Emergency Ops - Recall Items

Question 1

EMERGENCY ENGINE SHUTDOWN

Answer 1

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

Question 2

ENGINE FIRE ON GROUND

Answer 2

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

Question 3

HOT / HUNG START

ITT showing signs of exceeding Limits / N1 not increasing normally

Answer 3

Affected Engine:
1. Condition Lever. . . . . . . . . . . . FUEL CUTOFF
2. Ignition and Engine Start . . . . STARTER ONLY
3. Continue until the end of start time limit - 40 secs

Question 4

ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1)

Sufficient RWY Remaining

Answer 4

1. Power Levers . . . . . . . . . . . . . . . GROUND FINE
2. Brakes . . . . . . . . . . . . . . . . . . . . . MAXIMUM

Question 5

ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1)

If Insufficient Runway Remains for Stopping:

Answer 5

1. Power Levers . . . . . . . . . . . . . . . GROUND FINE
2. Brakes . . . . . . . . . . . . . . . . . . . . . MAXIMUM
3. Condition Levers . . . . . . . . . . .FUEL CUTOFF
4. Fuel FW Shutoff Valve . . . . . . .CLOSE
5. Master Switch . . . . . . . . . . . . . OFF (Gang Bar down)
6. Boost Pumps . . . . . . . . . . . . . .OFF

Question 6

ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1)

Answer 6

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

Question 7

ENGINE FAILURE IN FLIGHT
BELOW (VMCA)

Answer 7

1. Power . . . . . . . . . . . . .REDUCE
2. Nose . . . . . . . . . . . . . . LOWER TO ACCELERATE ABOVE VMCA

Question 8

2ND ENGINE FLAMEOUT

Answer 8

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.

Question 9

ELECTRICAL SMOKE OR FIRE

Answer 9

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

Question 10

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

Answer 10

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

Question 11

EMERGENCY DESCENT

Answer 11

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

Question 12

GLIDE

Answer 12

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)

Question 13

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

Answer 13

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

Question 14

PRESSURIZATION LOSS [CABIN ALT HI]

Answer 14

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

Question 15

HIGH DIFFERENTIAL PRESSURE

Anytime the Differential Pressure goes into the Red Arc:

Answer 15

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

Question 16

EMERGENCY EXIT

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

Answer 16

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.

Question 17

AUTOPILOT TRIM FAIL [TRIM]

Answer 17

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