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Bristow OPC > Memory Actions > Flashcards

Memory Actions Flashcards

1
Q

BOOST HARDOVERS

A
  1. AIRCRAFT ATTITUDE ………………..CONTROL
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2
Q

FD DEGRADED - BELOW 50 KIAS

SAR ONLY

A
  1. AIRCRAFT ATTITUDE ……………….CONTROL
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3
Q

JAMMED OR RESTRICTED

FLIGHT CONTROLS

A
  1. AIRCRAFT ATTITUDE ……………….CONTROL
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4
Q

SAS HARDOVERS

A
  1. AIRCRAFT ATTITUDE ……………….CONTROL
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5
Q

TRIM HARDOVERS

A
  1. AIRCRAFT ATTITUDE …………………………CONTROL using cyclic and collective trim releases
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6
Q

AC GENERATOR

FAILURE (DUAL)

A
  1. APU CTRL ………………………………………….ON
  2. APU GEN …………………………………………..ON
  3. AC GEN NO 1 and NO 2 ……..RESET / OFF then ON
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7
Q

DC (DUAL) AND

BACKUP CONVERTER FAILURE

A
  1. DC CONV BACKUP …………………………….OFF (to recover intercom)
  2. DC CONV 1 AND DC CONV 2 …………… RESET/OFF THEN ON
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8
Q

AUTOROTATIVE LANDING (PF)

A
  1. AUTOROTATION …………
    INITIATE AND ESTABLISH - 80-100 KIAS/105% Nr
  2. SEARCH LIGHT ……………..ON / ADJUST if required
  3. FLARE ……………………………….AT ~100 FT AGL to decrease airspeed and sink rate, and increase Nr.
  4. NOSE UP ATTITUDE …………..REDUCE TO MAXIMUM 10° as the flare loses effectiveness and the helicopter starts to settle
  5. LAND …………….CUSHIONING WITH COLLECTIVE

NOTE
• Automatic float deployment will not function when operating on battery
power only. Manual float deployment (via the collective mounted
FLOAT switch) will function when operating on battery power.

  1. FLOTATION GEAR………………DEPLOY immediately after water contact
  2. FLIGHT CONTROLS ……………DECREASE collective and NEUTRALISE cyclic immediately after landing
  3. WHEEL BRAKES ………………..APPLY as required
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9
Q

AUTOROTATIVE LANDING (PM)

A
  1. APU …………………………………..START
  2. THROTTLES AND FUEL………AS REQUIRED
  3. LANDING GEAR …………………DOWN
  4. PASSENGERS ……………………“BRACE, BRACE, BRACE”
  5. FLOTATION GEAR………………ARM below 80 KIAS (if over water)
  6. RADALT……………………………..CALL below 1000 ft
  7. AIRCRAFT …………………………EVACUATE when rotors stopped

PROCEDURE 5/2 - On Land, or
PROCEDURE 5/3 - On Water

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10
Q 
ENGINE FAILURE (SINGLE) - 
IN A HOVER
A
  1. COLLECTIVE …………………………….MAINTAIN collective setting
  2. COLLECTIVE …………………………….INCREASE to cushion landing
  3. AFTER TOUCHDOWN ………………..NEUTRALISE CYCLIC and REDUCE COLLECTIVE to minimum
  4. WHEEL BRAKES ……………………….APPLY
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11
Q 
ENGINE FAILURE (SINGLE) - 
BEFORE OR AT TDP
A
  1. FLY BRIEFED OEI REJECT PROFILE
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12
Q 
ENGINE FAILURE (SINGLE) - 
AFTER TDP
A
  1. CONTINUE TO FLY BRIEFED OEI TAKE-OFF PROFILE
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13
Q 
ENGINE FAILURE (SINGLE ) - 
IN THE CRUISE
A

1.COLLECTIVE ………………………………….ADJUST to maintain desired Nr while transitioning to OEI airspeed

WARNING
• Do not select two minute power until obstacle clearance is assured.

  1. OEI POWER ……………………………………….SELECT 2 MINUTE and MCP when conditions permit
  2. RIPS ………………………………………………….If in icing conditions, consider selecting manual HEAVY mode
    as required
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14
Q 
ENGINE FAILURE (SINGLE ) - BEFORE OR 
AT LDP - BALKED LANDING (GO AROUND)
A
  1. FLY BRIEFED OEI BALKED LANDING PROFILE
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15
Q 
ENGINE FAILURE (SINGLE) - 
AFTER LDP - SINGLE ENGINE LANDING
A
  1. FLY BRIEFED OEI LANDING PROFILE
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16
Q

ENGINE FAILURE (DUAL) - IN A HOVER

A
  1. AIRCRAFT ATTITUDE …….MAINTAIN LEVEL
  2. COLLECTIVE ……………………………………..INCREASE to cushion landing

After touchdown:

  1. CYCLIC ……………………………………………..SLIGHTLY FORWARD OF CENTRE
  2. COLLECTIVE ……………………………………..FULLY DOWN
  3. BRAKES …………………………………………….APPLY as required
17
Q

ENGINE FAILURE (DUAL) -
IN FORWARD FLIGHT

A
  1. AUTOROTATION…………………………….INITIATE MAINTAIN 100 -105% Nr
  2. AIRSPEED ………………………………………ESTABLISH between 80-100 KIAS
  3. LANDING GEAR ……………………………..Select DOWN
  4. THROTTLES …………………………………….STOP
  5. APU ……………………………………………….ON

If time, altitude & probability of success exists

  1. RESTART ………………………………….ONE OR BOTH ENGINES ATTEMPT

If neither engine will start

  1. PROCEDURE 5/1 ……………….FOLLOW - Autorotative Landing
18
Q

ENGINE HIGH SPEED SHAFT FAILURE

A
  1. AFFECTED ENGINE ………………………IDENTIFY POSITIVELY
  2. THROTTLE (affected engine) ………………..IDLE, PAUSE, STOP
19
Q

APU FIRE

A

1.FIRE ……………………………………………..CONFIRM
If fire cannot be confirmed see CONSIDERATION

With fire confirmed:

  1. APU CTRL ………………………………………….OFF
  2. APU FIRE/ARMED PUSHBUTTON….IDENTIFY/PUSH
  3. FIRE EXTG…………………………………………MAIN

NOTE
• Pressing the FIRE/ARMED pushbutton and deploying the MAIN
extinguisher should put out most APU fires. If the FIRE warning remains
on for several seconds after the first bottle is deployed, the pilot should
then select the RESERVE extinguisher.

If FIRE warning is still illuminated after several seconds:

  1. FIRE EXTG …………………………………RESERVE
20
Q

ENGINE FIRE - ON THE GROUND

A
  1. PARKING BRAKE ………………………APPLY
  2. FIRE …………………………………………CONFIRM – Smoke, burning odor or warnings from other aircraft or ground crew
  3. AFFECTED ENGINE …………………..IDENTIFY POSITIVELY
  4. THROTTLE (affected engine) ……….STOP
  5. FIRE/ARMED PUSHBUTTON ………PUSH
  6. FIRE EXTG………………………………..MAIN

NOTE
• Pressing the FIRE/ARMED pushbutton and deploying the MAIN
extinguisher should put out most engine fires. If the FIRE warning
remains on for several seconds after the first bottle is deployed, the pilot
should then select the RESERVE extinguisher.

If FIRE is still illuminated after several seconds:

  1. FIRE EXTG ………………………..RESERVE
21
Q

ENGINE FIRE - IN FLIGHT

A
  1. FIRE …………………………………………CONFIRM – Trailing smoke, erratic engine indications, burning odor. If fire cannot be confirmed see
    CONSIDERATION

With fire confirmed:
2. COLLECTIVE …………………………….ADJUST for OEI flight (if required)

  1. AFFECTED ENGINE …………………..IDENTIFY POSITIVELY
  2. THROTTLE (affected engine) ……….STOP
  3. FIRE/ARMED PUSHBUTTON ………IDENTIFY, PUSH
  4. FIRE EXTG………………………………..MAIN

NOTE
• Pressing the FIRE/ARMED pushbutton and deploying the MAIN
extinguisher should put out most engine fires. If the FIRE warning
remains on for several seconds after the first bottle is deployed, the pilot
should then select the RESERVE extinguisher.
If FIRE is still illuminated after several seconds:

  1. FIRE EXTG ………………………..RESERVE
22
Q

POST SHUTDOWN FIRE

A
  1. AFFECTED ENGINE …………………….IDENTIFY POSITIVELY
  2. THROTTLE (affected engine) ………………..STOP
  3. ENG START BUTTON ………………………….PRESS
23
Q

DOOR OPEN - SAR SLIDING DOOR

A
  1. AIRSPEED …………………………………….REDUCE
24
Q

PILOT INCAPACITATION

A
  1. CONTROL THE AIRCRAFT …………Clearly indicate that CONTROL HAS BEEN TAKEN. Ensure aircraft is established on a SAFE FLIGHT
    PATH. COMMAND the AIRCRAFT for
    REMAINDER of the flight
  2. AUTOPILOT ……………………………..COUPLE FLIGHT DIRECTOR MODES if appropriate
  3. INCAPACITATED PILOT ……………Ensure incapacitated pilot is CLEAR OF THE CONTROLS. If possible LOCK his/her SEAT HARNESS. If available, REQUEST CABIN CREW or the assistance of ONE PASSENGER to move the pilot’s seat fully aft with
    his/her feet clear of the pedals.
25
Q

TAIL ROTOR CONTROL FAILURE -

IN A HOVER

A
  1. LAND IMMEDIATELY AND POSITIVELY
  2. ATTITUDE ……………….MAINTAIN with cyclic
  3. GROUNDSPEED / DRIFT …………………….MINIMISE

After ground contact:
4. COLLECTIVE ………………………………..LOWER FULLY

  1. WHEEL BRAKES …………………………………………….APPLY
26
Q

TAIL ROTOR DRIVE

FAILURE - IN A HOVER

A
  1. ATTITUDE …………..MAINTAIN WITH CYCLIC
  2. GROUNDSPEED / DRIFT …………………….MINIMISE
  3. CALLOUT INSTRUCTION ……………………“CUT - CUT - CUT”
  4. THROTTLES ………………………………………STOP (5 to 10 feet)
  5. COLLECTIVE ……………………………………..INCREASE TO CUSHION LANDING

After ground contact:
6. COLLECTIVE ………………………………….LOWER FULLY

  1. BRAKES …………………………………………….APPLY
27
Q

TAIL ROTOR DRIVE FAILURE

- IN THE CRUISE

A
  1. AUTOROTATION ……………………………INITIATE maintain 100-105% NR
  2. AIRSPEED ……………………….MAINTAIN 80-100 KIAS
  3. LOSS OF TAIL ROTOR THRUST ………….CONFIRM
  4. LANDING GEAR ………………………………Select DOWN
  5. THROTTLES ………………….STOP prior to touchdown
  6. PROCEDURE 5/1….FOLLOW Autorotative Landing

Bristow OPC (3 decks)

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