Memory Profiles Flashcards
Aborted Engine Start
- FUEL CONTROL SWITCH (AFFECTED SIDE)–CUTOFF
Airspeed Unreliable
- AUTOPILOT DISENGAGE SWITCH–PUSH
- AUTOTHROTTLE (IF ENGAGED)–DISCONNECT
- F/D SWITCHES (BOTH)–OFF
- SET THE FOLLOWING GEAR UP PITCH ATTITUDE AND THRUST:
FLAPS EXTENDED—10° AND 80% N1
FLAPS UP—4° AND 75% N1
APU Fire
- APU FIRE SWITCH (CONFIRM)–PULL, ROTATE TO THE STOP, AND HOLD FOR 1 SECOND.
Cabin Altitude or Rapid Depressurization
- OXYGEN MASKS–ON
- CREW COMMUNICATIONS–ESTABLISH
- CABIN ALTITUDE AND RATE–CHECK
- IF THE CABIN ALTITUDE IS UNCONTROLLABLE:
PASS OXY SWITCH—PUSH AND HOLD FOR 1 SECOND
WITHOUT DELAY, DESCEND TO THE LOWEST SAFE ALTITUDE OR 10,000 FEET, WHICHEVER IS HIGHER
TO DESCEND:
MOVE THE THRUST LEVERS TO IDLE
EXTEND THE SPEEDBRAKE
IF STRUCTURAL INTEGRITY IS IN DOUBT, LIMIT AIRSPEED AND AVOID HIGH MANEUVERING LOADS
DESCEND AT Vmo/Mmo
Dual Engine Failure
- ENGINE START SELECTORS (BOTH)–FLT
- THRUST LEVERS (BOTH)–IDLE
- FUEL CONTROL SWITCHES (BOTH)–CUTOFF, THEN RUN
- IF ENGINE APPEARS STALLED OR EGT APPROACHES THE STANDBY ENGINE INDICATOR PLACARD LIMIT:
FUEL CONTROL SWITCH (AFFECTED ENGINE) CONFIRM—CUTOFF, THEN RUN
IF ENGINE APPEARS STALLED AGAIN OR EGT APPROACHES THE STANDBY ENGINE INDICATOR PLACARD LIMIT, REPEAT AS NEEDED - APU SELECTOR–START, RELEASE TO ON
Engine Fire or Severe Damage or Separation
- A/T ARM SWITCH–OFF
- THRUST LEVER (AFFECTED SIDE) CONFIRM–IDLE
- FUEL CONTROL SWITCH (AFFECTED SIDE) CONFIRM–CUT OFF
- ENGINE FIRE SWITCH (AFFECTED SIDE) CONFIRM–PULL
- IF THE ENGINE FIRE WARNING LIGHT IS ILLUMINATED:
ENGINE FIRE SWITCH (AFFECTED SIDE)–ROTATE TO THE STOP AND HOLD FOR ONE SECOND
IF, AFTER 30 SECONDS, THE ENGINE FIRE WARNING LIGHT STAYS ILLUMINATED:
ENGINE FIRE SWITCH (AFFECTED SIDE)–ROTATE TO THE OTHER STOP AND HOLD FOR ONE SECOND.
Engine Limit Or Surge Or Stall
- A/T ARM SWITCH– OFF
- THRUST LEVER (AFFECTED SIDE) CONFIRM–RETARD UNTIL INDICATIONS REMAIN WITHIN NORMAL LIMITS OR THE THRUST LEVER IS AT IDLE.
Engine Tailpipe Fire
- FUEL CONTROL SWITCH (AFFECTED SIDE)–CUTOFF
Do the ABORTED ENGINE START checklist for one or more of the following abort start conditions:
- The EGT does not increase by 25 seconds after the fuel control switch is moved to RUN. .
- There is no N1 rotation by 30 seconds after N2 is stabilized at idle.
- The EGT quickly nears or exceeds the START LIMIT.
- The OIL PRESSURE indication is not normal by the time that the engine is stabilized at idle.
Engine warm-up requirements:
Engine oil temperature must be above the BOTTOM of the temperature scale.
Engine warm-up recommendations:
- Run the engines for at least 3 minutes
* Use a thrust setting normally used for taxi operations
Engine After Landing
Engine cool-down recommendations: • Run the engines for at least 3 minutes.
Icing conditions exist when the OAT (on the ground) or TAT (in-flight) is 10 C or below and any of the following exist:
- visible moisture (clouds, fog with visibility of 1 SM (1600 m) or less, due to meteorological conditions such as rain, snow, sleet and ice crystals, or
- ice, snow, slush or standing water is present on the ramps, taxiways, or runways.
CAUTION: Do not use engine anti-ice when OAT (on the ground) is above 10°C. Do not use engine or wing anti-ice when TAT (in-flight) is above 10°C.
When engine anti-ice is required and the OAT is 3°C or below, do an engine run up, as needed, to minimize ice build-up. Use the following procedure:
- Check that the area behind the airplane is CLEAR.
- Run-up to a minimum of 60% N1 for approximately 30 seconds duration at intervals no greater than 30 minutes
During flight in moderate to severe icing conditions for prolonged periods with N1 settings at or below 70%, or if fan icing is suspected due to high engine vibration,
increase thrust on one engine at a time to a minimum of 70% N1 for 10 to 30 seconds every 10 minutes.
