Flashcards in Takeoff Emergencies Deck (33):
Seat must be adjusted so that the knee can be _____ at full ___ travel
If the flight director bars fail during or immediately after takeoff, cimb out at recommended _____ airspeed for 3 engines and _____ for 4 engines.
3 engine climbout speed (Vco), 3 engine climbout speed plus 10 knots (Vco+10)
A bank angle of 30 degrees at climbout speed with flaps down could reduce climb capability as much as ___.
If an engine failure occurs after attaining Vco, on max mode takeoff, climb at ___ speed
The speed attained at the point of engine failure
Any unusual rolling moment encountered during flap retraction could indicate____
What is the alarm bell signal to prepare for ditching or crash landing?
6 short rings
What is the alarm bell signal for ditching or crash landing?
1 Long ring
Boldface for Crash Landing or Ditching Immediately after takeoff
FLAPS – 50° (P, CP) GEAR – DOWN (UNLESS OVER WATER) (P,CP) THROTTLES – CUTOFF AFTER TOUCHDOWN (P,CP)
The copilot give the “Brace for crash landing” over the ___ position of the interphone and ___ ring(s) of the alarm bell.
If crash landing will occur, pilots must __ on their seats
Lock the inertial reels
If crash landing, pilot must maintain ___ approach speeds and land straight ahead making contact with the ground in ___ attitude.
Appropriate, normal landing attitude
If crash landing, do not cutoff engines prior to ___ as it would cause you to lose ____ and ___
Touchdown, primary electric power and hydraulic pressure
Separation of the nose radome will result in inaccurate indications of: (4 things)
Airspeed, Mach number, altitude, vertical velocity
With EFAS inoperative, Vmcg can increase as much as ____ knots
While still on the runway, don’t advance the throttle on asymmetric engine beyond____
Airspeed indications can exhibit errors during sideslip. ___ knots lower than indicated will exist at ____ degrees of sideslip
7 knots, 10 degrees
During rotation don’t exceed ___ degrees of bank
On wet and icy runways, deviations of up to ____ feet from takeoff path can be expected
Charted Vmcg for dry runway is based on immediate us of ___ and ___
Rudder and nosewheel steering
During actual or simulated engine loss, limit bank to ___ degrees until gear is up and ____ is achieved
15 degrees, maneuvering speed is reached
For an engine failure during takeoff, throttle reduction should not occur prior to ___
Landing gear retraction
Takeoff shouldn’t be attempted if oil pressure is greater than ___psi
In the case of asymmetric flaps, place the flaps in ___ position
The last working
If unable to synchronize flaps, consider ___ and ___ as soon as possible
Fuel dumping, land
When main flaps are retraced and one or both leading edge flaps remain extended the airplane should be flown with caution at load factors in excess of ___gs and in ___ speed range
1.5 gs, 215 and 305 KIAS
Don’t operate ___ and gear simultaneously. Slow operation of __ will result
FWD AR pumps, gear
Don’t operate the ___ and flaps simultaneously. Slow operation of ___ will result
AFT AR pumps, rudder
If leading edge flaps fail to retract when the outboards are raised above ___ degrees you should ___ the ___ spoilers.
6 degrees, cutoff the outboard spoilers
For nose up trim, set inboard spoiler switch to ____ which will give approx. ____ of equivalent trim
Cutoff, 2-3 degrees
If deviation between airspeed indicators occurs then ___ may be used to determine which is more accurate
Speed deviation indicators
On speed indication is equal to ___ AOA
If during a climb all airspeed indicators are inaccurate, continue max climb at ___ degrees of pitch