Memory Items, Manoeuvres, Limitations Flashcards
1
Q
Aborted Engine Start L, R
A
FUEL CONTROL switch (affected side)…….CUTOFF
2
Q
Dual Eng Fail/Stall
A
- FUEL CONTROL switches (both)…CUTOFF, then RUN
- RAM AIR TURBINE switch……………Push and hold
for 1 Second
3
Q
ENG AUTOSTART L, R
A
- FUEL CONTROL switch
(affected side)……..Confirm……..CUTOFF
4
Q
ENG LIMIT EXCEED L, R
A
- A/T ARM switch
(affected side)…….Confirm………….OFF - Thrust lever
(affected side)…….Confirm………..Retard until
ENG LIMIT EXCEED
message banks or
the thrust lever is at idle
5
Q
ENG SURGE L, R
A
- A/T ARM switch
(affacted side) ………….Confirm…….OFF - Thrust lever
(affected side) ……….Confirm……RETARD until
the ENG SURGE
message blanks or
the thrust lever is at idle
6
Q
Eng Svr Damage/Sep L, R
A
- A/T ARM switch
(affected side) ……………..Confirm……………OFF - Thrust lever
(affected side) ……………..Confirm……………Idle - FUEL CONTROL switch
(affected side) ………………Confirm…………CUTOFF - Engine fire switch ……..Confirm…………Pull
7
Q
CABIN ALTITUDE
A
- Don the oxygen masks.
- Establish crew communications.
- Check the cabin altitude and rate.
- IF the cabin altitude us uncontrollable:
PASS OXYGEN switch…… Push to ON
and hold for 1 secondWITHOUT DELAY, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
To descend:
- Move the thrust levers to idle
- Extend the speedbrakes
- If structural integrity is in doubt, limit airspeed and avoid high manoeuvring loads
- Descend at Vmo/Mmo
8
Q
FIRE ENG L, R
A
- A/T ARM switch……….Confirm………..OFF
- Thrust lever
(affected side) ………….Confirm…………Idle - FUEL CONTROL
switch (affected side)…..Confirm…..CUTOFF - Engine Fire switch
(affected side) ………….Confirm……..Pull - IF the FIRE ENG message stays shown:
Engine fire switch
(affected side)………….Rotate to the stop
and hold for 1 second
9
Q
[ ] STABILIZER
A
- STAB cutout switches (both) ……………CUTOUT
2. Do not exceed the current airspeed.
10
Q
[ ] AIRSPEED UNRELIABLE
A
- Autopilot disconnect switch…….Push
- A/T ARM switches (both) ……….. OFF
- F/D switches (both) ………………… OFF
- Set the following gear up pitch attitude and thrust:
Flaps extended ……………. 10* and 85% N1
Flaps up …………………………..4* and 70% N1
11
Q
Approach to Stall or Stall Recovery
A
- Initiate the recovery:
Smoothly apply nose down elevator
to reduce the angle of attack until buffet or stick shaker stops - Continue the recovery:
Roll in the shortest direction to wings level if needed
Advanced thrust levers as needed
Retract the speedbrakes
Do not change gear or flap configuration, except:
During liftoff, if flaps are up, call for flaps 1. - Complete the recovery:
Check airspeed and thrust as needed
Establish pitch attitude
Return to the desired flight path
Re-engage the autopilot and autothrottle if desired
12
Q
Ground Proximity Warning System (GPWS) Caution
A
Correct the flight path or the airplane configuration.
13
Q
GPWS Warning
PULL UP, OBSTACLE PULL UP, TERRAIN TERRAIN PULL UP
A
- Disconnect autopilot
- Disconnect autothrottle
- Aggressively apply maximum thrust
- Simultaneously roll wings level and rotate to an initial pitch attitude of 20*
- Verify the speedbrakes are retracted
- If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.
- Do not change gear or flap configuration until terrain separation is assured
- Monitor radio altimeter for sustained or increasing terrain separation
- When clear of the terrain, slowly decrease pitch attitude and accelerate
14
Q
TCAS TA
A
- Look for traffic using traffic display as a guide
- If traffic is sighted, manoeuvre if needed.
15
Q
Windshear Caution
“MONITOR RADAR DISPLAY”
A
Manoeuvre as required to avoid the windshear
