Memory items Flashcards
ABORTED ENGINE START
FUEL CONTROL SW (AE) - CUTOFF
AIRSPEED UNRELIABLE
AP DISENGAGE SW - PUSH
AT ARM SW - OFF
FD SW (BOTH) - OFF
SET THE FOLLOWING GEAR UP PITCH ATTIT AND THRUST
FLAPS EXT - 10DEG AND 90% N1
FLAPS UP - 4 DEG AND 80% N1
AUTOMATIC UNLOCK
FLT DECK DOOR LOCK SELECTOR - ROTATE TO DENY AND HOLD FOR 1 SEC
CABIN ALTITUDE
DON THE OXY MASKS
ESTABLISH CREW COMMS
CHECK THE CABIN ALTITUDE AND RATE. VERIFY THE PACKS ARE ON AND THE OUTFLOW VALVES ARE CLOSED
IF THE CABIN ALTITUDE IS UNCONTROLLABLE:
PASS OXY SW - PUSH TO ON and hold for 1 sec
WITHOUT DELAY, DESCEND TO THE LOWEST SAFE ALTITUDE OR 14,000 FT, WHICHEVER IS HIGHER
TO DESCEND: MOVE THE THRUST LEVERS TO IDLE EXT THE SPEEDBRAKES IF STRUCTURAL INTEGRITY IS IN DOUBT, LIMIT AIRSPEED AND AVOID HIGH MAN LOADS DESCEND AT VMO/MMO
ENGINE AUTOSTART
CONDITIONS
CONDITIONS:
AUTOSTART DID NOT START ENGINE
FCSW IN RUN POSITION AT LOW RPM WITH AUTOSTART SW OFF
ENGINE LIMIT OR SURGE OR STALL
THRUST LEVER (AE) - CONFIRM - RETARD UNTIL ENGINE INDICATIONS STAY WITHIN LIMITS, OR THE THRUST LEVER IS AT IDLE
FIRE ENGINE OR ENGINE SEVERE DAMAGE OR SEPARATION
THRUST LEVER (AE) - CONFIRM - IDLE
FUEL CONTROL SW (AE) - CONFIRM - CUTOFF
ENGINE FIRE SW (AE) - CONFIRM - PULL
IF FIRE ENG MSG IS SHOWN
ENGINE FIRE SW (AE) - ROTATE TO THE STOP AND HOLD FOR 1 SEC
IF AFTER 30 SECS, FIRE ENG MSG STAYS SHOWN
ENGINE FIRE SW (AE) - ROTATE TO THE OTHER STOP AND HOLD FOR 1 SEC
FIRE ENG OJU ONLY!!!!
TURBINE OVERHEAT DETECTED
MULTIPLE ENG FLAMEOUT OR STALL OEB-OEJ
FUEL CONTROL SW (AE) - CONFIRM - CUTOFF THEN RUN
IF EGT INCREASES RAPIDLY APPROACHING THE EGT TAKEOFF LIMIT:
REPEAT THE ABOVE STEP AS NEEDED
MULTIPLE ENG FLAMEOUT OR STALL OJU
CON IGNITION SW - ON
FUEL CONTROL SW (AE) - CONFIRM - CUTOFF THEN RUN
IF EGT INCREASES RAPIDLY APPROACHING THE EGT START LIMIT:
REPEAT THE ABOVE STEP AS NEEDED
APPROACH TO STALL OR STALL RECOVERY
INITIATE THE RECOVERY
- HOLD CONTROL COLUMN FIRMLY
- DISENGAGE AP DISCONNECT AT
- SMOOTHLY APPLY NOSE DOWN ELEVATOR TO REDUCE AoA UNTIL BUFFET OR STICK SHAKER STOPS. MAY NEED NOSE DOWN STAB TRIM
CONTINUE THE RECOVERY:
- ROLL SHORTEST DIRECTION TO WINGS LEVEL
- ADV THR LEVERS AS NEEDED
- RETRACT SB
- DO NOT CHANGE CONFIG
- – DURING LIFTOFF, IF FLAPS ARE UP, CALL FOR F1
COMPLETE RECOVERY:
- CHECK AIRSPEED AND ADJUST THR AS NEEDED
- ESTABLISH PITCH ATTIT
- RETURN TO DESIRED FLIGHT PATH
RE-ENGAGE AP AND AT AS NEEDED
REASONS FOR REJECTED TAKEOFF
CALL ‘STOP’
PRIOR 80KTS: ACTIVATION OF MASTER CAUTION SYS SYS FAILURE UNUSUAL NOISE OR VIBRATION TYRE FAILURE ABNORMALLY SLOW ACCEL TAKEOFF CONFIG WARNING FIRE OR FIRE WARNING ENGINE FAILURE PWS AIRPLANE UNSAFE OR UNABLE TO FLY
>80KTS BUT BEFORE V1 FIRE OR FIRE WARNING ENGINE FAILURE PWS AIRPLANE UNSAFE OR UNABLE TO FLY
RTO ACTIONS CAPT
SIMULT CLOSE THR LEVERS, DISCONNECT AT, AND APPLY MAX MANUAL BRAKING OR VERIFY OPERATION OF RTO BRAKING
IF RTO AUTOBRAKE SELECTED, MONITOR SYS PERFORMANCE AND IF ‘AUTOBRAKES’ MSG DISPALYED OR DECELERATION NOT ADEQUATE
RAISE SPEEDBRAKE LEVER
APPLY MAX REV ON SYMMETRIC ENGINES
CONTINUE MAX BRAKING UNTIL CERTAIN AIPLANE WILL STOP ON RUNWAY
RTO ACTIONS FO
VERIFY ACTIONS AS FOLLOWS: THR LEVERS CLOSED AT DISCONNECT MAX BRAKES APPLIED VERIFY SPEEDBRAKES 'UP' OR 'NOT UP' REV THR SYMMETICAL 'REVERSERS NORMAL' OR 'NO REVERSER NUMBER (?)' CALL 'AUTOBRAKES' WHEN EICAS MSG CALL OUT ANY OMMITTED ITEMS
80KTS
60KTS
ADVISE TWR AND CABIN
FO DOES ALERT PA
GPWS RECOVERY
DISENGAGE AP
DISCONNECT AT
AGGRESSIVELY APPLY MAX THR
SIMULT ROLL WINGS LEVEL AND PITCH TO 20DEG
RETRACT SB
IF TERRAIN REMAINS A THREAT, CONTINUE ROTATION TO PLI, STICK SHAKER OR BUFFET
DO NOT CHANGE GEAR OR FLAP CONFIG UNTIL TERRAIN SEP IS ASSURED
MONITOR RADIO ALTIMETER FOR SUSTAINED OR INCREASING TERRAIN SEP
WHEN CLEAR OF TERRAIN, SLOWLY DECREASE PITCH ATTIT AND ACCEL
AFTER RECOVERY MAN, CHECK A/C POSN AND MSA/LSALT
