Memory Actions Flashcards
BOOST HARDOVERS
- AIRCRAFT ATTITUDE ………………..CONTROL
FD DEGRADED - BELOW 50 KIAS
SAR ONLY
- AIRCRAFT ATTITUDE ……………….CONTROL
JAMMED OR RESTRICTED
FLIGHT CONTROLS
- AIRCRAFT ATTITUDE ……………….CONTROL
SAS HARDOVERS
- AIRCRAFT ATTITUDE ……………….CONTROL
TRIM HARDOVERS
- AIRCRAFT ATTITUDE …………………………CONTROL using cyclic and collective trim releases
AC GENERATOR
FAILURE (DUAL)
- APU CTRL ………………………………………….ON
- APU GEN …………………………………………..ON
- AC GEN NO 1 and NO 2 ……..RESET / OFF then ON
DC (DUAL) AND
BACKUP CONVERTER FAILURE
- DC CONV BACKUP …………………………….OFF (to recover intercom)
- DC CONV 1 AND DC CONV 2 …………… RESET/OFF THEN ON
AUTOROTATIVE LANDING (PF)
- AUTOROTATION …………
INITIATE AND ESTABLISH - 80-100 KIAS/105% Nr - SEARCH LIGHT ……………..ON / ADJUST if required
- FLARE ……………………………….AT ~100 FT AGL to decrease airspeed and sink rate, and increase Nr.
- NOSE UP ATTITUDE …………..REDUCE TO MAXIMUM 10° as the flare loses effectiveness and the helicopter starts to settle
- 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.
- FLOTATION GEAR………………DEPLOY immediately after water contact
- FLIGHT CONTROLS ……………DECREASE collective and NEUTRALISE cyclic immediately after landing
- WHEEL BRAKES ………………..APPLY as required
AUTOROTATIVE LANDING (PM)
- APU …………………………………..START
- THROTTLES AND FUEL………AS REQUIRED
- LANDING GEAR …………………DOWN
- PASSENGERS ……………………“BRACE, BRACE, BRACE”
- FLOTATION GEAR………………ARM below 80 KIAS (if over water)
- RADALT……………………………..CALL below 1000 ft
- AIRCRAFT …………………………EVACUATE when rotors stopped
PROCEDURE 5/2 - On Land, or
PROCEDURE 5/3 - On Water
ENGINE FAILURE (SINGLE) - IN A HOVER
- COLLECTIVE …………………………….MAINTAIN collective setting
- COLLECTIVE …………………………….INCREASE to cushion landing
- AFTER TOUCHDOWN ………………..NEUTRALISE CYCLIC and REDUCE COLLECTIVE to minimum
- WHEEL BRAKES ……………………….APPLY
ENGINE FAILURE (SINGLE) - BEFORE OR AT TDP
- FLY BRIEFED OEI REJECT PROFILE
ENGINE FAILURE (SINGLE) - AFTER TDP
- CONTINUE TO FLY BRIEFED OEI TAKE-OFF PROFILE
ENGINE FAILURE (SINGLE ) - IN THE CRUISE
1.COLLECTIVE ………………………………….ADJUST to maintain desired Nr while transitioning to OEI airspeed
WARNING
• Do not select two minute power until obstacle clearance is assured.
- OEI POWER ……………………………………….SELECT 2 MINUTE and MCP when conditions permit
- RIPS ………………………………………………….If in icing conditions, consider selecting manual HEAVY mode
as required
ENGINE FAILURE (SINGLE ) - BEFORE OR AT LDP - BALKED LANDING (GO AROUND)
- FLY BRIEFED OEI BALKED LANDING PROFILE
ENGINE FAILURE (SINGLE) - AFTER LDP - SINGLE ENGINE LANDING
- FLY BRIEFED OEI LANDING PROFILE
ENGINE FAILURE (DUAL) - IN A HOVER
- AIRCRAFT ATTITUDE …….MAINTAIN LEVEL
- COLLECTIVE ……………………………………..INCREASE to cushion landing
After touchdown:
- CYCLIC ……………………………………………..SLIGHTLY FORWARD OF CENTRE
- COLLECTIVE ……………………………………..FULLY DOWN
- BRAKES …………………………………………….APPLY as required
ENGINE FAILURE (DUAL) -
IN FORWARD FLIGHT
- AUTOROTATION…………………………….INITIATE MAINTAIN 100 -105% Nr
- AIRSPEED ………………………………………ESTABLISH between 80-100 KIAS
- LANDING GEAR ……………………………..Select DOWN
- THROTTLES …………………………………….STOP
- APU ……………………………………………….ON
If time, altitude & probability of success exists
- RESTART ………………………………….ONE OR BOTH ENGINES ATTEMPT
If neither engine will start
- PROCEDURE 5/1 ……………….FOLLOW - Autorotative Landing
ENGINE HIGH SPEED SHAFT FAILURE
- AFFECTED ENGINE ………………………IDENTIFY POSITIVELY
- THROTTLE (affected engine) ………………..IDLE, PAUSE, STOP
APU FIRE
1.FIRE ……………………………………………..CONFIRM
If fire cannot be confirmed see CONSIDERATION
With fire confirmed:
- APU CTRL ………………………………………….OFF
- APU FIRE/ARMED PUSHBUTTON….IDENTIFY/PUSH
- 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:
- FIRE EXTG …………………………………RESERVE
ENGINE FIRE - ON THE GROUND
- PARKING BRAKE ………………………APPLY
- FIRE …………………………………………CONFIRM – Smoke, burning odor or warnings from other aircraft or ground crew
- AFFECTED ENGINE …………………..IDENTIFY POSITIVELY
- THROTTLE (affected engine) ……….STOP
- FIRE/ARMED PUSHBUTTON ………PUSH
- 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:
- FIRE EXTG ………………………..RESERVE
ENGINE FIRE - IN FLIGHT
- 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)
- AFFECTED ENGINE …………………..IDENTIFY POSITIVELY
- THROTTLE (affected engine) ……….STOP
- FIRE/ARMED PUSHBUTTON ………IDENTIFY, PUSH
- 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:
- FIRE EXTG ………………………..RESERVE
POST SHUTDOWN FIRE
- AFFECTED ENGINE …………………….IDENTIFY POSITIVELY
- THROTTLE (affected engine) ………………..STOP
- ENG START BUTTON ………………………….PRESS
DOOR OPEN - SAR SLIDING DOOR
- AIRSPEED …………………………………….REDUCE
PILOT INCAPACITATION
- 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 - AUTOPILOT ……………………………..COUPLE FLIGHT DIRECTOR MODES if appropriate
- 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.
TAIL ROTOR CONTROL FAILURE -
IN A HOVER
- LAND IMMEDIATELY AND POSITIVELY
- ATTITUDE ……………….MAINTAIN with cyclic
- GROUNDSPEED / DRIFT …………………….MINIMISE
After ground contact:
4. COLLECTIVE ………………………………..LOWER FULLY
- WHEEL BRAKES …………………………………………….APPLY
TAIL ROTOR DRIVE
FAILURE - IN A HOVER
- ATTITUDE …………..MAINTAIN WITH CYCLIC
- GROUNDSPEED / DRIFT …………………….MINIMISE
- CALLOUT INSTRUCTION ……………………“CUT - CUT - CUT”
- THROTTLES ………………………………………STOP (5 to 10 feet)
- COLLECTIVE ……………………………………..INCREASE TO CUSHION LANDING
After ground contact:
6. COLLECTIVE ………………………………….LOWER FULLY
- BRAKES …………………………………………….APPLY
TAIL ROTOR DRIVE FAILURE
- IN THE CRUISE
- AUTOROTATION ……………………………INITIATE maintain 100-105% NR
- AIRSPEED ……………………….MAINTAIN 80-100 KIAS
- LOSS OF TAIL ROTOR THRUST ………….CONFIRM
- LANDING GEAR ………………………………Select DOWN
- THROTTLES ………………….STOP prior to touchdown
- PROCEDURE 5/1….FOLLOW Autorotative Landing
