Memory Profiles

Question 1

Aborted Engine Start

Answer 1

1. FUEL CONTROL SWITCH (AFFECTED SIDE)–CUTOFF

Question 2

Airspeed Unreliable

Answer 2

1. AUTOPILOT DISENGAGE SWITCH–PUSH
2. AUTOTHROTTLE (IF ENGAGED)–DISCONNECT
3. F/D SWITCHES (BOTH)–OFF
4. SET THE FOLLOWING GEAR UP PITCH ATTITUDE AND THRUST:
   FLAPS EXTENDED—10° AND 80% N1
   FLAPS UP—4° AND 75% N1

Question 3

APU Fire

Answer 3

1. APU FIRE SWITCH (CONFIRM)–PULL, ROTATE TO THE STOP, AND HOLD FOR 1 SECOND.

Question 4

Cabin Altitude or Rapid Depressurization

Answer 4

1. OXYGEN MASKS–ON
2. CREW COMMUNICATIONS–ESTABLISH
3. CABIN ALTITUDE AND RATE–CHECK
4. 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

Question 5

Dual Engine Failure

Answer 5

1. ENGINE START SELECTORS (BOTH)–FLT
2. THRUST LEVERS (BOTH)–IDLE
3. FUEL CONTROL SWITCHES (BOTH)–CUTOFF, THEN RUN
4. 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
5. APU SELECTOR–START, RELEASE TO ON

Question 6

Engine Fire or Severe Damage or Separation

Answer 6

1. A/T ARM SWITCH–OFF
2. THRUST LEVER (AFFECTED SIDE) CONFIRM–IDLE
3. FUEL CONTROL SWITCH (AFFECTED SIDE) CONFIRM–CUT OFF
4. ENGINE FIRE SWITCH (AFFECTED SIDE) CONFIRM–PULL
5. 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.

Question 7

Engine Limit Or Surge Or Stall

Answer 7

1. A/T ARM SWITCH– OFF
2. THRUST LEVER (AFFECTED SIDE) CONFIRM–RETARD UNTIL INDICATIONS REMAIN WITHIN NORMAL LIMITS OR THE THRUST LEVER IS AT IDLE.

Question 8

Engine Tailpipe Fire

Answer 8

1. FUEL CONTROL SWITCH (AFFECTED SIDE)–CUTOFF

Question 9

Do the ABORTED ENGINE START checklist for one or more of the following abort start conditions:

Answer 9

• 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.

Question 10

Engine warm-up requirements:

Answer 10

Engine oil temperature must be above the BOTTOM of the temperature scale.

Question 11

Engine warm-up recommendations:

Answer 11

• Run the engines for at least 3 minutes

* Use a thrust setting normally used for taxi operations

Question 12

Engine After Landing

Answer 12

Engine cool-down recommendations: • Run the engines for at least 3 minutes.

Question 13

Icing conditions exist when the OAT (on the ground) or TAT (in-flight) is 10 C or below and any of the following exist:

Answer 13

• 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.

Question 14

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:

Answer 14

• 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

Question 15

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,

Answer 15

increase thrust on one engine at a time to a minimum of 70% N1 for 10 to 30 seconds every 10 minutes.