B3 EP's Flashcards

1
Q

MGB CHIP LIGHT

A
  1. Power - Reduce
  2. Land as soon as possible
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2
Q

YAW SERVO SLIDE VALVE SEIZURE
(In flight)

A
  1. Airspeed - Adjust (40-60 KIAS)
  2. Hydraulic Pressure Switch - Off
  3. Land as soon as possible - Shallow approach/run-on landing

After landing

  1. Collective - Lock
  2. Engine shutdown
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3
Q

NG INDICATOR FAILURE

A
  1. Torque - Do not exceed maximum authorized value
  2. T4 - <810 °
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4
Q

LOW ENGINE OIL PRESSURE (GAUGE)

A
  1. WARN/FIRE Test - Check ENG P light

If ENG P light is off when tested:

  1. Autorotate/Engine Shutdown

If ENG P light is on when tested:

  1. Land as soon as possible
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5
Q

MAIN SERVO-CONTROL SLIDE VALVE SEIZURE

A
  1. Hydraulic Pressure Switch - Off
  2. Airspeed - Adjust (40-60 KIAS)
  3. Land as soon as possible - shallow approach/run-on landing

After landing

  1. Collective - lock
  2. Engine Shutdown - complete
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6
Q

NR RPM INDICATOR FAILURE

A
  1. Torque - Maintain above 10%
  2. Nf - monitor
  3. Land as soon as possible
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7
Q

VEMD DUAL SCREEN FAILURE

A
  1. Power - adjust (100 KIAS max)
    Land without hovering
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8
Q

TAIL ROTOR DRIVE FAILURE
(Hover OGE)

A
  1. Collective - reduce (as required)
  2. Airspeed - increase
  3. Land as soon as possible
  4. Autorotate/engine shutdown - Min touchdown speed
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9
Q

HIGH ENGINE OIL TEMPERATURE

A

Inflight or hover
1. Land as soon as possible

If landing is not possible

  1. Airspeed - 80 KIAS

If temperature decreases below the redline:

  1. Land as soon as practicable

If temperature remains above the redline:

  1. Land as soon as possible
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10
Q

YAW SERVO SLIDE VALVE SEIZURE
(Hover)

A

If yaw control is maintained:

  1. Land as soon as possible

If yaw control is not maintained:

  1. Hydraulic pressure switch (collective) - off
  2. Land as soon as possible

After landing:

  1. Collective - lock
  2. Engine Shutdown - complete
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11
Q

TORQUE METER FAILURE

A

Ng - maximum continuous -4

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12
Q

VEMD SINGLE SCREEN FAILURE

A
  1. Failed screen - off
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13
Q

TAIL ROTOR CONTROL FAILURE
(FIXED PITCH)

A
  1. Airspeed - set 70 KIAS/level flight
  2. HYD test - engage (5 sec)
  3. Land as soon as practicable - shallow approach/run-on landing
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14
Q

LAND IMMEDIATELY

LAND AS SOON AS POSSIBLE

LAND AS SOON AS PRACTICABLE

A
  1. Land immediately
  2. Landing at the nearest landing site at which a safe landing can be made.
  3. Continued flight is not recommended. Landing site and duration of flight are at the discretion of the pilot in command.
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15
Q

TAIL ROTOR DRIVE FAILURE
(In flight)

A
  1. Collective - reduce (as required)
  2. Airspeed - adjust (to minimize left yaw)
  3. Land as soon as possible
  4. Autorotate/engine shutdown - min touchdown speed
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16
Q

ENGINE FAILURE
(Cruise)

A
  1. Autorotate - airspeed (65 knots)
  2. Starting selector - off

Attempt restart when Ng is below 5%

  1. Fuel Pump - on
  2. GOV (Red and Amber) Lights - out
  3. Starting selector - FLT
  4. Fuel pump - off

If no restart

  1. Fuel shut-off - close
  2. Generator - off
  3. Master Cutoff (if there is a burning smell) - off
17
Q

MGB P LIGHT

A
  1. Power - reduce
  2. Land as soon as possible
18
Q

ENGINE FIRE
(In Flight)

A
  1. Autorotate - airspeed 65 KIAS
  2. Fuel shut-off - close
  3. Generator - off
  4. Master Cutoff (if there is a burning smell) - off
19
Q

ENGINE FIRE
(During start)

A
  1. Starting selector - off
  2. Fuel shut-off - close
  3. Rotor Brake (as necessary) - engage
  4. Fuel pump - off
  5. Crank switch - engage (for 10 sec)
  6. Master switch - off
  7. Fire Extinguisher - as required
20
Q

HYDRAULIC LIGHT
(In Flight)

A
  1. Airspeed - adjust (40-60 KIAS)
  2. Hydraulic pressure switch - off
  3. Land as soon as possible - shallow approach/run-on landing
21
Q

FUEL LIGHT

A
  1. Avoid large attitude changes
  2. Land as soon as practicable
22
Q

DOOR LIGHT

A
  1. Airspeed - 120 KIAS maximum
23
Q

ENG P LIGHT

A
  1. Power - reduce

If engine oil pressure is low or zero:

  1. Autorotate/engine shutdown

If engine oil pressure is normal:

  1. Land as soon as possible
24
Q

TGB CHIP LIGHT

A
  1. Land as soon as possible
25
Q

GOV LIGHT
(Amber/steady)

A
  1. Avoid abrupt power variations
  2. Land as soon as practicable
26
Q

GEN LIGHT

A
  1. Reset - attempt
  2. If reset unsuccessful - shed unessential electrical equipment
  3. Land as soon as practicable
27
Q

FUEL FILTER LIGHT
(Either)

A
  1. Power - reduce
  2. Land as soon as possible
28
Q

GOV LIGHT (RED)

A
  1. Collective lever twist grip - maintain Nr in green arc
  2. Land as soon as practicable - approach at 40 KIAS

Note - after touchdown, reduce fuel flow before lowering collective lever

29
Q

ENG CHIP LIGHT

A
  1. Land as soon as possible
30
Q

MGB T LIGHT

A
  1. Power - reduce
  2. Land as soon as possible
31
Q

FUEL P LIGHT

A
  1. Power - reduce
  2. Fuel pump on - on
  3. Land as soon as possible
32
Q

TAIL ROTOR DRIVE FAILURE
(Hover IGE)

A
  1. Twist grip - idle
  2. Land - maintain level attitude