Nice to know numbers Section I

Question 1

Gross weight fully fueled with two crewmembers is approximately

Answer 1

12,700 lbs.

Question 2

Gross weight fully fueled solo is approximately

Answer 2

12,500 lbs.

Question 3

Type engines

Answer 3

J85-GE-5

Question 4

Static thrust in MIL and MAX (pounds)

Answer 4

2,050 and 2,900 lbs.

Question 5

Fuel flow in MAX power at standard day at sea level is _____ at rest and _____ at Mach 1

Answer 5

7,300 and 11,400 lbs./hr.

Question 6

Air conditioning and pressurization uses _____ stage bleed air

Answer 6

8th

Question 7

The start button arms the ignition circuit for _____ sec

Answer 7

30 sec

Question 8

Moving a throttle to MAX energizes the main and afterburner igniters for _____ sec

Answer 8

30 sec

Question 9

Engine oil reservoirs contain _____ quarts with an air expansion space of _____ qt.

Answer 9

4, 1

Question 10

Oil consumption and venting through condensation and aerobatic flight should not exceed

Answer 10

1 pt./hr.

Question 11

Gravity fuel feed in MAX is normally sufficient to _____ft, guaranteed to _____ft, and flameouts have occurred at _____ft.

Answer 11

25k, 6k, 15k

Question 12

The fuel shutoff switches will shut off fuel flow in approximately _____ sec

Answer 12

1

Question 13

The front cockpit fuel indicators have an allowable error of _____lbs for the left system and _____lbs for the right

Answer 13

±47, ±32

Question 14

The rear cockpit fuel indicators should be within _____ lbs of the front cockpit indicators

Answer 14

±25

Question 15

The fuel quantity caution light will illuminate after _____ seconds with a fuel quantity indicator reads below _____

Answer 15

7.5, 275-225

Question 16

A shift mechanism keeps AC generator output between _____ and _____ cycles per seconds

Answer 16

320, 480

Question 17

Gearbox shift occurs in the _____ to _____ RPM range

Answer 17

65%, 75%

Question 18

AC generator output is

Answer 18

115 / 220 volts

Question 19

DC battery output is

Answer 19

28 volts

Question 20

Minimum battery voltage to close the battery relay is

Answer 20

18 volts

Question 21

The static inverter converts DC bus voltage to _____ VAC

Answer 21

115

Question 22

Hydraulic caution lights illuminate at

Answer 22

1500 psi

Question 23

Hydraulic caution lights extinguish at

Answer 23

1800 psi

Question 24

When the nose gear is extended 3/4 or less, rudder is limited to

Answer 24

6°

Question 25

When the nose gear is extended greater than 3/4, rudder is limited to

Answer 25

30°

Question 26

The majority of flap-slab interconnect compensation occurs in the first _____ of flap deflection

Answer 26

35%

Question 27

Normal landing gear extension takes approximately

Answer 27

6 sec

Question 28

Parameters for the gear warning tone and horn are:

Answer 28

Airspeed

Question 29

When airspeed is decreasing the gear warning system is active in the range of _____ to _____ KIAS

Answer 29

210, 180

Question 30

When the system is activated and airspeed is accelerating, the gear warning system may not extinguish until

Answer 30

240 KIAS

Question 31

The landing gear emergency release handle extends approximately

Answer 31

10 in

Question 32

Landing gear emergency extension may take between _____ and _____ seconds

Answer 32

15, 35

Question 33

If possible, avoid opening the canopy when relative wind exceeds _____ kts

Answer 33

30

Question 34

The external canopy jettison D handle must be pulled out _____ ft to jettison canopies

Answer 34

6 ft

Question 35

The external canopy jettison D handle jettisons the front canopy followed byt the rear canopy _____ sec later

Answer 35

1

Question 36

Seat belt automatic opening delay after ejection is

Answer 36

0.65 sec

Question 37

Parachute automatic opening delay is

Answer 37

0.25 sec

Question 38

An aneroid delays parachute opening until between _____ and _____ft

Answer 38

15k, 11.5k

Question 39

During ejection the canopy is jettisoned followed by the seat in

Answer 39

0.3 sec

Question 40

The seat can be adjusted through a vertical range of

Answer 40

5 in

Question 41

The shoulder harness will automatically lock during ejection and / or during a rapid ______ g acceleration

Answer 41

3

Question 42

The seat survival kit contains a life raft attached to a _____ft lanyard

Answer 42

20

Question 43

In AUTO, the survival kit releases ______ sec after parachute deployment

Answer 43

4

Question 44

Total usable fuel (JP-8) is

Answer 44

3,982 lbs.

Question 45

JP-8 weight is _____lbs./gal

Answer 45

6.83