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Aurora > Emergencies > Flashcards

Emergencies Flashcards

1
Q

Abort procedure

A
  1. Pilot-Aborting
    note-power levers retarded from max power to flight idle in under 1 second, significant RPM undershoot may result and generators may drop off line momentarily
  2. power levers-flight idle
    Warning-if malfunction causing abort is prop or engine related, ehandle associated engine prior to entering ground range
  3. Engine-E-handle
    Warning-do not pull power levers over the ramp into the ground range until below 135 to avoid pitchlock or decouple
    note-if no beta light, slowly bring power lever back in ground range, anticipating a swerve. If swerve occurs, e handle engine.
  4. Power levers- reverse as req
  5. rudder, aileron, power levers, nosewheel steering- be a pilot
  6. yoke- hold control column forward
  7. brakes- apply when required
  8. control column-transfer control
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2
Q

cracked front windshield check

A
  1. airspeed- reduce airspeed to 240 kias or below

2. windshield heat- FE selects WINDSHIELD HEAT OFF, on affected panels

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3
Q

cracked side window

A
  1. FE selects SIDE WINDOW HEAT OFF, on affected window
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4
Q

IN FLIGHT SINGLE GENERATOR OPS CHECK

A
  1. ELECTRICAL LOADS-REDUCE

2. APU-IN FLIGHT START (IAW APU IN FLIGHT START CHECK)

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5
Q

AC POWER FAILURE CHECK

A
  1. BOOST HANDLES-PULL OUT
    2.UTILITY LIGHT-ON (IF REQUIRED) AND POSITIONED
    WARNING-LEAVING THE ENGINE START SELECTOR SELECTED TO AN ENGINE WILL RESULT IN BATTERY DRAINAGE
  2. ENGINE START SELECTOR OR INVERTER BATTERY TEST-SELECTED TO AN ENGINE OR SELECT TEST
  3. RESTORE ELECTRICAL POWER-ATTEMPT GENERATOR RESET CHECK AND/OR APU IN-FLIGHT START CHECK
    NOTE-IF ABLE TO RESTORE ELECTRICAL POWER, SEE IN-FLIGHT SINGLE GENERATOR OPS CHECK OR RESUME NORMAL OPERATIONS, AS APPLICABLE. IF UNABLE TO RESTORE ELECTRICAL POWER, CONTINUE WITH CHECK
  4. IN-FLIGHT CONSIDERATIONS-REMAINDER OF THE FLIGHT WILL BE BOOST OUT, PARTIAL PANEL, WITHOUT ELECTRONIC NAVAIDS OR COMMUNICATIONS. FLAPS REMAIN IN LAST SELECTED POSITION. DE-ICE IS LIMITED TO ENGINE ANTI-ICE
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6
Q

EMERGENCY HIGH SPEED DESCENT PROCEDURE

A
  1. AFDS- DISENGAGE
  2. POWER LEVERS- FLIGHT IDLE
  3. LANDING GEAR- DOWN
  4. PRESSURIZATION- SET
  5. AIRSPEED-VNEABOVE FL245, 300 BELOW FL245
    NOTE-ADC MISCOMPARES MAY BE DISPLAYED ON CDUS DURING HIGH SPEED DESCENT
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7
Q

EMERGENCY LOW SPEED DESCENT PROCEDURE

A
  1. AFDS-DISENGAGE
  2. POWER LEVERS-FLIGHT IDLE
  3. LANDING GEAR- DOWN
  4. FLAPS-LAND
  5. PRESSURIZATION-SET
  6. AIRSPEED-MAX 170KIAS
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8
Q

APU FIRE PROCEDURE

A
  1. MAN REL AUX PWR UNIT EXTINGUISHER SWITCH-ACTIVATE

2. APU CONTROL SWITCH-OFF

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9
Q

BRAKE FIRE PROCEDURE

A
  1. TOWER-REQUEST FIREFIGHTING EQUIPMENT
  2. STOP AIRCRAFT-PARKING BRAKE SET OPPOSITE FIRE
  3. RPM-NORMAL OVER BURNING BRAKE
    4.SHP-1000SHP OVER BURNING BRAKE
    5.FLAPS-TAKEOFF
    6.ENGINES NOT REQUIRED-E-HANDLE ENGINES NOT REQUIRED
  4. EVACUATE UNNECESSARY PERSONNEL-EVACUATE OVER THE WING
    WARNING-PERSONNEL SHOULD EXERCISE CAUTIONTO REMAIN CLEAR OF THE FUEL DUMP DEFLECTION FENCE WHEN SLIDING OFF THE PORT WING
    ON ARRIVAL OF GROUND FIRE-FIGHTING EQUIPMENT
  5. REMAINING ENGINE-E-HANDLE
  6. APU-SHUTDOWN
  7. ABANDON AIRCRAFT-EVACUATE OVER THE WING
    WARNING-IF BRAKE FIRES ON BOTH SIDES, CONSIDER EVACUATING IMMEDIATELY. ACTION MUST BE TAKEN TO DEFLECT FLAMES FROM WINGS WITH MAX REVERSE ON 1 AND 4 AND HOLDING AIRCRAFT STATIONARY WITH POSITIVE ON 2 AND 3 UNTIL FIREFIGHTING EQUIPMENT ARRIVES. PRIOR TO ABANDONING, EHANDLE ALL ENGINES
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10
Q

CABIN FIRE CHECK

A
  1. CREW WARNING-PILOT ANNOUNCES “CREW CARRY OUT CABIN FIRE PROCEDURES.” CREW CARRIES OUT PROCEDURES LAID OUT IN CABIN FIRE RESPONSIBILITIES.
  2. SMOKE MASKS/ICS- IF REQUIRED, PILOT, COPILOT, AND FE DON SMOKE MASKS, SELECT ICS TO SMOKE MASK POSITION AND CONFIRM “ON.”
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11
Q

ENGINE FIRE ON THE GROUND PROCEDURE

A

1.ABORT
2. SHUTDOWN ENGINE- DIRECT EHANDLE, HRD
3. E-HANDLE, HRD
4. ALT HRD-DIRECT IF FIRE PERSISTS
5. ALT HRD-DISCHARGE
6. STOP AIRCRAFT
7. FIREFIGHTING EQUIPMENT-REQUEST AND NOTIFY TOWER
8. FLAPS-TAKEOFF
NOTE-IF INDICATIONS ARE THAT THE FIRE IS OUT, THE AIRCRAFT MAY BE TAXIED.
WARNING-ENSURE EVACUATION IS CARRIED OUT ON THE SIDE OF THE AIRCRAFT OPPOSITE THE FIRE
9.BRIEF CREW
10. REMAINING ENGINES/APU- EHANDLE AND SHUTDOWN
11.COMMAND BELL- PRESS

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12
Q

ENGINE FIRE IN FLIGHT PROCEDURE

A
  1. ADVISE PILOT OF FIRE
  2. SHUTDOWN ENGINE-DIRECT FE EHANDLE, HRD
  3. EHANDLE, HRD BOTTLE-PULL AND DISCHARGE
    WARNING-IF FIRE PERSISTS, INDICATED BY VISUAL FLAMES OR PERSISTENT SMOKE, THEN COMPLETE ITEMS 4, 5, AND 6, OTHERWISE GO TO ITEM 6.
  4. TRANSFER HRD BOTTLE-DIRECT IF FIRE PERSISTS
  5. ALTERNATE HRD-DISCHARGED
    WARNING- IF FIRE PERSISTS AFTER ALT HRD, WING FIRE COULD RESULT, IF IMMEDIATE LANDING CANNOT BE MADE, DITCHING SHOULD BE
    CONSIDERED
  6. PROP-PROP STOPPED/ROTATING FORWARD/BACKWARDS
    WARNING-IF PROP HAS FAILED TO STOP, CARRY OUT PROP FAIL TO FEATHER OR BACKWARD ROTATING PROP CHECK
    NOTE-CARRY OUT EMERGENCY SHUTDOWN CHECK
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13
Q

WING FIRE PROCEDURE

A

IF NOT ASSOCIATED WITH AN ENGINE, OMIT STEP 1

  1. ENGINE-CARRY OUT ENGINE FIRE IN FLIGHT PROCEDURE
  2. SPEED-INCREASE TAS
  3. SIDE-SLIP-AS REQUIRED, TO MINIMIZE EFFECT OF FLAMES TO FUSELAGE OR ENGINE
  4. LAND OR DITCH ASAP
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14
Q

AFDS DISCONNECT PROCEDURE

A
  1. DISCONNECT AUTOPILOT
  2. IF MALFUNCTION PERSISTS:
    A. AFDS-DISENGAGED
    WARNING-THE AUTOPILOT EMERGENCY DISCONNECT HANDLE MUST BE STOWED IN THE HORIZONTAL POSITION OR IT WILL BE IMPOSSIBLE TO PULL THE THREE FLIGHT CONTROL BOOSTER LEVERS TO THE BOOST OUT POSITION
    NOTE-AUTOPILOT WILL BE DISCONNECTED ELECTRICALLY IF THE HANDLE IS PULLED 6 INCHES. AUTOPILOT WILL BE AVAILABLE WHEN THE HANDLE IS RELEASED. FULL TRAVEL OF THE HANDLE WILL DISCONNECT THE AUTOPILOT ELECTRICALLY AND MECHANICALLY.
    B. AUTOPILOT EMERGENCY DISCONNECT HANDLE-PULL
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15
Q

BINDING FLIGHT CONTROL PROCEDURE

A

1.AFDS-DISCONNECT
NOTE-IF ELECTRICAL DISCONNECT DOES NOT SOLVE THE PROBLEM, CARRY OUT A FULL MECHANICAL DISCONNECT TO FULLY ELIMINATE ANY POSSIBILITY OF AFCS INTERFERING WITH THE FLIGHT CONTROL SYSTEM REGARDLESS OF WHETHER IT WAS ENGAGED OR NOT AT THE TIME OF CONTROL DIFFICULTY
2.TRIM TABS-CHECK FOR NORMAL POSITION
WARNING-DO NOT APPLY FORCE TO CONTROL SURFACE WHILE SHIFTING BOOSTER HANDLES TO AVOID A SUDDEN CHANGE IN CONTROL SURFACE POSITION.
3. BOOSTER HANDLE-PULL APPROPRIATE BOOSTER HANDLE
UNABLE TO SHIFT FOR ANY REASON
4.BOOSTER HANDLES-PULL HANDLES FOR OTHER 2 SURFACES
5.HYDRAULIC PUMPS-OFF
6. BOOSTER HANDLE-PULL FOR MALFUNCTIONING SURFACE
7. HYD PUMPS-ON, UNLESS SHIFT CANNOT BE COMPLETED. LEAVE THEM OFF IN THAT CASE
IF HYD PRESSURE IS RESTORED
8. BOOSTER HANDLE-PUSH IN FOR TWO OTHER SURFACES

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16
Q

FREE/INEFFECTIVE FLIGHT CONTROL

A 
IF ELEVATOR CONTROL IS LOST
1. ELEVATOR BOOSTER HANDLE-FE ENSURES IN
2.AFDS- PILOT SILECTS AP ENGAGE
IF AILERON CONTROL IS LOST
1. AILERON AND RUDDER BOOSTER HANDLES-FE ENSURES IN
2. AFDS- PILOT SELECTS AP ENGAGE
IF RUDDER CONTROL IS LOST
1. RUDDER BOOSTER HANDLE-FE ENSURES IN
2. AFDS YAW DAMPER- PILOT SELECTS ENGAGE
17
Q

BOOST OUT LANDING PROCEDURE

A
  1. TRAFFIC PATTERN-FLY WIDER THAN NORMAL
  2. AIRSPEED- FLY SAME SPEED SCHEDULE AS NO FLAP LANDING
  3. FLAPS-LANDING SHOULD BE CARRIED OUT FLAPS UP OR APPROACH
  4. GLIDE PATH-FLY SLIGHTLY FLATTER THAN NORMAL
    5.TOUCHDOWN -LAND WITH POWER ON AND NOSE SLIGHTLY UP
    WARNING-DO NOT PULL POWER LEVERS OVER THE RAMP INTO THE GROUND RANGLE UNTIL SPEED IS BELOW 135 KIAS WITH ELECTRICAL POWER OR 125 KIAS WITHOUT ELECTRICAL POWER TO PREVENT PITCH LOCK OR DECOUPLE
  5. REVERSE THRUST-REVERSE AS REQUIRED HAVING THE COPILOT HOLD THE CONTROL COLUMN IN THE FORWARD POSITION
18
Q

ASYMMETRIC FLAP CHECK

A

WARNING-IF THE FLAP ASYMMETRY PROTECTION SYSTEM MALFUNCTIONS, AN UNNANUNCIATED SPLIT FLAP CONDITION MAY OCCUR RESULTING IN UNCOMMANDED YAW AND ROLL AND POSSIBLY, LOSS OF CONTROL.

  1. AIRCRAFT-CONTROL WITH AILERON, RUDDER, AND DIFFERENTIAL POWER AS REQUIRED. INCREASE AIRSPEED, TO INCREASE AIRCRAFT CONTROL.
  2. FLPA HANDLE-DO NOT MOVE FROM SELECTED POSITION. IF THE AIRCRAFT CANNOT BE CONTROLLED, RETURN HANDLE TO LAST POSITION.
19
Q

ZERO FLAP LANDING PROCEDURE

A
  1. BRIEF COPILOT MIN AIRSPEED ON FINAL WILL BE 1.2VS OR 135 KIAS MINIMUM AND TO CALL BELOW 135 ON ROLLOUT SO THE POWER LEVERS CAN GO INTO REVERSE.
  2. INSTRUMENT PATTERN-BE A PILOT
  3. VISUAL PATTERN- FLAY A PATTERN MAINTAINING 1.52 VS OR 160 KIAS, WHICH EVER IS GREATER UNTIL ESTABLISHED ON FINAL
  4. RUDDER BOOST SHUTOFF VALVE-PULL
  5. LANDING LIGHTS- ADJUSTED FOR NOSE HIGH ATTITUDE
  6. TOUCHDOWN-SLOW AIRCRAFT TO ARRIVE OVER THE THRESHOLD AT 1.2 Vs OR 135 KIAS MIN. BE A PILOT
20
Q

LOSS OF AIRSPEED INDICATION CHECK

A
  1. CONTROL-FLY KNOWN COMBINATIONS OF ATTITUDE AND POWER

2. PITOT HEAT-ON

21
Q

ATTITUDE/EGI FAILURE CHECK

A
  1. DCP/NORM ALT-DEPRESS TO SELECT ALTERNATE EGI IF AVAILABLE
22
Q

HEADING FAILURE CHECK

A
  1. DCP/NORM ALT-DEPRESS TO SELECT ALTERNATE EGI
23
Q

FUEL BOOST PUMP FAILURE IN CLIMB CHECK

A

WARNING-IF FUEL BOOST PUMP POWER CIRCUIT-BREAKERS AND/OR CONTROL CIRCUIT-BREAKERS ARE OUT-DO NOT RESET. TURN THE FUEL BOOST PUMP SWICTH OFF

24
Q

FUEL TRANSFER PUMP FAILURE CHECK

A

WARNING-IF FUEL TRANSFER POWER CIRCUIT-BREAKERS AND/OR CONTROL CIRCUIT-BREAKERS ARE OUT- DO NOT RESET

25
Q

FUEL QUANTITY SYSTEM FAILURE

A

WARNING-DO NOT CONNECT OR DISCONNECT FUEL QUANTITY INDICATOR PLUGS WHILE IN FLIGHT. THIS ACTION MAY CAUSE A SPARK TO BE GENERATED INSIDE THE FUEL TANK UNDER CERTAIN CONDITIONS

26
Q

LOSS OF BOTH HYDRAULIC SYSTEMS PROCEDURE

A
  1. HYD PUMPS-CONFIRM PRESS LOSS OF BOTH SYSTEMS, THEN OFF
  2. FLIGHT CONTROL BOOSTER HANDLES- PULL OUT ALL THREE
  3. BOMB BAY-IF REQUIRED, OPERATE USING BOMB BAY DOORS HYD FAILURE CHECK
  4. FLAPS-REMAIN AT CURRENT SETTING
  5. AIR BRAKE HANDLE WITNESS WIRE-CUT, EXERCISING CARE TO PREVENT INADVERTENT AIR BRAKE APPLICATION
  6. HYD BRAKE PRESS-CHECK PRESSURE TO DETERMINE NUMBER OF BRAKE APPLICATIONS AVAILABLE. IF LFUID REMAINS IN NO. 1 SYSTEM RESERVOIR, SELECT 1B PUMP ON
    NOTE-DO NOT CHECK BRAKES ON PRE-LANDING CHECK
  7. LANDING GEAR-LOWER GEAR BY EMERGENCY LANDING GEAR EXTENSION CHECK (WITHOUT HYD CONTROL)
  8. LANDING-LAND USING BOOST OUT LANDING PROCEDURE
27
Q

TIRE FAILURE PROCEDURES

A
  1. TAKEOFF (AT OR ABOVE 80 KNOTS)-CONTINUE TAKE-OFF (STUPID)

2. LANDING GEAR-DO NOT RAISE THE LANDING GEAR AS THE BLOWN TIRE MAY JAME THE GEAR IN THE WHEEL WALL

28
Q

EXPLOSIVE/RAPID DECOMPRESSION PROCEDURE

A

1.OXYGEN- AS REQUIRED
IF EXPLOSIVE DECOMPRESSION
2. EMERGENCY DESCENT-CARRY OUT APPROPRIATE EMERGENCY DESCENT PROCEDURE AND ADVISE ATC. LEVER OFF AND INVESTIGATE
IF RAPID DECOMPRESSION
3. RESTORE PRESSURE-CARRY OUT PRESSURIZATION RESTORATION CHECK

29
Q

PRESSURIZATION RESTORATION CHECK

A
  1. CABIN PRESSURIZATION GRD CHECK SWITCH-TEST

2. GRD AIR COND SWITCH-ON

30
Q

ENGINE FAILURE AFTER Vr PROCEDURE

A
  1. RUDDER AND AIRLERON-BE A PILOT
  2. CONTROL COLUMN-HOLD SLIGHTLY FORWARD FOR DIRECTIONAL CONTROL
    WARNING-FULL AILERON CONTROL WHEEL AWAY FROM THE FAILED ENGINE MAY BE NESCESSARY TO MAINTAIN WINGS LEVEL
  3. AIRSPEED-ACCELERATE TO Vro, ROTATE AND ACCELERATE TO THREE-ENGINE CLIMBOUT SPED (V50 THREE-ENGINE)
  4. WING-RAISE INOERATIVE ENGINE 5 DEGREES TO OPTIMIZE Vmca
  5. LANDING GEAR-WITH RATE OF CLIMB, RAISE GEAR
    NOTE-FUEL DUMP AND/OR ARMAMENT JETTISON MAY BE REQUIRED TO REDUCE WEIGHT WITH LOSS OF MORE THAN ONE ENGINE
  6. FLAPS-MANUEVER AFTER 160 WITH GEAR UP AND CLEAR OF TERRAIN. UP AFTER 180 KIAS
  7. EMERGENCY SHUTDOWN-COMPLETE WHEN CONDITONS PERMIT
  8. AIRSPEED-THREE-ENGINE CLIMBOUT SPEED (190)
31
Q

EMERGENCY SHUTDOWN PROCEDURE

A
  1. E HANDLE ENGINE
  2. PROP STOPPER-EMERGENCY SHUTDOWN CHECK
    FORMWARD-PROP FAILS TO FEATHER THEN EMERGENCY SHUTDOWN CLEAN UP CHECK
    PROP BACKWARDS-BACKWARDS ROTATING PROP CHECK THEN EMERGENCY SHUTDOWN CLEANUP CHECK
32
Q

THREE ENGINE LANDING PROCEDURE BRIEF

A
  1. RUNWAY SELECTION, LENGTH, AND CONDITION
  2. WIND EFFECT ON APPROACH, LANDING, AND OVER SHOOT
  3. COPILOT DUTIES
33
Q

THREE ENGINE OVERSHOOT PROCEDURE

A

WARNING-A LOSS OF DIRECTIONAL CONTROL MAY DEVELOP WITH THE APPLICATION OF ASYMMETRICAL POWER IF MINIMUM APPROACH SPEEDS ARE NOT MAINTAINED AND/OR A CROSSWIND CORRECTION IS APPLIED TOWARD THE INOPERATIVE ENGINE

  1. POWER-ADVANCE POWER AS QUICKLY AS DIRECTIONAL CONTROL PERMITS.
  2. OPTIMUM BANK- RAISE THE DED ENGINE 5 DEGREES
  3. FLAPS-TAKEOFF
  4. LANDING GEAR-UP
  5. FLAPS-MANUEVER, THEN UP
  6. POST TAKEOFF CHECK

Aurora (5 decks)

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