Good to know Numbers Flashcards by Glenn Herping

Gross weight with fuel and two souls

12,800 lbs

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One engine thrust, at rest, MIL and MAX

2200, 3300

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Fuel flow for one engine, MAX at rest and Mach 1

7,300, 11,400 pph

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Pushing start arms ignition circuit for ____

30s

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One engine normal oil capacity and air expansion space

4 qt, 1 qt

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Gravity flow guaranteed up to _____

6,000’ MSL

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Fuel cutoff switches is operated by ___ and cuts off fuel in ___

DC, 1s

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Fuel low level light comes on after ___ sec below ___

7.5s, 250lbs

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Gearbox shift occurs at ___ range

65 - 75%

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Voltage of battery is ___V and DC rectifiers are ___V

24, 28

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AC system provides ___/___V power

115/200

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AC generators cut-in between _____

43 - 48%

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Min battery voltage of ___ is required to close battery relay

18 V

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Left engine provides ___ psi for ___ system

3200, utility

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Right engine provides ___ psi for ___ system

3200, flight control

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UTILITY/FLIGHT HYDRAULICS comes on at ___ psi, and goes back out at ___ psi

1500, 1800

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Rudder limited to ___ deg each side when nosegear out 3/4 or less

6°

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Landing gear extension/retraction takes approx ___

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Gear horn and warning light come on when gear not down and locked and ≤____
KCAS, altitude ≤___, and both throttles below ___

210, 10,000’, 96%

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When accelerating, gear light may not go out until ___

240KCAS

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Landing gear alt release pulled out ___ inches, and requires ___ sec

10, 15-35

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Rear canopy follows front by ___ after canopy jettison when pulling the outside D-handle

1 s

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Fuel for left engine is ___ gal serviced/usable and ___ lbs usable

293/286 gal, 1916 lbs

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Fuel for right engine is ___ gal serviced/usable and ___ lbs usable

305/297 gal, 1990 lbs

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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

If EGT doesn't rise w/in ___ sec of fuel flow indication, abort start

Flaps should be +/- ___ of 60% position

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

Abort takeoff if either afterburner doesn't light within ___ sec

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

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

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

Due to oil supply restriction, negative G flight restricted to ___ sec

Rudder system failure may push rudder to ___ deg

Stab aug system failure may push rudder to ___ deg

Touchdown greater than ___ KCAS should not be attempted

200

With asymmetric flaps, maintain ___ kts above final appr/touchdown speed

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

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

Landing light retraction takes ___ sec

AOA max range is ___. Max endurance/best angle of climb is ___

0.18; 0.3

Nozzles should stabilize within ___ sec after rapid throttle movements

``` 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

Controllability check should be accomplished at ___ or higher

6,000' AGL

Maintain ___ KCAS above min controllable airspeed in descent/landing approach

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