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Chapter 9 Emergency Procedures > EP's > Flashcards

EP's Flashcards

1
Q

Emergency Engine Shutdown

A 
Eng Pwr Control Levers   -  OFF
Eng Emer Off Handles    -  Pull
Fuel Boost Pump Ctl Switches  -  OFF 
Monitor TGT if above 538 C
Air Source Heat Start Switch  -  As Req
Eng Ignition Switch   -  OFF
Starter button press and motor for 30 seconds or until TGT is below 538 C
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2
Q

Lockout Definition

A

manual control of the engine RPM while bypassing the 700 ECU and 701 DEC functions. Bypass will be required with RPM 1 or 2 decreases below normal demand speed.

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3
Q

Lockout

A

EPCL pull down and advance full forward while maintaining downward pressure. Then adjust to set RPM as required.

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4
Q

EMER APU Start

A

APU start to accomplish an emergency procedure.
Fuel Pump Switch - APU Boost
APU Control Switch - On

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5
Q

Single Engine Failure

A 
Collective - Adjust to maintain %RPMR
External Cargo/Stores - Jettison (if required)
If continued flight is not possible
LASAP
If continued flight is possible
Establish Single Engine Airspeed
LASAPrac
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6
Q

Dual Engine Failure

A

Autorotate

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7
Q

Decreasing % RPM R

A

Collective - Adjust to control % RPM
EPCL - (Low Torque low TGT Engine) LOCKOUT maintain trq approx 10% below other eng
Land ASAPract

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8
Q

Increasing % RPM R

A

EPCL - (high Torque high TGT Engine) Retard - maintain trq approx 10% below other eng
Land ASAPrac
if Eng is not responding between fly and idle
establish SE airspeed
Emer Eng Shutdown on affected engine
Refer to SE failure emergency procedure

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9
Q

Engine Compressor Stall

A 
Collective - Reduce
if condition persists
EPCL - Retard to retard (TGT should decrease)
EPCL - Fly 
if condition reoccurs
Establish SE airspeed
Emer Eng Shutdown - affected engine
Refer to SE failure emergency procedures
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10
Q 
Engine Oil Filter Bypass Caution 
Engine Chip Caution
Eng Oil Pressure Caution
Eng Oil Temp Caution
Engine Oil Press / Temp high / low
A 
EPCL - (affected engine) Retard (to reduce trq) 
if oil pressure is low or temp is high
Establish Emer SE Airspeed
Emer Eng Shutdown - affected eng
Refer to SE failure emergency procedures
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11
Q

Engine High Speed Shaft Failure

A

Collective - Adjust
Establish SE Airspeed
Emer Eng Shutdown - Affected engine
Refer to SE failure emergency procedure

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12
Q

Lightning Strike

A

EPCL - Adjust as req to control RPM R

Land ASAP

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13
Q

Loss of Tail Rotor Thrust in cruise flight

A

Airspeed adjust to 80 kias or above
Autorotate - maintain airspeed at or above 80 kias
EPCL - Off (during deceleration when intended point of landing is assured)

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14
Q

Loss of TR Thrust or Tail Rotor Quadrant caution appears with loss of control at low airspeed / hover right rotation

A

Collective - reduce

EPCL - OFF (5-10 feet above touchdown)

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15
Q

Tail Rotor Quadrant caution appears in Cruise Flight

A

Collective - adjust to determine controllability fixed right or left
Land ASAPrac

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16
Q

Tail Rotor Quadrant caution appears or loss of control at low airspeed / hover left rotation

A

EPCL - Retard to begin a partial power decent
Collective - adjust to preserve RPM R
EPCL - OFF (5-10 feet above touchdown)
Collective - Adjust for landing

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17
Q

Pedal Bind/Restriction or drive with no accompanying caution

A

Apply pedal force to oppose the drive

18
Q

Main XMSN Oil press caution appears / XMSN press low/ XMSN oil temp high or XMSN Oil Temp caution appears

A 
Land ASAP
if time permits 
slow to 80 kias
EMER APU Start
gen 1 & 2 off
19
Q

Chip input mdl LH or RH

A

EPCL - affected engine IDLE

Land ASAP

20
Q

Chip main MDL Sump, Chip access MDL LH or RH, Chip Tail XMSN or Chip INT XMSN/Tail XMSN Oil Temp or INT XMSN Oil Temp caution appears

21
Q

Main XMSN Failure

A

Collective - adjust only enough to begin a partial power decent with power remaining applied to the main xmsn throughout the decent and landing.
Land ASAP

22
Q

Enging / Fuselage Fire Grnd

A

EPCL - OFF
EMER Eng off handle - PULL
Fire EXTGH switch - MAIN/RESERVE as req

23
Q

APU Compartment Fire

A

APU Fire T-Handle - PULL

Fire EXTGH switch - Main/Reserve as required

24
Q

ENG Fire in Flight

A 
Establish SE airspeed
EPCL - (affected engine) OFF
Eng Emer Off Handle - pull
Fire EXTGH switch - Main/Reserve as required
Land ASAP
25
Q

Electrical Fire in Flight

A

Batt and Gen switches - OFF

Land ASAP

26
Q

1 and #2 Fuel Filter Bypass caution

27
Q

1 or #2 Fuel Pressure caution

A

Eng Fuel system selector (affect engine) - XFD
Fuel Boost pump ctl switch - ON (as applicable)
Land ASAP
Emer Eng Shutdown after landing

28
Q

1 and #2 Fuel Pressure Caution appear

A

Land ASAP

Emer Eng Shutdown after landing

29
Q

1 and #2 GEN Failure (#1 & #2 Conv and AC Essential BUS off cautions appear)

A

EMER APU START

30
Q

1 & #2 HYD Pump Cautions appear

A

Land ASAP - restrict control movements to moderate rates.

31
Q

1 or #2 HYD Pump Caution Appear and Back-up pump advisory doesn’t appear

A

Airspeed - Adjust - to a comfortable airspeed
Back-Up Hyd Pump Switch - ON
if back up pump advisory does not
FPS and Boost Switches - OFF for #2 Hyd Pump
Land ASAP

32
Q

1 or #2 Primary Servo Pressure Caution Appears

A

SVO Off Switches - Check both are centered
If the caution appears with SVO off centered, move the svo off switch to turn off the malfunctioning svo
Land ASAP

33
Q

1 RSVR LOW & #1 HYD PUMP Caution appear with Back-up pump appearing

A

Land ASAPrac
if Back-Up RSVR Low caution also appears
SVO OFF Switch - 1st stage
LAND ASAP

34
Q

2 RSVR LOW & #2 HYD PUMP Caution appears with Back-Up Pump appearing

A 
Power on Reset switches - simultaneously press then release
Land ASAPrac
if Back-Up RSVR Low caution also appears
SVO OFF Switch - 2nd stage
Land ASAP
35
Q

Collective Boost SVO Hardover/Power piston failure (up to 150 lbs)

A

Boost Switch - OFF

Land ASAPrac

36
Q

Ditching Power Off

A

Autorotate
Cockpit doors jettison and cabin doors open prior to entering water
cyclic - position in direction of roll
exit when main rotor has stopped

37
Q

Flight Control/Main Rotor System Malfunction

A

Land ASAP

Emer Eng Shutdown after landing

38
Q

Stabilator Malfunction - Auto Mode Failure

A

Cyclic Mounted Stabilator Slew up switch - Adjust if necessary to prevent nose down pitch rate
Auto Control Reset - Press on once after establishing a comfortable airspeed

39
Q

Uncommanded Nose Down Pitch Attitude Change

A

Cyclic - Adjust as required
Collective - Maintain or increase
Cyclic Mounted Stabilator Slew up switch - adjust as required to arrest nose down pitch rate

40
Q

Uncommanded Nose Up Pitch Attitude Change

A

Cyclic - Adjust as required
Collective - Reduce as required
Man Slew Switch -

41
Q

Emergency Release of Rescue Hoist Load

A

cable cut from cockpit
Cable Shear Switch - Fire
cable cut from hoist operators position
Cable Cut Switch - Fire

Chapter 9 Emergency Procedures (1 decks)

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