EMRGENCY PROCEDURES Flashcards

1
Q

SIMULATING ZERO THRUST (1 ENGINE INOP)

A
  1. 1800 RPM´S
  2. POWER - 100 LBS TORQUE
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2
Q

SPINS

A
  1. ELEVATOR - FULL FORWARD
  2. RUDDER - OPPOSITE DIRECTION.
  3. POWER - IDLE
  4. CONTROLS - NEUTRAL
  5. SMOOTH RECOVER (PULL UP)
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3
Q

CABIN DOOR WARNING ANNUNCIATOR

A
  1. ADVISE PAX - FASTEN SB/ REMAIN FAR AWAY FRM THE DOOR.
  2. START DESCENT
  3. DEPRESSURIZE THE CABIN - DUMP VALVE ON PEDESTAL
  4. SAFE ALTITUDE (10,000 FT)
  5. LAND AS SOON AS PRACTICAL
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4
Q

EMERGENCY EXIT NEEDED

A
  1. CABIN DEPRESSURIZED
  2. EMERGENCY RELEASE HATCH COVER - OPEN
  3. RELEASE BOTTON - PUSH
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5
Q

CRACKED WSH OUTER PANEL

A

NO ACTION NEEDED (WIPERS AND HEATING ELEMENTS INOP)

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6
Q

CRACKED WSH INNER PANEL

A
  1. DESCENT
  2. RESET PRESSURIZATION TO ACHIEVE 3.0 PSI OR LESS DIFFERENTIAL PRESSURE.
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7
Q

ELECTRICAL SMOKE OR FIRE

A
  1. OXYGEN
    *SYSTEM READY (PULL ON)
    *CREW (QUICK DON MASK 100% POSITION)
    *MIC SELECTOR (OX MASKS)
    *AUDIO SPEAKER (ON)
  2. CABIN TEMP MODE (OFF)
  3. VENT BLOWER (AUTO)
  4. AVIONICS MASTER (OFF)
  5. NONESSENTIAL ELECTRICAL EQUIPMENT (OFF)

IF FIRE PERSISTS

  1. CABIN PRESSURE (DUMP)
  2. LAND ASAP
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8
Q

GRAY SMOKE IS ASSOCIATED WITH…

A

ELECTRICAL FAILURE ( EYES AND NOSE SORENESS)

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9
Q

IF THERE IS SMOKE ON THE CABIN, YOU MUST DEPLOY THE OXYGEN MASK?

A

NO, IF THEY ARE DEPLOYED AUTOMATICALLY YOU MUST ADVISE PAX NOT TO USE THEM, UNLESS CABIN ALTITUDE EXCEEDS 15,000 FT.

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10
Q

INVERTER FAILURE

A

SELECT THE OTHER INVERTER

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11
Q

GENERATOR INOP (L/R DC GEN)

A
  1. LOAD METTER - VERIFY GENERATOR IS OFF (0%)
  2. GENERATOR - RESET, THEN ON
    * IF GENERATOR DOES NOT RESET *
  3. GENERATOR - OFF
  4. LOAD METTER - DO NOT EXCEED 100%
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12
Q

BATTERY CHARGE RATE (BATTERY CHARGE) INFLIGHT

A
  1. BATTERY SWITCH - OFF
  2. BATTERY CHARGE - ANN EXTING
    CONTINUE FLIGHT
  3. BATTERY CHARGE ANN STILL ILLUMINATED - LAND ASAP
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13
Q

WHAT DOES THE ANNUNCIATOR “BATTERY CHARGE” MEANS INFLIGHT?

A

POSSIBLE BATTERY FAILURE

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14
Q

BATTERY CHARGE ANN ILLUMINATED BEFORE TAKEOFF

A

ABORT TAKEOFF

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14
Q

EXCESIVE LOAD METTER INDICATION (ABOVE 100%)

A
  1. BATTERY - OFF
    *LOAD METTER STILL INDICATING ABOVE 100%
  2. NON ESSENTIAL EQUIPMENT - OFF
    *IF LOAD METTER SHOWS BELOW 100%
  3. BATTERY - ON
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14
Q

NON ESSENTIAL CIRCUIT BRAKER TRIPPED

A
  1. ESSENTIAL CIRCUIT BRAKER - DO NOT RESET INFLIGHT
14
Q
A
14
Q

ESSENTIAL CIRCUIT BRAKER TRIPPED

A

PUSH TO RESET (ONCE PENDEJO)

14
Q
A
14
Q

AVIONICS MASTER POWER SWITCH FAILURE

A

AVIONICS MASTER CRCUIT BRAKER - PULL

14
Q

BOOST PUMP FAILURE

A
  1. INOP FUEL BOOST PUMP - OFF
  2. DETERMINE WHETER CONTINUATION OF FLIGHT WITH CROSS-FEED OPEN IS POSSIBLE.
14
Q

HOW CAN YOU DETERMINE WHICH BOOST PUMP HAS FAILED?

A
  1. “FUEL CROSSFEED” ANN -ILUMINATED
  2. CROSSFEED - CLOSED
    3 - L-R “FUEL PRESS” - ILLUMINATE
  3. BOOST PUMP FAILED - IDENT
  4. CROSSFEED - OPEN
  5. “FUEL PRESS” - OFF
14
Q

IF CROSSFEED IS DISCUNTINUED DURING A BP FAIL…

A

EXPECT LOSS POWER
1. OPEN CROSSFEED IMMEDIATELY
2. REDUCE POWER/ DESCENT TO A LOWER ALTITUDE/ WAIT FOR FUEL TO COOL.

15
Q

ACCUMULATED TIME OF “FUEL PRESS” OPERATION

A

LIMITED ON 10 HOURS

15
Q

CROSSFEED (EMERGENCY ONE ENG INOP)

A

1- BOOST PUMPS - ON
2. TRANSFER PUMPS - ON
3. CROSFFEED - OPEN (CHECK FUEL CROSSFEED IS ON)
4. BOOST PUMP (INOP ENG) - OFF (CHECK RESPECTIVE “FUEL PRESS” OUT)

15
Q

TO DISCONTINUE CROSSFEED

A
  1. BOTH BOOST PUMPS - ON
  2. CROSSFEED SWITCH - CLOSED
  3. FUEL BOOST PUMP (INOP ENG) - OFF
15
Q

TRANSFER PUMP FAILURE

A
  1. TRANSFER PUMP - OFF
16
Q

L/R “NO FUEL XFR” WITH FUEL IN BOTH TANKS, INDICATES

A

TRANSFER PUMP FAILS , BUT CONTINUE RECEIVING FUEL BY GRAVITY

17
Q

TRANSFER PUMP INOP, DECREASES NACELLE TANK BY …

A

28 GAL