Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
30 Cards in this Set
- Front
- Back
ejection seat has the capability for_____altitude/airspeed ejection
|
0/0
|
|
to preclude injury, hold the canopy breaker tool so that the _______ edge of the blade is towards you
|
curved
|
|
the effects of tire failure are most pronounced at heavy gross weights and speeds below ____ KCAS
|
100
|
|
aerodynamic braking is more effective than cautious wheel braking above ______
|
100
|
|
during heavy gross weight aborts, the nose will lowr at approximately
|
120
|
|
optimum braking should not be attempted above
|
100
|
|
aerodynamic braking with less than full flaps or less than ____ degree pitch attitude becomes progressively less effective
|
12
|
|
cautious wheel braking must be exercised when applying wheel brakes between _____ as locked wheels or tire skids are difficult to recognize. If one is detected, immeditately release both brakes and cautiously reapply
|
100-130
|
|
BAK-15 can be used by fighter type aircraft at speeds up to
|
200
|
|
the BAK 15 should be in position -_______ seconds
|
5-7
|
|
for MA-1/MA-1A barriers the minimum engagement speed is ____, the designed dynamic limit is ____ for all aircraft and expect nose or main gear failure above _____
|
60 150 120
|
|
SETOS is
|
the minimum speed the aircraft can take off and fly out of ground effecgt with a minimum of 100 fpm rate of climb
|
|
SETOS +10: between SETOS and SETOS+10, single engine climb performance increases at _____ fpm per knot above SETOS
|
8-50
|
|
SE climb is resricted to _____ until ______. gear should be retracted above ______. flaps raised above _____.
|
minimum necessary 200; SeTOS +10; 200
|
|
gear retraction with left engine windmilling, when initiated between SETOS+10 and 200 knots may take up to _____
|
1 minute
|
|
if landing gear is stuck down, best climb capability is ____ with 60 flaps and _____ with flaps up. At high gross weight with landing gear extended, do not retract flaps above _____ knots
|
200 220 220
|
|
landing gear light and warning horn with ALL THREE of the following conditions:
|
both throttles below 96%, below 10000 feet, and airspeed below 240 KCAS.
|
|
if unable to raise the landing gear, aircraft will use _____ pounds of fuel per nautical mile
|
10-15 (pounds per nautical mile)
|
|
configured with full flaps below 220, aircraft will burn _____ at low altitudes
|
60 (pounds per minute)
|
|
heart of the airstart envelope
|
18-20
|
|
zoom to eject attitude
|
20 deg NH
|
|
flap slab interconnect failure requires action within_____ t0 ensure recovery without loss of altitude
|
3 seconds
|
|
with flap slab interconnect failure, a no flap landing is preferred. however if flaps are required what setting provides limited but adequate nose down control authority and manageable stick forces?
|
30-45%
|
|
touchdowns at greater than ____ should not be attempted
|
200 KCAS
|
|
with any structural damage, do not aerobrake. aerobraking could increase normal landing distance by as much as
|
`50%
|
|
controlled/uncontrolled ejection altitude
|
2000; 15000
|
|
optimimum speed for ejection
|
200-300 knots
|
|
loss of canopy slow to below ____. minimum drag occurs at approximately ____.
|
300 225
|
|
landing gear alternate extension takes approximately
|
15-35 seconds
|
|
there is a _____ second delay between front and rear seat ejection sequence
|
0.85
|