T-38 Dash One Chapter Three

Front 1

ejection seat has the capability for_____altitude/airspeed ejection

Back 1

0/0

Front 2

to preclude injury, hold the canopy breaker tool so that the _______ edge of the blade is towards you

Back 2

curved

Front 3

the effects of tire failure are most pronounced at heavy gross weights and speeds below ____ KCAS

Back 3

100

Front 4

aerodynamic braking is more effective than cautious wheel braking above ______

Back 4

100

Front 5

during heavy gross weight aborts, the nose will lowr at approximately

Back 5

120

Front 6

optimum braking should not be attempted above

Back 6

100

Front 7

aerodynamic braking with less than full flaps or less than ____ degree pitch attitude becomes progressively less effective

Back 7

12

Front 8

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

Back 8

100-130

Front 9

BAK-15 can be used by fighter type aircraft at speeds up to

Back 9

200

Front 10

the BAK 15 should be in position -_______ seconds

Back 10

5-7

Front 11

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 _____

Back 11

60 150 120

Front 12

SETOS is

Back 12

the minimum speed the aircraft can take off and fly out of ground effecgt with a minimum of 100 fpm rate of climb

Front 13

SETOS +10: between SETOS and SETOS+10, single engine climb performance increases at _____ fpm per knot above SETOS

Back 13

8-50

Front 14

SE climb is resricted to _____ until ______. gear should be retracted above ______. flaps raised above _____.

Back 14

minimum necessary 200; SeTOS +10; 200

Front 15

gear retraction with left engine windmilling, when initiated between SETOS+10 and 200 knots may take up to _____

Back 15

1 minute

Front 16

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

Back 16

200 220 220

Front 17

landing gear light and warning horn with ALL THREE of the following conditions:

Back 17

both throttles below 96%, below 10000 feet, and airspeed below 240 KCAS.

Front 18

if unable to raise the landing gear, aircraft will use _____ pounds of fuel per nautical mile

Back 18

10-15 (pounds per nautical mile)

Front 19

configured with full flaps below 220, aircraft will burn _____ at low altitudes

Back 19

60 (pounds per minute)

Front 20

heart of the airstart envelope

Back 20

18-20

Front 21

zoom to eject attitude

Back 21

20 deg NH

Front 22

flap slab interconnect failure requires action within_____ t0 ensure recovery without loss of altitude

Back 22

3 seconds

Front 23

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?

Back 23

30-45%

Front 24

touchdowns at greater than ____ should not be attempted

Back 24

200 KCAS

Front 25

with any structural damage, do not aerobrake. aerobraking could increase normal landing distance by as much as

Back 25

`50%

Front 26

controlled/uncontrolled ejection altitude

Back 26

2000; 15000

Front 27

optimimum speed for ejection

Back 27

200-300 knots

Front 28

loss of canopy slow to below ____. minimum drag occurs at approximately ____.

Back 28

300 225

Front 29

landing gear alternate extension takes approximately

Back 29

15-35 seconds

Front 30

there is a _____ second delay between front and rear seat ejection sequence

Back 30

0.85