Good to know Numbers Flashcards
Gross weight with fuel and two souls
12,800 lbs
One engine thrust, at rest, MIL and MAX
2200, 3300
Fuel flow for one engine, MAX at rest and Mach 1
7,300, 11,400 pph
Pushing start arms ignition circuit for ____
30s
One engine normal oil capacity and air expansion space
4 qt, 1 qt
Gravity flow guaranteed up to _____
6,000’ MSL
Fuel cutoff switches is operated by ___ and cuts off fuel in ___
DC, 1s
Fuel low level light comes on after ___ sec below ___
7.5s, 250lbs
Gearbox shift occurs at ___ range
65 - 75%
Voltage of battery is ___V and DC rectifiers are ___V
24, 28
AC system provides ___/___V power
115/200
AC generators cut-in between _____
43 - 48%
Min battery voltage of ___ is required to close battery relay
18 V
Left engine provides ___ psi for ___ system
3200, utility
Right engine provides ___ psi for ___ system
3200, flight control
UTILITY/FLIGHT HYDRAULICS comes on at ___ psi, and goes back out at ___ psi
1500, 1800
Rudder limited to ___ deg each side when nosegear out 3/4 or less
6°
Landing gear extension/retraction takes approx ___
6s
Gear horn and warning light come on when gear not down and locked and ≤____
KCAS, altitude ≤___, and both throttles below ___
210, 10,000’, 96%
When accelerating, gear light may not go out until ___
240KCAS
Landing gear alt release pulled out ___ inches, and requires ___ sec
10, 15-35
Rear canopy follows front by ___ after canopy jettison when pulling the outside D-handle
1 s
Fuel for left engine is ___ gal serviced/usable and ___ lbs usable
293/286 gal, 1916 lbs
Fuel for right engine is ___ gal serviced/usable and ___ lbs usable
305/297 gal, 1990 lbs
Total fuel is ___ gal serviced/usable and ___ lbs usable
598/583 gal, 3906 lbs
With single-engine and less than ___ in either system, leave both boost pumps on and crossfeed on
250 lbs
A minimum of ___ RPM is required to achieve any engine fuel flow (during flight)
12-14%
___% RPM is the heart of airstart envelope at any altitude:
18-20%
Ignition must occur before fuel flow reaches ___
360 lbs/hr
After aborted start, wait ___ min before attempting another start
2
If EGT doesn’t rise w/in ___ sec of fuel flow indication, abort start
12
Flaps should be +/- ___ of 60% position
5%
Normal liftoff speed on initial takeoff is ___
165 KCAS
Delay takeoff a min of ___ minutes behind large aircraft or helicopter and ___ behind heavy aircraft
2; 4
With a xwind > __ knots, spacing behind large/heavy aircraft may be reduced
5
Abort takeoff if either afterburner doesn’t light within ___ sec
5
Final turn speed is ___ plus 1 knot per 100 lb over 1000 lb fuel
180 KCAS
Final appr speed is ___ plus 1 knot per 100 lb over 1000 lb fuel
160 KCAS
Touchdown speed is ___ plus 1 knot per 100 lb over 1000
135 KCAS
Minimum Hydraulic pressure ___
1500 psi
Each generator is ___ phase
3
The O2 low light comes on at or below ___ liter, may blink at or below ___
1; 3
Below __, the engine anti-ice is always open, regardless of switch position
65% RPM
There are ___ rotating beacons, located where ___
2; top of vertical stabilizer and on the lower fuselage
There are ___ position lights, located where ___
4; each wingtip, in the vertical stabilizer, and in the lower fuselage
Battery energizes DC bus for ___
15 min
The radio attenuation switch reduces UHF and VHF volume by ___
66%
IDENT sends a pulse with transponder replies for ___ seconds
15
Standby Al provides ___ deg climb, ___ deg dive, ___ deg roll capacity
92; 78, 360
Standby AI provides ___ minutes of useful info within +/- ___ deg after DC failure
9; 6
Due to oil supply restriction, zero G flight restricted to ___ sec
10
Due to oil supply restriction, negative G flight restricted to ___ sec
30
Rudder system failure may push rudder to ___ deg
30
Stab aug system failure may push rudder to ___ deg
2
Touchdown greater than ___ KCAS should not be attempted
200
With asymmetric flaps, maintain ___ kts above final appr/touchdown speed
20
Do not touchdown at less than ___ KCAS with asymmetric flaps
165
On SE go-around, climb only as necessary until reaching ___ KCAS
200
When landing with all gear up, touch down ___ kts faster than normal
10
Maximum speed for nosewheel on runway
174 KCAS
Anti-ice will cause a loss of ___ % thrust in MIL and ___ in MAX
8.5; 5.5
If flap-slab interconnect fails and flaps needed for landing, ___ % flaps
provides adequate control authority and controllable stick forces
30 - 45%
Pressure reg. maintain cabin alt of ___ +/- ___ from ___ alt.to ___ alt
8,000’; 1,000’
8,000’; 23,000’
Avoid Max thrust dives when below ___ lb in either fuel tank
650
Increase final approach speed and touchdown speed by ___ gust factor
1/2
Estimation for landing roll is ___ ft + fuel weight (not including 1000 ft down)
2,500
Increase final turn, approach and touchdown by ___ KCAS for no flap
15
Landing light retraction takes ___ sec
10
AOA max range is ___. Max endurance/best angle of climb is ___
0.18; 0.3
Nozzles should stabilize within ___ sec after rapid throttle movements
10
Max allowable sink rates for landing: \_\_\_ fpm normal landing and \_\_\_\_ fpm crab landing (full fuel); and \_\_\_\_, \_\_\_\_\_ for < 1700 lbs fuel
340; 200;
590; 395
First 4½” of stick travel provides ___ aileron deflection. Next 1½” of stick travel provides ___ aileron deflection
1/2; full
Crossfeed recommended with fuel imbalance of ___ or greater
200 lbs
Holding airspeed
250 - 265 KCAS
Radar pattern typically burns ___ fuel
325 lbs
Turbulent air/thunderstorm penetration speed is ___ KCAS
280
Climb possible at SETOS is ___ fpm
100 fpm
Climb increased by ___ fpm each kt between SETOS and SETOS + 10 KCAS
8 - 50 fpm
Gear retraction may take ___ when retracted between SETOS+ 10 and 200
1 min
If unable to retract gear, best climb at ___ for 60% flaps, ___ for 0% flaps
200 KCAS; 220 KCAS
Optimum pitch for ejection zoom
20° NH
With loss of canopy, slow to ___ KCAS; min drag occurs at ___ KCAS
300; 225
If one hydr system reads zero, hydr system transfer may occur, and flight time could be limited to ___ min
35
Controllability check should be accomplished at ___ or higher
6,000’ AGL
Maintain ___ KCAS above min controllable airspeed in descent/landing approach
20
Touchdown greater than ___ KCAS should not be attempted
200
Use ___ knots as go/no-go for simple tire failure
100
Normal rotation speed on initial takeoff is ___:
141 (rounded to 145)
Maintain a minimum of ___ RPM to ensure effective anti-ice operation:
80%
Landing roll approximately ___ for no flap landing:
Doubled
If oil pressure is high in cold weather, should be in limits Win ___:
6 min
Minimum/maximum engagement speed for a MA-1 or MA-1A:
60kts / 150kts
Maximum engagement speed for BAK-15:
200 kts
How long does it take to raise a BAK-15:
5 - 7 seconds
