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Check Rides & Exams > Primary 1 > Flashcards

Primary 1 Flashcards

1
Q

TOT Limits (FLI, Temp, Time)

A

FLI Temp Time
Max TOT Starting 8.5 785C -
Starting Transient 11 865 5s

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2
Q

AEO Limits (FLI, Torque, Time)

A

FLI TQ Time
T/O Power Range 8.5-10 71-88% 5min
Max T/O Power 10 88% 5min
Transient 10.5 97% 12s

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3
Q

OEI Limits (FLI, Torque, Time)

A

FLI Torque Time
OEI MCP 11 91.5% -
2.5min Power 12 125% 2.5min
OEI Transient 14 140% 12s

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4
Q

Engine Starter Time Limits Battery & EPU

A

Battery: 30s - 60s - 30s - 60s - 30s - 30min
EPU: 20s - 60s - 20s - 60s - 20s - 30min

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5
Q

Engine Ventilation Time Limits Battery & EPU

A

Battery: 20s - 60s - 20s - 23min
EPU: 15s - 60s - 15s - 23min

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6
Q

Engine Oil Pressure

A

Caution: 1.3 - 1.5 bar
Continuous: 1.5 - 5 bar

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7
Q

Engine Oil min. power application & max. temperature limits

A

3 cSt & 3.9 cSt: -10 C
5 cSt: 0 C
Max: 115 C

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8
Q

Main transmission oil pressure

A

Caution range: 1 - 1.5 bar
Continuous: 1.5 - 5 bar

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9
Q

Main transmission oil temperature continuous operation & max

A

Continuous: -10 C - 105 C
Maximum: 105 C

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10
Q

Rotor RPM Conditions & Indications

A

NRO =< 95%: steady light & low pitch beeping

NRO >= 106%: flashing light & warning gong
NRO >= 110%: flashing light & steady high pitch tone

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11
Q

Land immediately/ ASAP/ as practicable

A

The urgency of landing is paramount. Primary consideration is to assure survival of the occupants. Landing in water, trees or other unsafe areas should be considered only as last resort.

Land without delay at the nearest adequate site at which a safe approach and landing can be made.

The landing site and duration of flight are at the discretion of the pilot. Extended flight beyond the nearest approved landing area where appropriate assistance can be expected is not recommended.

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12
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 max
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13
Q

Double Engine Emergency Shutdown

A

On Ground
1. Both Twist grips - OFF
2. Both fuel pump prime sw - OFF
3. BAT MSTR sw - OFF

In Flight
1. Both Twist grips - OFF
If there is an indication that engines are still running:
2. Both EMER OFF sw - Press

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14
Q

Autorotation

A
  1. Collective - Lower to maintain NRO within limits
  2. Airspeed - 75 KIAS recommended
  3. Double Engine Emergency Shutdown - Perform
  4. BAT MSTR sw - OFF
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15
Q

Fire (ENG 1 or ENG 2)

A
  1. OEI flight condition - Establish
  2. Airspeed - Reduce if >100 KIAS
  3. Fire sw (affected engine) - Raise guard, press
  4. BOT 1/BOT 2 pb - Press, bottle 1 activates, EXT indicator light comes on (EMER OFF sw pln)
  5. Stopwatch - Start (after BOT 1 & EXT indication has come off (EMER OFF sw pnl))
  6. Affected engine - Identify
  7. Single Engine Emergency Shutdown - Perform
  8. Land as soon as possible

If Fire warning still on after 1min:
9. BOT 1/BOT 2 pb - Press, bottle 2 activates, EXT indicator light comes on (EMER OFF sw pnl)

If Fire warning remains on:
10. Land immediately

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16
Q

ENG CHIP (System 1 or 2)

A

On Ground
1. Affected engine - Identify
2. Single Engine Emergency Shutdown - Perform

In Flight
1. OEI flight condition - Establish
2. Affected engine - Identify
1. Alternative:
3. Single Engine Emergency Shutdown - Perform
2. Alternative:
3. Twist grip (affected engine) - Rotate slowly to IDLE, check indications
4. Land as soon as practicable

17
Q

ENG Oil P (System 1 or 2)

A
  1. Engine oil pressure - Check
  2. OEI flight condition - Establish
  3. Affected engine - Identify
  4. Single Engine Emergency Shutdown- Perform
  5. Land as soon as practicable
18
Q

Engine oil temperature high

A
  1. OEI flight condition - Establish
  2. Affected engine - Identify
  3. Twist grip (affected engine) - Adjust to 20-30% torque (TWIST GRIP caution comes on)
  4. Oil temperature indicator (affected engine) - Monitor

If engine temperature decreases below limit;
5. Land as soon as practicable

If engine temperature still remains above limits:
6. Single Engine Emergency Shutdown - Perform
7. Land as soon as practicable

19
Q

Single engine failure - takeoff

A
  1. Collective lever - Adjust to maintain NRO

Rejected takeoff:
2. Landing attitude - Establish
3. Collective lever - Raise as necessary to stop descent and cushion landing
After landing:
4. Affected engine: Identify
5. Single Engine Emergency Shutdown - 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
After reaching safe altitude:
5. Collective lever - Reduce to OEI MCP or below
6. Affected engine - Identify
7. Single Engine Emergency Shutdown - Perform
8. Land as soon as practicable

20
Q

XMSN OIL PRESS

A

If one XMSN oil pressure indication below 1 bar:
1. Power - Reduce
2. Land as soon as practicable

If both indications below 1 bar:
3. Land immediately

21
Q

XMSN OIL TEMP

A
  1. XMSN oil temperature and pressure indication - Check

If indications are within limits:
2. Land as soon as practicable

If indications are above limit:
2. Power - Reduce as much as possible

If oil temperature indication remains above limit:
3. Land as soon as possible

22
Q

Single engine failure - hover IGE

A
  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
    After landing:
  4. Affected engine - Identify
  5. Single Engine Emergency Shutdown - Perform
23
Q

Single engine failure - flight

A
  1. OEI flight condition - Establish
  2. Rotor speed - Trim to max
  3. Affected engine - Identify
  4. Single Engine Emergency Shutdown - Perform
  5. Land as soon as practicable
24
Q

GEN OVHT (System 1 or 2)

A
  1. Affected GEN sw - OFF

If GEN OVHT caution indication remains on for more than 1 min (or burning odor/smoke):
2. OEI flight condition - Establish
3. Affected engine - Identify
4. Single Engine Emergency Shutdown - Perform
5. Land as soon as practicable

25
Q

Compressor stall

A
  1. Collective lever - Lower
  2. Engine instruments - Monitor
  3. Collective lever - Raise slowly

If compressor stall returns:
4. Affected engine - Identify
5. Single Engine Emergency Shutdown - Perform

  1. Land as soon as practicable
26
Q

Single engine failure - hover OGE

A
  1. Collective lever - Adjust as necessary to maintain NRO
  2. Airspeed - Increase if possible

Forced landing:
3. Landing attitude - Establish
4. Collective lever - Raise as necessary to stop descent and cushion landing
After landing:
5. Affected engine - Identify
6. Single Engine Emergency Shutdown - Perform

Transition to OEI - flight
3. Collective lever - Reduce to OEI limits or below
4. Rotor speed - Trim to max
5. Airspeed - Gain 65 KIAS
After reaching safe altitude:
6. Collective lever - Reduce to OEI MCP or below
7. Affected engine - Identify
8. Single Engine Emergency Shutdown - Perform
9. Land as soon as practicable

27
Q

ENGINE OVERSPEED - GOVERNOR FAILURE

A
  1. Collective lever - Raise as necessary to maintain N2 and NRO within limits
  2. VAR NR System NORM/MAN sw - Check MAN
  3. N2 TRIM sw - Try to trim NRO to 101% with matched torque
    If step 3 is not possible:
    4. Affected engine - Identify
    5. Twist grip (affected engine) - Rotate towards IDLE until N2 and NRO stabilize in normal range and FLI needles match
    6. Land as soon as practicable
28
Q

ENGINE UNDERSPEED - GOVERNOR FAILURE

A
  1. OEI flight condition - Establish
  2. Bleed air consumers - Off
  3. VAR NAR System NORM/MAN pb - Check MAN
  4. Affected engine - Identify
  5. N2 TRIM sw - Compensate N2/NRO drop and try to match torque
    If torque match is not possible:
    6. Twist grip (affected engine) - Release stop plate and rotate towards Flight until N2 and NRO stabilize in normal range and FLI needles match
  6. Land as soon as practicable
    If no residual torque (affected engine) is available
  7. Single engine emergency shutdown- Perform
29
Q

Tail Rotor Drive Failure/Fixed-pitch - Fwd Flight

A
  1. Collective Lever - Reduce to obtain minimum sideslip angle
  2. Airspeed - Maintain 70 KIAS or higher
  3. Shallow approach with nose left - Perform
    If airspeed can be reduced below 40 kts with nose pointing to the left:
  4. Airspeed - Reduce close to the ground until nose is aligned with the flight direction
  5. Landing - Perform

If the nose direction changes to right at airspeed > 40 kts:
5. Airspeed - Increase
6. Approach - Abort, climb to sufficient height for autorotation
7. Autorotation - Perform

30
Q

Low Fuel (Sys 1/2)

A

Fuel quantity indication - Check
If positive fuel in the main tank:
Both FUEL XFER sw (Aft & Fwd) - Check ON
Both FUEL XFER circuit breakers - Check IN

If both Fuel warning lights remain on:
Land within 10 min

In one remains on:
Expect single engine failure

31
Q

BAT Temp

A

On Ground
BAT MSTR sw - OFF

In Flight
BAT MSTR sw - OFF
Land as soon as possible

32
Q
A
33
Q

Max Gross Weight

A

3585 kg
7903 lbs

Check Rides & Exams (10 decks)

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