EPs Flashcards

1
Q

For every abnormal/emergency condition

A

Control the aircraft

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2
Q

Land Immediately

A

Land without delay. Pilots are to bear in mind that consequences of continued flight are likely to be more hazardous than, for example, ditching (even in adverse conditions) or landing in trees.

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3
Q

Land as Soon as Possible

A

Land at the nearest suitable site where a safe landing can be made.

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4
Q

Land as Soon as Practicable

A

Means extended flight is not recommended. The landing site and duration of flight is at the discretion of the pilot.

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5
Q

A/R As Required

A

A determination made by pilots if the situation justifies this action

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6
Q

Over Water Flight

A

Emergencies over water, “LAND AS SOON AS POSSIBLE” is at the discretion of the PIC based on the situation

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7
Q

Emergency Transponder Codes

A

7700- Distress
7600- Lost Comms
7500- Hijacking

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8
Q

Normal Airspeeds

A

Vtoss - 35 kts
Vy - 0 degree yaw - 65 kts
- 10 degree yaw - 60 kts

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9
Q

Auto-rotational Speeds

A

Below 2600’ DA (NR 100-106%) - 65 kts 106%*

Above 2600’ DA (NR 100-106%) - 80 kts 100%*

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10
Q

Engine Failure OGE Hover Best Landing Airspeed

A

30 kts best for cushioning

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11
Q

Water Entry Speed (Maximum)

A

30 kts

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12
Q

Running Landing Speed (Maximum)

A

Power Off - 40 kts

Power On - 60 kts

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13
Q

Single Engine Final Approach Speed (For Min Ground Run)

A

Below 2600’ DA - 30 kts

Above 2,600’ DA - 40 kts

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13
Q

SAS Failures (Maximum Speed)

A

Single SAS Failure VFR - 110 kts

Dual SAS Failure VFR - 100 kts

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15
Q
  1. Emergency Aircraft Shutdown
A
  1. ECLs (Both) - STOP
  2. Fire T-Handles (Both) - PULL
  3. Rotor Brake - ARMED/ENGAGE
  4. Master Switch - OFF
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16
Q
  1. Emergency Descent/Landing
A
  1. COLLECTIVE - LOWER TO MAINTAIN Nr
  2. Airspeed - 120 kts or VNE
  3. Bank Angle - UP TO 30 DEGREES
    After Landing:
  4. Emergency Aircraft Shutdown (Proc. 1) - A/R
17
Q
  1. Emergency Evacuation
A
  1. Emergency Aircraft Shutdown (Proc. 1 - PERFORM
  2. Emergency Exits - OPEN
  3. Aircraft - EVACUATE FROM NEAREST EXIT
18
Q
  1. Engine Post-Shutdown Fire
A

Indicated by a rapid rise in TIT above 250 C

  1. *ECLs(Both) - CONFIRM/STOP
  2. Ignition Switch - OFF
  3. Start Button(Affected Engine) - CONFIRM/MOTOR (Until TIT is below 100 C)
  4. Fire T-Handle(Affected Engine) - CONFIRM/PULL
19
Q
  1. Engine Fire (Lighted Fire Handle)
A
  1. Engine Fire - CONFIRM
  2. ECL(Affected Engine) - CONFIRM/STOP
  3. Fire Handle - CONFIRM/PULL
  4. Emergency Descent(Proc. 2) - PERFORM
    If Fire Persists
    1. Agent Discharge Switch - UNUSED BOTTLE
19
Q
  1. Cabin Area/Cockpit Fire - In Flight
A
  1. Emergency Aircraft Shutdown(Proc. 1) - PERFORM
  2. Fire Extinguisher - A/R
  3. Emergency Evacuation(Proc. 3) - A/R
19
Q
  1. Cabin Area/Cockpit Fire - In Flight
A
  1. Emergency Descent(Proc. 2) - PERFORM
  2. Land - AS SOON AS POSSIBLE
  3. Fire Extinguisher - A/R
20
Q
  1. Heater Fire T-Handle Warning Light ON
A
  1. Heater Switch - OFF
  2. Heater Fire T-Handle - PULL
    If Fire Persists
    1. Agent Discharge Switch - BOT 1
21
Q
  1. Electrical Fire Known Source
A
  1. System Switch or Circuit Breaker - OFF/PULL
22
Q
  1. Single-Engine Failure
A
  1. Collective - ADJUST TO MAINTAIN 94% Nr
  2. Airspeed - ADJUST
  3. Engine Beeps - BOTH MAX
  4. Parking Braking - DISENGAGED
23
Q
  1. NO. 1 or NO. 2 ENG OIL PRESS Caution Light
A

Confirm related engine oil pressure below 20 PSIG

Checklist

24
Q
  1. Imminent Transmission Failure
A
  1. Collective - MIN POWER (DO NOT Autorotate)
  2. Airspeed - 65 kts
  3. Control Inputs - MINIMIZE
  4. Land - IMMEDIATELY
25
Q
  1. Nf Overrunning Nr (Sprag Clutch Failure)
A
  1. ECL(Affected Engine) - CONFIRM/STOP
    When Ng reaches zero (0)
  2. ECL(Engaged Engine) - CONFIRM/STOP
26
Q
  1. Aircraft Control Erratic
A
  1. Control Inputs - MINIMIZE
  2. Collective Pitch - REDUCE
    If control remains erratic
    1. SAS Selector Switch - OFF
      If control remains erratic with SAS off
    2. External Load - PUT ON THE GROUND OR JETTISON
27
Q
  1. Ground Resonance
A
  1. *Collective - Become Airborne

Or

  1. *Collective - Full Down
  2. *ECLs - Stop
28
Q
  1. HYD BOOST FAIL Caution Light
A
  1. Cockpit And Companionway Gauges - CHECK
    Any pressure fluctuation in the second system
  2. Emergency Descent(Proc. 2) - PERFORM
  3. Land - IMMEDIATELY
29
Q
  1. Dual-Engine Failure
A

Hover
1. Collective - ADJUST TO CUSHION LANDING
Flight
1. Collective - PERFORM

30
Q
  1. CHIP DETECTOR Caution Light
A
  1. Secondary Indications - CHECK
    Indications confirmed
  2. Imminent Transmission Failure(Proc. 32) - PERFORM
31
Q
  1. XMSN OIL TEMP Caution Light
A

Caution light indicates oil temp in either sump has exceeded 115 C

  1. Secondary Indications - CHECK
  2. Imminent Transmission Failure(Proc. 32) - PERFORM
32
Q
  1. Emergency Engine Shutdown
A
  1. ECL(Affected Engine) - CONFIRM/STOP
  2. Fire T-Handle(Affected Engine) - CONFIRM/STOP
  3. Fuel Boost Pump(Affected Engine) - CONFIRM/OFF