EP/Limits Exam Flashcards

1
Q

Single Engine Emergency Shutdown

A
  1. Twist grip (affected engine) - rotate slowly to idle, check indications, then to off
  2. Rotor Speed - trim to maximum
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Double Engine Emergency Shutdown

A

ON GROUND
1. Both twist grips - OFF
2. Both FUEL PRIME PUMP sw - OFF
3. BAT MSTR sw - OFF

IN FLIGHT
1. Both twist grips - OFF
If there is an indication that the engines are still running:
2. Both EMER OFF sw - Press

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Warning Light Indications - FIRE (ENG 1 or 2)

A

OAF BC ASL BL

  1. OEI Conditions - Establish
  2. Airspeed - reduce if IAS is exceeding 100 KIAS
  3. Fire sw (affected eng) - Raise guard, Press
  4. BOT 1/BOT 2 pb - Press; Bot 1 activated; EXT indicator light comes on (EMER OFF sw pnl)
  5. Clock - start (when BOT 1 legend and EXT indicator light go off) (EMER OFF sw pnl)
  6. Affected engine - ID
  7. Single engine emer s/d - Perform
    (8. Passengers - Alert)
  8. Land as soon as POSSIBLE

(if fire warning still on after 1 min)
10. BOT 1/BOT 2 pb - Press; Bot 1 activated; EXT indicator light comes on (EMER OFF sw pnl)

(if fire warning remains on)
11. Land IMMEDIATELY

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Caution Indication - ENG CHIP (System 1 or 2)

A

ON GROUND
1. Affected Engine - ID
2. Single engine emer s/d - Perform

IN FLIGHT
1. OEI flight condition - Establish
2. Affected Engine - ID
Alternatives:
3a. Single engine emer s/d - Perform
3b. Twist grip (affected engine) - Rotate slowly to IDLE, check indications
4. Land as soon as PRACTICABLE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Caution Indication - ENG OIL P (System 1 or 2)

A
  1. Engine oil pressure - check
  2. OEI flight condition - establish
  3. Affected engine - ID
  4. Single engine emer s/d - Perform
  5. Land as soon as PRACTICABLE
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Engine Oil Temperature High

A
  1. OEI flight condition - Establish
  2. Affected Engine - ID
  3. Twist grip (affected eng) - Adjust to 20-30% torque
  4. Oil Temperature Indicator - Monitor

(if engine oil temp decreases below limit)
5. Land as soon as PRACTICABLE

(if engine oil temp still remains above limit)
5. Single engine emer s/d - Perform
6. Land as soon as PRACTICABLE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Warning Light Indications - LOW FUEL (1 and/or 2)

A
  1. Fuel quantity indication - Check
    (if positive fuel indication in main tank)
  2. Both fuel pump XFER sw - Check ON
  3. Both fuel pump XFER circuit breakers - Chcek IN
    (if both FUEL LOW warning lights remain on)
  4. Land Within 10 minutes
    (if one FUEL LOW warning light remains on)
  5. Expect Single Engine Failure
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Single Engine Failure - Takeoff

A
  1. Collective Lever - adjust to maintain rotor RPM

REJECTED TAKEOFF:
2. Landing Attitude - Establish
3. Collective Lever - raise as necessary to stop descent and cushion landing
4. Affected Engine - ID
5. Single engine emer s/d - Perform

TRANSITION TO OEI FLIGHT:
2. Collective Lever - adjust to OEI limits or below
3. Rotor Speed - trim to maximum
4. Airspeed - Gain, 65 KIAS
5. Collective Lever - reduce to OEI MCP or below
6. Affected engine - ID
7. Single engine emer s/d - Perform
8. Land as soon as PRACTICABLE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Warning Light Indications - XMSN OIL PRESS

A

(if one XMSN oil press is below 1 bar)
1. Power - reduce
2. Land as soon as PRACTICABLE
(if both XMSN oil press are below 1 bar)
1. Land IMMEDIATELY

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Caution Indications - XMSN OIL TEMP

A
  1. XMSN oil temp and oil press indications - Check Indication
    (if indications are within limits)
  2. Land as soon as PRACTICABLE
    (if indications are above limits)
  3. Power - reduce, as much as possible
    (if oil temp indication remains above limit)
  4. Land as soon as POSSIBLE
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Single Engine Failure - Hover IGE

A

CLCAS

  1. Collective lever - adjust to OEI limits or below
  2. Landing attitude - Establish
  3. Collective lever - raise as necessary to stop descent and cushion landing
  4. Affected engine - ID
  5. Single engine emer s/d - Perform
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Single Engine Failure - Flight

A

ORASL

  1. OEI flight conditions - establish
  2. Rotor speed - trim to maximum
  3. Affected engine - ID
  4. Single engine emer s/d - Perform
  5. Land as soon as PRACTICABLE
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Warning Light Indications - ROTOR RPM

A

NRO Low:
-NRO (95%) or less - (steady light)
-Audio signal - (low-pitched beeping tone)
NRO High:
-NRO (106%) or above - (flashing light and warning gong)
-Audio signal at (110%) or above - flashing light and high-pitched steady tone)

Procedure:
1. Rotor RPM indicator - Check
2. Collective Lever - adjust as necessary to maintain Nro within normal range

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Autorotation

A

CADB

  1. Collective Lever - reduce to maintain Nro within limits
  2. Airspeed - 75 KIAS recommended
  3. Double engine emer s/d - Perform
  4. BAT MSTR sw - OFF
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Autorotation EP Additional Details

A

Maximum range airspeed - 90 KIAS
Minimum rate of descent airspeed - 60 KIAS
At approximately (100 ft) AGL:
4. Flare attitude - 15-20 degrees
AT APPROXIMATELY (8-12 ft AGL):
5. Flare attitude - reduce to approx 7 deg
6. Heading - maintain
7. Collective lever - raise as necessary to stop descent and cushion landing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Caution Indications - GEN OVHT (1 or 2)

A
  1. Affected GEN sw - OFF
    CAUTION if GEN OVHT remains (ON) and there are indications of a fire such as burning (ODOR) or (SMOKE, SHUT DOWN AFFECTED ENGINE)
    (if GEN OVHT remains on for more than (1 min):
  2. OEI flight conditions - establish
  3. Affected engine - ID
  4. Single engine emer s/d - perform
  5. Land as soon as PRACTICABLE
17
Q

Compressor Stall

A

Indications:
- (popping) sounds
- torque and N1 indication may (decrease)
-TOT may (increase)
-slight yaw (jerk)

Procedure:
1. Collective lever - lower
2. Engine instruments - monitor
3. Collective lever - raise slowly
(if compressor stall returns)
4. Affected engine - ID (TOT)
5. Single engine emer s/d - Perform
6. Land as soon as PRACTICABLE

18
Q

Single Engine Failure - Hover OGE - Forced Landing

A

CALCAS

  1. Collective lever - adjust to maintain rotor RPM
  2. Airspeed - increase if possible
  3. Landing attitude - establish
  4. Collective lever - raise as necessary to stop descent and cushion landing
  5. Affected engine - ID
  6. Single engine emer s/d - perform
19
Q

Single Engine Failure - Hover OGE - Flyaway

A

CAC RAC ASL

  1. Collective lever - adjust to maintain rotor RPM
  2. Airspeed - increase if possible
  3. Collective lever - adjust to OEI limits or below
  4. Rotor speed - trim to max
  5. Airspeed - gain, 65 KIAS
  6. Collective lever - reduce to OEI MCP or below
  7. Affected engine - ID
  8. Single engine emer s/d - perform
  9. Land as soon as PRACTICABLE
20
Q

ENGINE OVERSPEED

A

CVNATL

  1. Collective lever - raise as necessary to maintain N2 and Nro within limits
  2. VARTOMS - check MAN mode
  3. N2 trim sw - try to trim Nro to 101 with matched torque
  4. Affected engine - ID
  5. Twist grip (affected engine) - rotate towards idle until N2 and Nro stabilize in normal operating range and FLI needles match
  6. Land as soon as PRACTICABLE
21
Q

ENGINE UNDERSPEED

A

OBVANTLS

  1. OEI flight conditions - establish
  2. Bleed air consumers - OFF
  3. VARTOMS - check MAN mode
  4. Affected engine - ID
  5. N2 trim sw - compensate for drop in N2 and Nro with matched torque
  6. Twist grip (affected engine) - raise stop plate, rotate towards flight until N2 and Nro stabilize in normal range and FLI needles match
  7. Land as soon as PRACTICABLE
  8. Single engine emer s/d - perform
22
Q

Tail Rotor Drive Failure - flight

A

CASSALAAA

  1. Collective lever - reduce to obtain minimum sideslip angle
  2. Airspeed - maintain 70 KIAS or higher
  3. Suitable landing area - select
  4. Shallow approach with nose left - perform
  5. Airspeed - reduce close to the ground until nose is aligned with the flight direction
  6. Landing - perform

(if nose direction chances from left to right above 40 kts):
5. Airspeed - increase
6. Approach - abort, climb to sufficient height for autorotation
7. Autorotation - perform

23
Q

Tail Rotor Drive Failure - Hover

A
  1. Both twist grips - Rotate to idle
  2. Landing attitude - Establish
  3. Collective lever - apply as necessary
  4. Double engine emer s/d - Perform
24
Q

Fire (on the ground)

A

F BB CD BB

  1. Fire sw (affected eng) - raise guard, press
  2. Both Fuel Pump Prime sw - check OFF
  3. BOT1/BOT2 pb - press; BOT1 activated, EXT indicator light comes on (emer off sw pnl)
  4. Clock stopwatch - start when BOT1 legend and EXT indicator light go off (emer off sw pnl)
  5. Double eng emer s/d - Perform
    (if fire still on after 1 min)
  6. BOT1/BOT2 pb - press; BOT2 activated, EXT indicator light comes on (emer off sw pnl)
  7. BAT MSTR sw - OFF
25
Q

XMSN oil temp

A
  1. XMSN oil temp and oil pressure indication - Check
    (if indications are in limits)
  2. Land as soon as PRACTICABLE
    (if indications are above limits)
  3. Power - reduce as much as possible
    (if indications remain above limits)
  4. Land as soon as POSSIBLE