Memory Items, Manoeuvres, Limitations Flashcards
Aborted Engine Start L, R
FUEL CONTROL switch (affected side)…….CUTOFF
Dual Eng Fail/Stall
- FUEL CONTROL switches (both)…CUTOFF, then RUN
- RAM AIR TURBINE switch……………Push and hold
for 1 Second
ENG AUTOSTART L, R
- FUEL CONTROL switch
(affected side)……..Confirm……..CUTOFF
ENG LIMIT EXCEED L, R
- 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
ENG SURGE L, R
- 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
Eng Svr Damage/Sep L, R
- 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
CABIN ALTITUDE
- 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
FIRE ENG L, R
- 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
[ ] STABILIZER
- STAB cutout switches (both) ……………CUTOUT
2. Do not exceed the current airspeed.
[ ] AIRSPEED UNRELIABLE
- 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
Approach to Stall or Stall Recovery
- 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
Ground Proximity Warning System (GPWS) Caution
Correct the flight path or the airplane configuration.
GPWS Warning
PULL UP, OBSTACLE PULL UP, TERRAIN TERRAIN PULL UP
- 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
TCAS TA
- Look for traffic using traffic display as a guide
- If traffic is sighted, manoeuvre if needed.
Windshear Caution
“MONITOR RADAR DISPLAY”
Manoeuvre as required to avoid the windshear
Windshear Warning - TAKEOFF
“WINDSHEAR AHEAD, WINDSHEAR AHEAD”
- prior to V1, reject takeoff
- after V1, perform the Windshear Escape Manoeuver
Windshear Escape Manoeuver
MANUAL FLIGHT: - Disconnect autopilot - Push either TO/GO switch - Aggressively apply maximum thrust - Disconnect autothrottle - Simultaneously roll wings level and rotate toward an initial pitch attitude of 15* - Verify the speedbrakes are retracted - Follow flight director TO/GA guidance AUTOMATIC FLIGHT: - Push either TO/GA switch - Verify TO/GA mode annunciation - Verify GA thrust - Verify the speedbrakes are retracted - Monitor system performance
- Do not change gear or flap configuration until windshear is no longer a factor
- Monitor vertical speed and altitude
- Do not attempt to regain lost airspeed until windshear is no longer a factor.
UPSET - Nose High Recovery
- Recoginize and confirm the developing
- Disconnect autopilot and autothrottle
RECOVER:
- Apply nose down elevator. Apply as much elevator as needed to obtain a nose down pitch rate
- Apply appropriate nose down stabilizer trim
- Reduce thrust
- Roll (adjust bank angle) to obtain nose down pitch rate
COMPLETE THE RECOVERY:
- When approaching the horizon, roll to wings level
- Check airspeed and adjust thrust
- Establish pitch attitude
UPSET - Nose Low Recovery
- Recoginize and confirm the developing
- Disconnect autopilot and autothrottle
RECOVER:
- Recover from stall, if needed
- Roll in the shortest direction to wings level. If bank angle is more than 90*, unload and roll
COMPLETE THE RECOVERY:
- Apply nose up elevator
- Apply nose up trim, if needed
- Adjusted thrust and drag, if needed
Limitations - Max runway slope
+/- 2%
Limitations - Maximum Takeoff and Landing Tailwind Component
15 knots
Limitations - Maximum Operating Altitude
43,100ft
Limitations - Maximum Takeoff and Landing Altitude
14,000ft
Limitations - RVSM
Do not fly in RVSM on ISFD alone.
Prior to takeoff 75ft between captain’s or first officers altitude display and field elevation.
Limitations -Turbulent Air Penetration Speed
- 290KIAS below 25,000ft
- 310KIAS/.84Mach
Limitations - MTOW
254,692kg
Limitations - Maximum Landing Weight
192,776kg
Max Zero Fuel Weight
181,436kg
