apply full collective to

decay rotor RPM as helicopter settles.

  1. Canopies — JETTISON prior to entering water.
  2. Cyclic — Position in direction of roll.
  3. Exit when main rotor has stopped.
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39
Q

BUCS Fail

A
  1. LAND AS SOON AS POSSIBLE.
  2. APU — ON.
  3. EMERG ENG(S) SHUTDOWN.
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40
Q

BUCS On

A
  1. LAND AS SOON AS POSSIBLE.
  2. APU — ON.
  3. EMERG ENG(S) SHUTDOWN.
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41
Q

Main Rotor Components

A
  1. LAND AS SOON AS POSSIBLE.
  2. EMERG ENG(S) SHUTDOWN
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42
Q

EGI In-Flight Misalignment

A
  1. Position update — Perform. Monitor POSITION CONFIDENCE.

If misalignment continues:

  1. Airspeed — Adjust to level unaccelerated flight at 80 KTAS or less at a constant heading.
  2. Select misaligned EGI as Secondary.
  3. Reset Secondary INU.
  4. After the INU reset, wait a minimum of 90 seconds after the primary INU select button (L3) becomes unbarriered to allow adequate time for detecting and displaying an INU MISCOMPARE caution/advisory event. During this time interval, do not change Primary

INU’s for an INU miscompare caution or advisory.

If misalignment continues:

  1. Stabilator — Monitor position and manually control as required.
  2. LAND AS SOON AS PRACTICABLE.
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43
Q

INU Miscompare - Attitude (ATT) or Heading (HDG).

A
  1. Select TSD UTIL page — Note primary INU. Compare the Standby Attitude Indicator and/or Magnetic Compass to the flight page. If the data is correct leave the INU as primary.
  2. LAND AS SOON AS PRACTICABLE.

If there is a noticeable difference between the Standby

Attitude Indicator and/or Magnetic Compass and flight

page data:

  1. Select the other INU as primary.

If condition persists:

  1. LAND AS SOON AS PRACTICABLE.
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44
Q

INU Miscompare - Velocity (VEL).

A
  1. Select TSD UTIL page — Reference Doppler Data Status Window to determine if the INU selected as primary is displaying a yellow triangle indicator in any axis.

If the primary INU is not reporting the miscompare:

  1. LAND AS SOON AS PRACTICABLE.

If the primary INU is reporting a miscompare:

  1. Select the other INU as primary.

If condition persists:

  1. LAND AS SOON AS PRACTICABLE.
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45
Q

9-18. STABILATOR AUTOMATIC MODE FAILURE

A
  1. RESET button — Press.

If automatic mode is not restored:

  1. Use manual stabilator control.
46
Q

9-19. STABILATOR AUTO AND MANUAL MODE FAILURE

A

LAND AS SOON AS PRACTICABLE

47
Q

9-20. STABILIZATION EQUIPMENT MALFUNCTION

A
  1. FMC release button — Press.
  2. FMC — Re-engage unaffected FMC axes

(A/C UTIL page).

48
Q

9-22. WING STORES JETTISON

a. All Armament Wing Stores.

A
  1. Airspeed — 130 KTAS maximum.
  2. Collective JETT button — Press.
49
Q

9-22. WING STORES JETTISON

b. Selected Armament Wing Stores.

A
  1. Airspeed — 130 KTAS maximum.
  2. Selected STORES JETTISON buttons —

Press to ARM.

  1. JETT button — Press.
50
Q

c. External Fuel Wing Stores.

A
  1. Airspeed — 100 KTAS maximum.
  2. Selected STORES JETTISON buttons —

Press to ARM.

  1. JETT button — Press.
51
Q

9-23. FLARE EMERGENCY JETTISON

A
  1. CMDS JETTISON button—Press to ARM.
  2. JETT button — Press.

or

  1. JETTISON switch cover — Open.
  2. JETTISON switch — Up.
52
Q

PNVS Failure.

A

NVS select switch (Pilot) — TADS.

53
Q

IHADSS/HDU Failure or IHADSS STALE.

A
  1. NVS MODE switch — FIXED.
  2. NVS select switch — TADS or PNVS.
  3. VID page — PLT or CPG HMD (as
    necessary) .
54
Q

Single DP Operation.

A
  1. NVS SELECT Switch — Reselect (PNVS

or TADS).

or

  1. Crewmember (not on controls) — Assume

control.

55
Q

Dual DP Failure.

A

LAND AS SOON AS POSSIBLE.

56
Q

Dual SP Failure

A

LAND AS SOON AS POSSIBLE

57
Q

GEARBOX VIBRATION

A

LAND AS SOON AS POSSIBLE

58
Q

AFT DECK FIRE

A

LAND AS SOON AS POSSIBLE

59
Q

TAIL ROTOR HYD

A

LAND AS SOON AS POSSIBLE

60
Q

ACC OIL PSI LOW

A

APU only: Shutdown as soon as

possible.

In flight: LAND AS SOON

AS PRACTICABLE.

61
Q

AFT FUEL LOW

A

LAND AS SOON AS PRACTICABLE

62
Q

APU ON

A

APU button - Press

63
Q

AUTO/MAN STAB FAIL

A

LAND AS SOON AS PRACTICABLE

64
Q

ENGINE 1 or 2 CHIPS

A

POWER lever - IDLE when conditions permit.

LAND AS SOON AS PRACTICABLE.

65
Q

ENG 1 or 2 FUEL BYPASS

A

POWER lever - IDLE when conditions permit.

LAND AS SOON AS PRACTICABLE

66
Q

ENG 1 or 2 FUEL PSI LOW

A

Achieve safe single engine airspeed.

LAND AS SOON AS PRACTICABLE.

67
Q

Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW

A

FUEL page, BOOST button - Press ON.

LAND AS SOON AS POSSIBLE

68
Q

ENG 1 or 2 OIL BYPASS

A

POWER lever - IDLE when conditions permit.

LAND AS SOON AS PRACTICABLE.

69
Q

ENG 1 or 2 OIL PSI LOW

A

EMERG ENGINE SHUTDOWN when conditions permit. LAND AS SOON AS PRACTICABLE.

70
Q

FORWARD FUEL LOW

A

LAND AS SOON AS PRACTICABLE.

71
Q

GEARBOX TEMP HIGH

A

LAND AS SOON AS PRACTICABLE

72
Q

GEARBOX VIBRATION

A

LAND AS SOON AS POSSIBLE

73
Q

GEARBOX 1 or 2 CHIPS

A

POWER lever - IDLE when conditions permit.

LAND AS SOON AS PRACTICABLE.

74
Q

GEARBOX 1 or 2 OIL HOT

A

POWER lever - IDLE when conditions permit.

LAND AS SOON AS PRACTICABLE.

75
Q

GENERATOR 1 or 2 FAIL

A

GEN RST panel - GEN 1 or GEN 2.

If condition persists:

LAND AS SOON AS PRACTICABLE.

76
Q

GRBX 1 or 2 OIL PSI LOW

A

POWER lever - IDLE when conditions permit.

LAND AS SOON AS PRACTICABLE

77
Q

ICING SEVERE

A

Verify or turn on anti-ice system

78
Q

MAG FORCE TRIM OFF

A

Turn Force Trim ON.

79
Q

MAIN XMSN CHIPS

A

LAND AS SOON AS POSSIBLE.

80
Q

PRI HYD BYP

A

LAND AS SOON AS PRACTICABLE.

81
Q

PRI HYD LEVEL LOW

A

LAND AS SOON AS PRACTICABLE

82
Q

PRI HYD PSI LOW

A

LAND AS SOON AS POSSIBLE

83
Q

Both RECTIFIER 1 FAIL and RECTIFIER 2 FAIL

A

LAND AS SOON AS POSSIBLE

84
Q

ROTOR BRAKE ON/LK

A

RTR BRK switch - OFF.

LAND AS SOON AS POSSIBLE.

85
Q

UTIL HYD BYP

A

LAND AS SOON AS PRACTICABLE.

86
Q

UTIL HYD LEVEL LOW

A

LAND AS SOON AS PRACTICABLE

87
Q

UTIL HYD PSI LOW

A

LAND AS SOON AS POSSIBLE.

88
Q

XFEED 1 or 2 VALVE FAIL

A

Achieve safe single engine airspeed.

If CAUTION message extinguishes, continue mission.

If CAUTION message remains,

be prepared for a single engine flame-out.

LAND AS SOON AS PRACTICABLE.

89
Q

XMSN 1 or 2 OIL HOT

A

LAND AS SOON AS PRACTICABLE.

90
Q

Both XMSN 1 OIL HOT and XMSN 2 OIL HOT

A

LAND AS SOON AS POSSIBLE

91
Q

XMSN 1 or 2 OIL PSI LOW

A

LAND AS SOON AS PRACTICABLE.

92
Q

Both XMSN 1 OIL PSI LOW and XMSN 2 OIL PSI LOW

A

LAND AS SOON AS POSSIBLE.

93
Q

ATS1 or ATS2 HANG

A

Eng START switch to IGN ORIDE, then OFF

94
Q

AUTO STAB FAIL

A

RESET button - Press.

95
Q

BLEED AIR HOT

A

Identify High TGT Engine and turn OFF affected bleed air.

96
Q

CANOPY OPEN

A

Identify and close appropriate canopy.

97
Q

EXT PWR DOOR OPEN

A

Close the external power door.

98
Q

ICING DETECTED

A

Verify or turn on anti-ice system.

99
Q

IGN 1 or 2 FAILED ON

A

Perform Abort Start Procedure.

100
Q

MPD HOT

A

Reduce Crew Station ECS temperature; and reduce

MPD brightness as much as practicable.

101
Q

SAS SATURATED

A

Re-trim aircraft.

102
Q

Cockpit Fogging

A

Ensure the CANOPY ANTI-ICE is ON.

Select DEFOG ON. If canopy fogging is not visibly reduced, turn DEFOG OFF.

103
Q

Lightning Strike Causes Loss of Power

A

The flight crew shall have to react immediately

to retard the POWER levers to IDLE and enter

autorotation. The pilot could then advance the POWER

levers, restoring power.

104
Q

Surface Winds Above 45 Knots Inadvertently Encountered

A
  1. Aircraft — Head into the wind.
  2. NP/NR — 101%.
  3. TAIL WHEEL button — LOCK.
  4. PARK BRAKE — Set.
  5. Stabilator — AUTO.
  6. Cyclic and Collective — Adjust as required.
105
Q

Engine Bleed Air Start

A

Ensure adequate bleed air pressure is available by increasing collective pitch to a value that will increase NG of the bleed air source engine to a minimum of 95%.

106
Q

Define: Emergency Engine Shutdown

A

engine shutdown without delay. Engine shutdown in flight is usually not an immediate action item unless a fire exists. Before attempting an engine shutdown, identify the affected engine by checking engine-out warning messages on the EUFD and observe the ENG page for TGT, NP, NG, TORQUE%, and OIL PSI.

107
Q

Define: Wing Stores Jettison

A

jettisoning any or all of the wing stores as appropriate using one of two methods: emergency and selective. The method to be used will be determined by the aircrew depending on the situation at the time of the emergency and the wing stores inventory.

108
Q

Goggle Failure

A
  1. Announce ANVIS failure by crew station.

During NOE or contour flight, begin a climb at a rate that will ensure obstacle avoidance.

  1. Transfer the flight the controls if applicable.
  2. Troubleshoot ANVIS failure.
  3. Announce results of troubleshooting
109
Q

Failure of both primary and secondary drives to the accessory gearbox

A

activate the Emergency Hydraulics and LAND WITHOUT DELAY.

110
Q
A

EP's and Limits (2 decks)

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