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CAE C90 > Emergency Ops - Recall Items > Flashcards

Emergency Ops - Recall Items Flashcards

1
Q

EMERGENCY ENGINE SHUTDOWN

A
  1. Condition Lever . . . . . . . . . .FUEL CUTOFF
  2. Propeller Lever . . . . . . . . . . FEATHER
  3. Fuel FW Shutoff Valve . . . . .CLOSE
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2
Q

ENGINE FIRE ON GROUND

A

Affected Engine:
1. Condition Lever. . . . . . . . . . . . FUEL CUTOFF
2. Fuel FW Shutoff Valve . . . . . . .CLOSE
3. Ignition and Engine Start . . . . STARTER ONLY

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3
Q

ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1)

Sufficient RWY Remaining

A
  1. Power Levers . . . . . . . . . . . . . . . GROUND FINE
  2. Brakes . . . . . . . . . . . . . . . . . . . . . MAXIMUM
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4
Q

ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1)

If Insufficient Runway Remains for Stopping:

A
  1. Condition Levers . . . . . . . . . . .FUEL CUTOFF
  2. Fuel FW Shutoff Valve . . . . . . .CLOSE
  3. Master Switch . . . . . . . . . . . . . OFF (Gang Bar down)
  4. Boost Pumps . . . . . . . . . . . . . .OFF
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5
Q

ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1)

A
  1. V1 Speed . . . . . . . . . . . .ROTATE TO APROX 10°
  2. Landing Gear (Positive climb estab) . .UP
  3. Propeller (Inoperative Engine) . VERIFY FEATHERED
  4. Power . . . . . . . . . . . . . . . . . . . . . . MAX ALLOWABLE
  5. Airspeed . . . . . . . . .MAINTAIN V2 SPEED OR ABOVE UNTIL 400 FEET
    THEN ACCELERATE TO 106 KNOTS
  6. Flaps (At 400 feet & 106 Knots - minimum) . . . UP

V2 99 KIAS STD

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6
Q

ENGINE FAILURE IN FLIGHT
BELOW (VMCA)

A
  1. Power . . . . . . . . . . . . .REDUCE
  2. Nose . . . . . . . . . . . . . . LOWER TO ACCELERATE ABOVE VMCA
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7
Q

2ND ENGINE FLAMEOUT

A
  1. Power Lever . . . . . . . . . . .IDLE
  2. Propeller . . . . . . . . . . . . . .DO NOT FEATHER
  3. Condition Lever . . . . . . . .FUEL CUTOFF
  4. Conduct Air Start Procedures in Section 3A, Abnormal Procedures.

The propeller will not unfeather without engine operating.

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8
Q

ELECTRICAL SMOKE OR FIRE

A
  1. Oxygen Mask(s) . . . . . . . . . .DON
  2. Mask Selector Switch . . . . .EMER Position
  3. Mic Switch(es) . . . . . . . . . . . OXY
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9
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A
  1. Oxygen Mask(s) . . . . . . . . . .DON
  2. Mask Selector Switch . . . . .EMER Position
  3. Mic Switch(es) . . . . . . . . . . . OXY
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10
Q

EMERGENCY DESCENT

A
  1. Power Levers . . . . . . . . . . . . . . . . . . . IDLE
  2. Propeller Levers . . . . . . . . . . . . . . . . .HIGH RPM
  3. Flaps (184 knots maximum) . . . . . . .APPROACH
  4. Landing Gear (182 knots maximum) . .DOWN
  5. Airspeed . . . . . . . . . . . . . . . . . . . . . . . 182 KIAS MAX
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11
Q

GLIDE

A
  1. Landing Gear . . . . . . . . . .UP
  2. Flaps . . . . . . . . . . . . . . . . . UP
  3. Propellers . . . . . . . . . . . . .FEATHERED
  4. Airspeed . . . . . . . . . . . . . .125 KNOTS
  5. Glide Ratio . . . . . . . . . 1.8 nautical miles for each 1000 feet of altitude.
    Decrease by 0.2 nautical miles for each 10 knots of headwind.
  6. ELT Switch . . . . . . . . . . . . . ON
    (Yellow XMT blinking)
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12
Q

DUAL GENERATOR FAILURE [L DC GEN] & [R DC GEN]

A
  1. Instrument Emergency Lights . . . .ON
  2. Generators . . . . . . . . . . . . . . . . . . . .RESET, THEN ON
    If Either Generator Will Reset:
  3. Operating Generator Load Meter . DO NOT EXCEED 100%
    If Neither Generator Will Reset:
  4. Environmental Mode Selector . . . ..OFF
  5. Vent Blowers . . . . . . . . . . . . . . . . . . . AUTO
  6. Non-essential equipment . . . . . . . . OFF
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13
Q

PRESSURIZATION LOSS [CABIN ALT HI]

A
  1. Oxygen Mask(s). . . . . . . . . DON
  2. Mic Switch(es) . . . . . . . . . . OXY
    Masks must be set to 100% at cabin altitudes above
    20,000 feet. Duration tables are based on masks set at normal below 20,000 feet.
  3. Descend . . . . . . . . . . . . . . .AS REQUIRED
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14
Q

HIGH DIFFERENTIAL PRESSURE

Anytime the Differential Pressure goes into the Red Arc:

A
  1. Cabin Altitude Controller . . . . . . . SELECT HIGHER CABIN ALTITUDE
    SETTING
    If Condition Persists:
  2. Bleed Air Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED
  3. Cabin Pressure (after cabin is depressurized). . . . . . . . . . . . . . . DUMP
  4. Bleed Air Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
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15
Q

EMERGENCY EXIT

The third cabin window on the right side is the EMERGENCY EXIT hatch.

A
  1. Emerg Release Hatch Cover . . . OPEN
  2. Release Button . . . . . . . . . . . . . . .PUSH
  3. If release button will not push,
    PULL hooks to override pressure lock and then PUSH the release button.
  4. PULL handle and PUSH out hatch.
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16
Q

AUTOPILOT TRIM FAIL [TRIM]

A
  1. Flight Controls. . . . . . . . . . . . HOLD FIRMLY
  2. AP . . . . . . . . . . . . . . . . . . . . . . DISENGAGE

CAE C90 (11 decks)

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