TOLD Flashcards
Define takeoff distance
Distance in feet from brake release to main gear liftoff
Define critical field length
Total runway length required to accelerate with both engines operating to critical engine failure speed, have an engine failure and either continue to SETOS (approx 700’ from start of rot at SETOS) or stop in same distance
Define refusal speed
Max speed to which the aircraft is able to accel in MAX with both engines operating and abort. There is an RS-BEO and RS-EF (both engines operating and engine failure)
Define SETOS
Speed at which the ac is able to climb, once clear of the ground effect, at a minimum of 100’/NM with gear down, flaps 60%
Define critical engine failure speed (CEFS)
Speed to which the ac accelerates with both engines, experiences an engine fail and permits either accel to SETOS and takeoff or stop in same distance
Define decision speed (DS)
Min speed at which the ac is able to experience instantaneous engine fail and still accel to SETOS and takeoff in the remaining runway
Define rotation speed
The speed at which aft stick is initiated
What are CFL assumptions?
Valid up to SETOS
Assumes no aerobrake
What are RS assumptions?
3 s to recognize and pull throttles to idle
Wheel braking not used w aerobraking, applied when NW on grd in 2 s
Accel continues at MAX with either one windmilling or both still at MAX
Nosewheel stays off rwy until 120 kts then settles at 120 kts
Attitude of 7.5 deg NH held if rotated
During BEO both engines produce idle thrust; during EF one is windmilling
Aerobrake not assumed
Braking cautious 135 to 100, optimum at 100
What are SETOS assumptions?
- Rotation is started at SETOS during single engine TO
- Min SETOS is 2-engine takeoff speed
- Accel to SETOS in 3 pt attitude
- Delaying rotation improves performance
- Best rate of climb with gear, flaps 60% is 200 kts at #12,800 220 kts with gr dn flaps up
What are CEFS assumptions?
DS assumptions apply if accel to SETOS
RS assumptions apply if aborting
CEFS valid up to SETOS
Aerobrake not assumed
What are DS assumptions?
- 3 sec delay to react, in which engines stay one MAX other windmilling
- if ac hits rotation speed during time, rotation attitude is set
- after 3 sec ac maintains or returns to a 3 point attitude to accel to SETOS w neutral stick
Define NACS
Normal Accel Check Speed
Approximate speed an ac will reach at a predetermined distance down the runway
What are NACS assumptions?
Normal accel
Check distance must be less than go/no-go speed
Define MACS
Min Accel Check Speed
min acceptable speed at check distance with which TO continued