TAKE OFF Flashcards
Before calling before take off check
Once “Cabin Secure” do Departure review
depending taxi route and passenger load can be done before
T/O prohibited Brakes amber
RSP: Current weight < GTWO STATUS and MAP selected on the MFD, verbalize “ALL GREEN”, No EICAS, > MIN BRK fuel
PF radar and Pm terrain
Callout is: “Standby” (default configuration) or “Auto”
RSP “AT armed”
“TO” white lsp confirms
Different take off techniques:
Static
Normal
Rolling Takeoff
Tailwind T/O > 13kt = Normal or stattic
Xwind > 30 kt = Normal or static
Captain’s Only Takeoff parameters
- Contaminated runway;
- Windshear reported; and
- Crosswind greater than 25 kts.
- Tailwind above 13 kts
- Training different
Distance for normal vs rolling t/o
Normal Takeoff - increases by approximately 98 feet
Rolling Takeoff - approximately 902 ft
Crosswind >30kts T/O procedure
- Brakes set - 60% - BRK rel - gndsp 20 - AT - TOGA
- For takeoffs with crosswind above 30 kt, the N1 is limited to 60% maximum with ground speed below 20 kt
- 4 degrees prevent ground spoilers
- maintain correction through out roll and rotation
- Maximum Crosswind Component for Takeoff: 36 kt (gust included)
- For takeoffs with crosswind above 30 kt, the N1 is limited to 60% maximum with ground speed below 20 kt.
Note: The use of this method is prohibited on contaminated runways.
FLEX takeoff is cancelled and ATTCS automatically commands RSV thrust if one of the following events occurs:
- Difference between both engine N1 values is greater than 15%;
- OEI (One Engine Inoperative);
- Thrust levers are moved to MAX detent; or
- Windshear is detected.
DERATE takeoff thrust, this method provides larger thrust reductions and may
increase engine life. Less severe operation means lower:
- Fuel flow degradation rate, reducing fuel burn over the on- wing life of engine,
- Inter Turbine Temperature (ITT) degradation rate (Increases time-on-wing),
- Maintenance costs, reducing shop visit rate and cost per shop visit.
Note: The use of this method is prohibited on contaminated runways.
ROLL indication changes to TRACK when the airplane is above
100 KIAS
___will guard the thrust levers until V1 is called.
LSP
displayed during the takeoff if the thrust levers are out of the TO/GA position.
ENG TLA NOT TOGA EICAS message
thrust levers to the TO/GA position before
60 KIAS to get AT HOLD mode, if not advance to TOGA
procedure for LSP to guard the thrust levers as PM
-guard below
-check thrust take over
-V1 off
- gear up RSP on the thrust levers
Abort take off
LSP does it
EICAS message that occurs large pitch or high bank angles on TO/Climb
FUEL 1 (2) LO LEVEL EICAS message.
TSA function is not capable of protecting the airplane from tail strikes due to _____ and needs a speed of _____ at an angle of___
excessive rotation, 30kts, 9.7
Immediate turn
dep limit
-V2 +10 kts
AFE limit
vertical limit of the departure area
The minimum acceleration altitude for Slat/Flap retraction is
400 ft. “F-bug” or Green Dot +10 KIAS.
N1
Climb at V2 +10 KIAS until 800 ft (NADP 1) or 1500 ft (ICAO A) AAE.
Verify VNAV engagement at the height set on MCDU at or above 800 ft (NADP 1) or 1500 ft (ICAO A) AAE.
Verify that climb thrust is set and maintain V2 +10 to 20 KIAS.
At 3000 ft AAE, accelerate and retract SLAT/FLAP on schedule or following the F-BUG.
N2
Climb at V2 +10 KIAS until 800 ft (NADP 2) or 1000 ft (ICAO B) AAE, then accelerate to and maintain VFS
+10 to VFS +20 KIAS (or F-BUG) and retract SLAT/FLAP.
Verify VNAV engagement at the height set on MCDU: at or above 800 ft (NADP 2) or 1000 ft (ICAO B)
AAE. Verify that climb thrust is set and maintain VFS until 3000 ft.
At 3000 ft AAE, accelerate to the enroute climb speed.
ECS OFF Takeoff Procedure
APU is on till after take off checklist
