Nice to know numbers Section I Flashcards
Gross weight fully fueled with two crewmembers is approximately
12,700 lbs.
Gross weight fully fueled solo is approximately
12,500 lbs.
Type engines
J85-GE-5
Static thrust in MIL and MAX (pounds)
2,050 and 2,900 lbs.
Fuel flow in MAX power at standard day at sea level is _____ at rest and _____ at Mach 1
7,300 and 11,400 lbs./hr.
Air conditioning and pressurization uses _____ stage bleed air
8th
The start button arms the ignition circuit for _____ sec
30 sec
Moving a throttle to MAX energizes the main and afterburner igniters for _____ sec
30 sec
Engine oil reservoirs contain _____ quarts with an air expansion space of _____ qt.
4, 1
Oil consumption and venting through condensation and aerobatic flight should not exceed
1 pt./hr.
Gravity fuel feed in MAX is normally sufficient to _____ft, guaranteed to _____ft, and flameouts have occurred at _____ft.
25k, 6k, 15k
The fuel shutoff switches will shut off fuel flow in approximately _____ sec
1
The front cockpit fuel indicators have an allowable error of _____lbs for the left system and _____lbs for the right
±47, ±32
The rear cockpit fuel indicators should be within _____ lbs of the front cockpit indicators
±25
The fuel quantity caution light will illuminate after _____ seconds with a fuel quantity indicator reads below _____
7.5, 275-225
A shift mechanism keeps AC generator output between _____ and _____ cycles per seconds
320, 480
Gearbox shift occurs in the _____ to _____ RPM range
65%, 75%
AC generator output is
115 / 220 volts
DC battery output is
28 volts
Minimum battery voltage to close the battery relay is
18 volts
The static inverter converts DC bus voltage to _____ VAC
115
Hydraulic caution lights illuminate at
1500 psi
Hydraulic caution lights extinguish at
1800 psi
When the nose gear is extended 3/4 or less, rudder is limited to
6°
When the nose gear is extended greater than 3/4, rudder is limited to
30°
The majority of flap-slab interconnect compensation occurs in the first _____ of flap deflection
35%
Normal landing gear extension takes approximately
6 sec
Parameters for the gear warning tone and horn are:
Airspeed
When airspeed is decreasing the gear warning system is active in the range of _____ to _____ KIAS
210, 180
When the system is activated and airspeed is accelerating, the gear warning system may not extinguish until
240 KIAS
The landing gear emergency release handle extends approximately
10 in
Landing gear emergency extension may take between _____ and _____ seconds
15, 35
If possible, avoid opening the canopy when relative wind exceeds _____ kts
30
The external canopy jettison D handle must be pulled out _____ ft to jettison canopies
6 ft
The external canopy jettison D handle jettisons the front canopy followed byt the rear canopy _____ sec later
1
Seat belt automatic opening delay after ejection is
0.65 sec
Parachute automatic opening delay is
0.25 sec
An aneroid delays parachute opening until between _____ and _____ft
15k, 11.5k
During ejection the canopy is jettisoned followed by the seat in
0.3 sec
The seat can be adjusted through a vertical range of
5 in
The shoulder harness will automatically lock during ejection and / or during a rapid ______ g acceleration
3
The seat survival kit contains a life raft attached to a _____ft lanyard
20
In AUTO, the survival kit releases ______ sec after parachute deployment
4
Total usable fuel (JP-8) is
3,982 lbs.
JP-8 weight is _____lbs./gal
6.83
