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P3C > Memory Items > Flashcards

Memory Items Flashcards

1
Q

FUS DUCT HOT LIGHT

A
  1. ON GROUND, SECURE GROUND AC AND ALL ENGINE AND APU BLEED AIR, AND RETURN TO THE LINE
  2. IN FLIGHT, CLOSE ALL ENGINE BLEED AND FUSELAGE SHUTOFF VALVES
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2
Q

START VALVE LIGHT ON AFTER START

A

CHECK OVERHEAD PANEL FOR INDIVIDUAL START CONTROL VALVE OPEN LIGHT

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3
Q

NTS INOPR

A
  1. CONTINUE HOLDING OUT FEATHER BUTTON
  2. EMERGENCY SHUTDOWN HANDLE-PULL
  3. FEATHER BUTTON-PUSH
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4
Q

1, 2, 3, OR 4 STARTER CONTROL VALVE OPEN LIGHT

A

IF LIGHT REMAINS ON OR COMES ON AFTER START, SECURE ENGINE BY PULLING EMERGENCY SHUTDOWN HANDLE

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5
Q

FIRE OF UNKNOWN ORIGIN

A
  1. ALERT THE CREW, ACTIVATE THE FIRE BILL

2. CABIN EXHAUST FAN-OFF

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6
Q

RAPID DECOMPRESSION

A
  1. PRESSURIZATION GROUND CHECK SWITCH-TEST

2. GROUND AC- ON

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7
Q

EMERGENCY DEPRESSURIZATION

A
  1. AUX VENT-OPEN
  2. OUTFLOW VALVE-OPEN
  3. EDCS-DUMP
  4. AUX VENT- CLOSE AT 1 IN DIFFERENTIAL
    W/O ELECTRICAL POWER
  5. FREEFALL CHUTE-OPEN
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8
Q

EMERGENCY DESCENT

A
  1. AUTOPILOT-DISENGAGED
  2. POWER LEVERS-IDLE
  3. LANDING GEAR-AS REQUIRED (DOWN)
  4. AIRSPEED-AS REQUIRED (300 KTS)
  5. PRESSURIZATION-AS REQUIRED
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9
Q

BRAKE FIRE

A
  1. REQUEST GROUND FIREFIGHTING EQUIPMENT

2. STOP THE AIRCRAFT

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10
Q

ENGINE FIRE ON THE GROUND

A
  1. EMERGENCY SHUTDOWN HANDLE-PULL
  2. HRD-DISCHARGED
    CALL FOR ENGINE FIRE ON THE GROUND CHECKLIST
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11
Q

EMERGENCY SHUTDOWN PROCEDURE

A
  1. EMERGENCY SHUTDOWN HANDLE-PULL
  2. HRD (FIRE ONLY)-DISCHARGED
    CALL FOR SHUTDOWN CHECKLIST CHECKLIST
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12
Q

SHIFTING TO BOOST OFF

A
  1. DISCONNECT THE AUTOPILOT
  2. ATTEMPT TO ATTAIN A SAFE ALTITUDE
  3. SET CONDITION V
  4. TRIM TAB SETTING- CHECK FOR NORMAL POSITION
    IF ABNORMAL FORCES STILL PRESENT
  5. BOOSTER SHIFT HANDLE- PULL
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13
Q

INDICATIONS OF A PROP MALFUNCTION

A

PROP PUMP LIGHT, LEAK OR AN OFFSPEED CONDITION DETECTED AUDIBLY. CONSIDERED OFFSPEED IF FLUX IS +/- 1% OF MECHANICAL OR ELECTRICAL GOVERNING OR ANY SUSTAINED OSCILLATION OCCURS

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14
Q

2 WARNINGS WITH PROP PUMP

A
  1. IF SIGNIFICANT AIRFRAME VIBRATION ACCOMPANIES LIGHT OR LEAK, CONSIDER EMERGENCY SHUTDOWN
  2. IF OVERSPEEDS ABOVE 115%, REDUCE AIRSPEED AS SOON AS POSSIBLE, NO LESS THAN 150 KIAS. GO TO OPS WITH PITCHLOCKED PROP
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15
Q

PROPELLER MALFUNCTIONS

A
  1. IF RPM AT OR ABOVE 115%- REDUCE AIRSPEED (150 KIAS MIN) AND PERFORM OPERATION WITH A PITCHLOCKED PROP PROCEDURE, PARAGRAPH 15.12.2
  2. IF RPM IS BELOW 115%- SMOOTHLY ADVANCE AFFECTED POWER LEVER AND INCREASE TAS, NOTING ENGINE INDICATIONS
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16
Q

PROP FAILS TO FEATHER

A
  1. FEATHER BUTTON-IN
  2. PCO-PRESS
  3. ALTERNATE BUS (1&4)- SELECT
  4. PROP FEATHER CIRCUIT BREAKERS- CHECK IN
  5. AIRSPEED- DECREASE TOWARDS 150 KIAS
    IF FEATHER BUTTON LIGHT REMAINS ON
  6. PROP FEATHER CONT CB- PULL
17
Q

LOSS OF ALL AIRSPEED INDICATION

A
  1. CHECK PITOT HEAT-ON
18
Q

OUT OF CONTROLLED FLIGHT

A
  1. POWER LEVERS-IDLE
  2. FLIGHT CONTROLS-NEUTRALIZE
  3. AIRSPEED, AOA, TURN NEEDLE-CHECK
    IF IN A SPIN
  4. RUDDER-FULL OPPOSITE TURN NEEDLE
    AS SOON AS YAWING MOTION STOPS
  5. CONTROLS-NEUTRALIZE
  6. UNUSUAL ATTITUDE-RECOVER
19
Q

TCAS RESOLUTION ADVISORY PROCEDURE

A

AUTOPILOT-DISCONNECT
POWER LEVERS-AS REQUIRED
COMPLY WITH VERTICAL GUIDANCE
ATTEMPT TO GAIN AND MAINTAIN VISUAL CONTACT WITH TRAFFIC

20
Q

WINDSHEAR ESCAPE PROCEDURE

A

MAX POWER-SET
PITCH ATTITUDE-10 DEGREES UP
LANDING GEAR-UP
FLAPS- DO NOT CHANGE UNTIL OUT OF WINDSHEAR

21
Q

SPLIT FLAP PROCEDURE

A

IF UNCONTROLLABLE, RESET FLAPS TO PREVIOUS POSITION

IF CONTROLLABLE, LAND WITH THE FLAP HANDLE IN THE SELECTED POSITION

22
Q

2 ENGINE WAVEOFF

A

A/S- 145 KIAS MINIMUM
POWER LEVERS-ADVANCE TO MAX POWER AS SOON AS DIRECTIONAL CONTROL IS GAINED
RAISE THE WING WITH THE INOPERATIVE ENGINES SUFFICIENTLY TO OPTIMIZE CONTROL AND CLIMB PERFORMANCE (UP TO 5 DEGREES, IF NECESSARY)
WING FLAP LEVER-APPROACH
LANDING GEAR LEVER-UP
WING FLAP LEVER-MANUVER, THEN UP (145 KIAS MIN)

23
Q

PRESSURIZATION LOSS

A

DON SMOKE MASKS
ALERT CREW
(NOT ASTERICK)
VERIFY OBSTACLE CLEARANCE
INVESTIGATE PRESSURIZATION LOSS

24
Q

FLIGHT WITH CRACKED FRONT WINDSHIELD

A

TURN OFF HEAT OF AFFECTED PANELS

HELMETS ON, VISORS DOWN

25
Q

STALL RECOVERY PROCEDURES

A

STEPS 1 AND 2 ARE TO BE PERFORMED SIMULTANEOUSLY
AP-DISCONNECT
POWER LEVERS-SYMMETRICALLY ADVANCE
YOKE-RELAX BACK PRESSURE
ATTITUDE-LEVEL WINGS, CENTER BALL
PITCH ATTITUDE-RECOVER AS AIRSPEED INCREASES

26
Q

STALL RECOVERY PROCEDURES

A

STEPS 1 AND 2 ARE TO BE PERFORMED SIMULTANEOUSLY
AP-DISCONNECT
POWER LEVERS-SYMMETRICALLY ADVANCE
YOKE-RELAX BACK PRESSURE
ATTITUDE-LEVEL WINGS, CENTER BALL
PITCH ATTITUDE-RECOVER AS AIRSPEED INCREASES

27
Q

DITCHING PROCEDURES

A

ALERT CREW TIME TO IMPACT-ALERTED

28
Q

OUT OF CONTROLLED FLIGHT

A

POWER LEVERS-FLIGHT IDLE
FLIGHT CONTROLS-NEUTRALIZE
AIRSPEED, AOA, TURN NEEDLE-CHECK
IF IN A SPIN:
RUDDER-FULL OPPOSITE TURN NEEDLE
AS SOON AS YAWING MOTION STOPS:
FLIGHT CONTROLS-NEUTRALIZE
UNUSUAL ATTITUDE-RECOVER

P3C (10 decks)

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