B412 Immediate Actions Flashcards

1
Q

ENGINE FIRE DURING START

A
  1. Throttles …………BOTH TO IDLE/SHUT OFF/CONFIRM FIRE
  2. T Handle (affected engine)………………………….IDENTIFY/PULL
  3. Fire ………………………………….. IF FIRE PERSISTS – FIRE MAIN
    If Fire persists for more than 10 seconds:
  4. Fire Ext ……………………………………………….FIRE RESERVE
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2
Q

ENGINE FIRE DURING TAKEOFF OR APPROACH

A
  1. Land if a suitable area is available
  2. Collective ……… LOWER AS ALTITUDE PERMITS, BELOW OEI
  3. Airspeed …………………………………………… 45 KT MINIMUM
  4. Throttle …………………….. IDENTIFY/IDLE/CHECK FOR FIRE
    IF FIRE CONFIRMED OR DOUBT EXISTS – CLOSED
  5. T Handle ………………………………………………………..IDENTIFY/PULL
  6. Fire Ext ……………………………………………………………FIRE MAIN
    If Fire persists for more than 10 seconds:
    Fire Ext ………………………………………………………… FIRE RESERVE
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3
Q

ENGINE FIRE IN FLIGHT

A
  1. Collective ……………………… LOWER TO OEI POWER
  2. Throttle …………………………… IDENTIFY/IDLE/CHECK FOR FIRE
    If Fire confirmed or Doubt Exists:………. THROTTLE CLOSED
  3. T Handle (affected engine) ……………………. IDENTIFY/PULL
  4. Fire Ext ………………..FIRE MAIN/CHECK FOR SIGNS OF FIRE
    If Fire persists for more than 10 seconds:
  5. Fire Ext ……………………………………………….. FIRE RESERVE
  6. N2 RPM …………………………………………………..BEEP to 100%
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4
Q

HOT START/SHUTDOWN

A

Abort Start

  1. Throttle ………………………………………………………… CLOSED
  2. Starter …… MAINTAIN ENERGISED UNTIL ITT BELOW 150°C
  3. Fuel Switch (affected engine) …………………….. IDENTIFY/OFF
  4. Boost Pump …………………………………………………………. OFF
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5
Q

BAGGAGE COMPARTMENT FIRE

A
  1. Power ………………………… REDUCE TO MINIMUM REQUIRED
  2. LAND AS SOON AS POSSIBLE
    Check for signs of fire/smoke, if confirmed or doubt exists:
  3. LAND IMMEDIATELY
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6
Q

SMOKE AND FUME ELIMINATION

A
  1. Vent Blower Switch ……………………………………….. ON
  2. Vents/Windows …………………………………………… OPEN
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7
Q

ELECTRICAL FIRE IN FLIGHT

A
  1. IAS …………….REDUCE SPEED IF REQUIRED TO OPEN DOOR
  2. Cockpit Windows ………………………………………………….OPEN
  3. Passengers …………………………………………………………….. BRIEF
  4. Electrical Systems ……………….. BEGIN SWITCHING OFF POSSIBLE SOURCES OF CURRENT DRAIN
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8
Q

ENGINE FAILURE IN HOVER

A
  1. Collective ……….. FREEZE/LOWER TO MINIMISE NR DECAY
  2. Cyclic/Pedals ……………………… CORRECT DRIFT AND YAW
  3. Collective …………. AS REQUIRED TO CUSHION LANDING
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9
Q

ENGINE FAILURE DURING TAKE-OFF BEFORE

‘COMMITTED’/’FLY AWAY’ POINT (OR ON APPROACH AFTER ‘COMMITTED’)

A
  1. Collective …………………………….. ADJUST TO CONTAIN NR
  2. Cyclic …………….. FLARE TO REDUCE GROUND SPEED
  3. Collective . USE AS NECESSARY TO CUSHION LANDING
    THEN LOWER SMOOTHLY
  4. Cyclic/Pedals … CORRECT DRIFT/YAW BEFORE TOUCHDOWN
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10
Q

ENGINE FAILURE DURING TAKE-OFF AFTER ‘COMMITTED/FLY

AWAY’ (OR ON APPROACH BEFORE ‘COMMITTED’)

A
  1. Collective ………………………… ADJUST TO CONTAIN NR ABOVE 97% WITHIN OEI LIMITS NR BEEP TO 100%
  2. Cyclic ………………… SELECT ATTITUDE TO ACHIEVE VTOSS (45 KT) UNTIL CLEAR OF OBSTACLES
  3. Cyclic …………….ACCELERATE TO VY, CLIMB AT VY (70 KT)
  4. NFP/AC……………… CALL NR TRENDS UNTIL SAFE FLIGHT
    MONITOR REMAINING ENGINE WITHIN OEI LIMITS
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11
Q

ENGINE FAILURE IN THE CRUISE

A
  1. Collective …. ADJUST TO CONTAIN NR AT OR ABOVE 97%
  2. IAS ………………………………….. ADJUST IF NECESSARY
    TO MAINTAIN VY (70 KT) OR ABOVE
  3. RPM Switch …………………………………………….. BEEP TO 100%
  4. Remaining Engine ..CONFIRM OPERATION WITHIN LIMITS
  5. NFP/AC ………………. CALL NR TRENDS UNTIL SAFE FLIGHT
    MONITOR REMAINING ENGINE WITHIN OEI LIMITS
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12
Q

DUAL ENGINE FAILURE

A
  1. Collective … LOWER TO ACHIEVE AUTOROTATIVE DESCENT
  2. Airspeed ………… ESTABLISH MIN ROD AIRSPEED 65-70 KT OR RANGE AIRSPEED (90 KT)
  3. Passengers …………………………………………. BRIEF/BRACE
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13
Q

ENGINE LOW OIL PRESSURE

ENGINE OIL TEMPERATURE HIGH

A
  1. Collective ………… LOWER TO WITHIN OEI POWER LIMITS
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14
Q

ENGINE CHIP

A
  1. Collective ……….. LOWER TO WITHIN OEI POWER LIMITS

2. Safe Flight …… ENSURE PRIOR TO ENGINE SHUTDOWN

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15
Q

HIGH SIDE FAILURE

LOW SIDE FAILURE

A
Torque Split
Rotor High/Lo (Contain NR)
Identify Engine
Confirm Engine with ITT/N1
Select Engine and Select Idle
GOV to Manual
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16
Q

MAIN DRIVE SHAFT FAILURE

A
  1. Collective …………………………….. ENTER AUTOROTATION
  2. Airspeed ………. 65-70 KT (MIN ROD) OR 90 KT (RANGE)
  3. Throttles ………………………………………………… BOTH CLOSED
17
Q

TRANSMISSION OIL PRESSURE
TRANSMISSION OIL TEMPERATURE
COMBINING GEAR BOX LOW OIL PRESSURE OR HIGH
TEMPERATURE

A
  1. Collective ………… REDUCE TO MINIMUM POWER REQUIRED

2. Confirm ………….. CHECK Respective Gauge

18
Q

TRANSMISSION OR COMBINING GEAR BOX CHIP

A
  1. Collective ……. REDUCE TO MINIMUM POWER REQUIRED
  2. IAS ……………………….. CONSIDER REDUCING IAS TO 70 KT
  3. LAND AS SOON AS PRACTICAL
19
Q

ROTOR BRAKE WARNING LIGHT

A
  1. Rotor Brake Handle ……………………….CHECK DETENT
    If rotor brake is in the detent and light illuminated:
  2. LAND AS SOON AS POSSIBLE
20
Q

LOSS OF TAIL ROTOR THRUST AT HOVER

A
  1. Throttles ……………………………………………………………. CLOSED
  2. Attitude …………………………………………………………………. LEVEL
  3. Groundspeed ………………………………………………………….. ZERO
  4. Collective ………….. INCREASE TO CUSHION LANDINGS
21
Q

LOSS OF TAIL ROTOR THRUST IN FORWARD FLIGHT

A
  1. Throttles …………………………………….. CLOSED FLIGHT IDLE
    WARNING
    Do not allow rotor rpm to decay below minimum limits
  2. Collective ………………………… ENTER AUTOROTATION
  3. Airspeed ……………………………………………………………… 70 KT
22
Q

HYDRAULIC SYSTEM FAILURE

A
  1. Confirm Failure ……… VERIFY WITH GAUGE INDICATIONS
23
Q

AFCS FAILURE TO ENGAGE OR DISENGAGES

A
  1. IAS …………………………….. REDUCE TO 115 KT OR LESS
24
Q

HARDOVER OR ABNORMAL CONTROL DISTURBANCE

AUTOTRIM RUNAWAY

A
  1. Cyclic …… MANUALLY CONTROL THE AIRCRAFT ATTITUDE
  2. Cyclic Trim Release ….. PRESS FORCE TRIM RELEASE AND HOLD
  3. Airspeed ………………………………. REDUCE TO BELOW 115 KT
25
Q

DOUBLE AC INVERTER FAILURE

A
  1. Standby AI ……………….. FLY WITH REFERENCE TO STBY AI
    AND STBY COMPASS
26
Q

DC GENERATOR OVERHEAT LIGHT

A
  1. DC GEN Switch ……………………………………………………….OFF
27
Q

DOUBLE FUEL BOOST PUMP FAILURE

A
  1. Fuel Boost Pump Switches ……………….CHECK BOTH ON
28
Q

CABIN HEATER MALFUNCTION

A
  1. Heater Switch ………………………………………………SELECT OFF