T-38 See Description

Front 1

LDG gear extension / retraction take __ sex

Back 1

6

Front 2

GEAR warning tone when airpseed is below ___ KCAS, altitude below __ feet, and BOTH throttles below ___ %

Back 2

210, 10000, 96

Front 3

with a ___ electric failure, rear cockpit ___ gear light does not illuminate due to gear wiring

Back 3

DC, nose

Front 4

Alt gear extention takes __ to __ sex

Back 4

15, 35

Front 5

with nose gear 3/4 or less, rudder deflection is __ degrees from neutral. 3/4 or more, ___ degrees

Back 5

6, 30

Front 6

Rudder trim switch can move the rudder __ degrees in either direction

Back 6

2

Front 7

the majority of the flap slab compensation occurs in the first ___ % of flap deflection

Back 7

35

Front 8

cabin pressure is 0 psi from SL to ___ feet

Back 8

8000

Front 9

cabin pressure is 8000 +-1000 from__ to ___ feet

Back 9

8000, 23000

Front 10

cabin pressure is ___ psi above ambient pressure (+_2000) above ___ feet

Back 10

5, 23000

Front 11

At engine speeds of __ to __ RPM, an increase in EGT of ___ *C is normal with Anti Ice switch MAN ON

Back 11

94, 98, 15

Front 12

below ___ % RPM, the anti-ice valve is always open

Back 12

65

Front 13

with engine anti ice switch on you lose ___ +- ___ pounds of thrust

Back 13

180, 10

Front 14

with engine anti ice switch on you lose approx ___ % thrust at MIL and ___% in MAX

Back 14

8.5, 5.5

Front 15

a birdstrike at ___ knots on the windscreen can impact the HUD and shatter it

Back 15

400

Front 16

avoid opening the canopy when relative wind exceeds __ Knots

Back 16

30

Front 17

an aneroid delays parachute from opening until between ___ and ___ feet pressure altitude when free falling

Back 17

13000, 11500

Front 18

oxygen low light comes on at __ liter. the light may blink due to system sloshing at ___ liters

Back 18

1, 3