Other Memory Items Not Official Flashcards
Aircraft Upset Parameters
Pitch Attitude > 25deg nose up
Pitch attitude > 10deg nose down
Bank angle > 45deg
Within the above but at an airspeed inappropriate for the conditions
Nose High Recovery
Recognize and Confirm Disengage Autopilot and disconnect Autothrottle Apply as much as full nose down elevator Apply appropriate nose down Trim Reduce thrust Roll to obtain a nose down pitch rate Complete the recovery - approaching the horizon roll to wings Level - check airspeed and adjust Thrust - establish pitch attitude
Nose low Recovery
Recognize and Confirm Disengage Autopilot and disconnect Autothrottle Recover from Stall if required Roll in the shortest direction to wings level ( unload and roll if bank angle is > 90deg ) Recover to level flight - apply nose up elevator - apply nose up Trim if required - adjust thrust and drag as required
Flight reference both engine
280000lbs
GEAR UP
Flaps Up/ level/ 210kias/ 3000ft
4.5deg ~ 59%N1
Flaps 1/ level/ 195Kias/ 3000ft
6deg ~ 61% N1
Flaps 5/ level/ 175Kias/ 1500ft
4.5deg ~ 62% N1
GEAR DOWN
Flaps 20/ level/ 155Kias/ 1500ft
4.5deg ~ 68%
Flaps 30/ level/ 140Kias/ 1500ft
5deg ~ 74%
Flaps 30/ 3deg ILS Final/ HW 7kt
2.5 to 3deg ~ 61-62%
Flaps 20 Abnormal landing/ 3deg ILS Final
VREF20+5/ 2.5deg ~ 50%N1
Flight Reference Single Engine
280000lb
GEAR UP
Flap Up/ level/ 3000ft/ 210kt
4deg ~ 76%N1
Flap 1/ level/ 195Kias/ 3000ft
6deg ~ 80%
Flap 5/ level/ 175KIAS/ 2000ft
5deg ~ 81%
Flap 5/ Des 1000fpm/ 174Kias/ 2000ft
2deg ~ 49%
Des 500fpm/3000-1500
3deg ~69%
GEAR DOWN
Flap 20/ 3deg ILS Final/ HW 7kts/ 149Kias
2.5 ~ 69%
Add 2-3%for each 10kt headwind and slight increase in pitch attitude to approx 3deg with 20kts HW
Flap placard speed
Flap 767-300 767-300ER 1 245kt 250kt 5 225kt 230kt 15 205kt 210kt 20 205kt 210kt 25 175kt 180kt 30 165kt 170kt
Flap manouvre speeds
0 - Vref 30+80 1 - Vref30+60 5 - Vref30+40 15/20 - Vref30+20 25 - Vref25 30 - Vref30
Weights 767-300
Max Taxi Wt 290700lb
MTOW. 288700lb
MLW. 280000lb
MZFW. 278000lb
What limits Mmo
High speed limit by shock wave
What limits Vmo
High speed limit by air load
What is VA
Maximum speed for maximum pitch control
You do not exceed the max load acceleration limits ( -1G to 2.5G flap up ) at design weight ( MTOW )
Landing gear placard speed
Normal system
Retraction 270kt
Extension 270kt/ .82M
Alternate system
Extension 250kt/ .75M
- Extended VLE : 270kt/ .82M
Runway slope limit
+ or - 2%
Max operating pressure Altitude
43100ft
Max Takeoff and landing pressure Altitude
8400ft