Dash 1 Ch 1 Flashcards by Mads-Emil Zinckernagel

One engine thrust, MIL and MAX:

2200/3300

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

7300, 11,400 lb/hr

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Pushing start arms ignition circuit for ___

30 sec

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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 ___ alt:

6,000

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Fuel cutoff switches operated by ___ and cut off fuel in ___:

DC, 1 sec

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Fuel low level light comes on after ___ sec below ___ amount

7.5. 250 lbs

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Gearbox shift occurs at ___ range:

65-75%

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Voltage of battery is ___V and of DC rectifiers is ___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 batt 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, flt control

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Hyd low press 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 deg

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Landing gear extension/retraction takes approx ___:

6 sec

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Gear horn and warning light come on when gear not down and locked and ____ kts or less, attitude ___ or below, and both throttles below ___:

210 kts, 10,000, 96%

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When accelerating, gear light may not go out until ___:

240 kts

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

10 in, 15-35 sec

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Rear canopy follows front by ___ after canopy jettison:

1 sec

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Aneroid delays parachute opening until between ___:

15,000 to 11,500

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Seat ejection occurs ___ after canopy jettison:

0.3 sec

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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

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

12-14%

___% RPM is the heart of airstart envelope at any altitude:

18-20%

Ignition must occur before fuel flow reaches ___:

360 lb/hr

After aborted start, wait ___ min before attempting another start:

2 min

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

12 sec

Flaps should be +/- ___ of 60% position:

Normal rotation speed on initial takeoff is ___:

141 KIAS (this is rounded to 145)

Normal liftoff speed on initial takeoff is ___:

165 KIAS

Delay takeoff a min of ___ minutes behind large and ___ behind heavy aircraft

2, 4

With a xwind > __ knots, spacing behind large/heavy aircraft can be reduced

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

Final turn speed is ___ plus I knot per 100 lb over 1000 lb fuel:

180 KIAS

Final appr speed is ___ plus I knot per 100 lb over 1000 lb fuel:

160 KIAS

Touchdown speed is ___ plus I knot per 100 lb over 1000 lb:

135 KIAS

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 liters

Below __, the engine anti-ice is always open, regardless of switch position:

65 % RPM

There are ___ rotating beacons, located where ___:

2, tail/lower fuselage

Battery energizes DC bus for ___:

15 minutes at 80% power

If oil pressure is high in cold weather, should be in limits Win ___:

6 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, and provides ___ minutes of useful info within +/- ___ deg after DC failure:

92, 78, 360 deg, 9 min, + 6 deg

Maintain a minimum of ___ RPM to ensure effective anti-ice operation:

80% RPM

Due to oil supply restriction, zero G flight restricted to ___ sec:

10 sec

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

30 sec

Rudder system failure may push rudder to ___ deg

30 deg

Stab aug system failure may push rudder to ___ deg

2 deg

Touchdown greater than ___ KCAS should not be attempted

200 kts

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

20 kts;

Do not touchdown at less than ___ kts with asymmetric flaps:

165 kts

On SE go-around, climb only as necessary until reaching ___ kts:

200 kts

When landing with all gear up, touch down ___ kts faster than normal:

10 kts

Maximum speed for nosewheel on runway:

174 kts

Estimation for landing roll is ___ ft + fuel (not including 1000 ft down):

2500 ft

Landing roll approximately ___ for no flap landing:

doubled

Anti-ice will cause a loss of ___ % thrust in MIL and ___ in MAX:

8.5%, 5.5%

If flab-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:

8000 +/- 2000, 8 to 23

Avoid Max thrust dives when below ___ lb in either fuel tank:

650

Use ___ knots as go/no-go for simple tire failure:

100 kts

Increase final approach speed and touchdown speed by ___ gust factor:

Increase final turn, approach and touchdown by ___ kts for no flap:

15 kts

How many seconds until full parachute deployment:

3.42 sec

Landing light retraction takes ___ sec:

10 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:

10 sec

Max allowable sink rates for landing: ___ fpm normal landing and ____ fpm crab landing (>1700 lbs fuel); and ____, _____ for

340, 200, 590, 395

First 4½ " of stick travel provides ___ aileron deflection, Next 1½ " of stick travel provides ___ aileron deflection:

50% , Full

Crossfeed recommended with fuel imbalance of ___ or greater:

200 lbs

Holding airspeed:

250-265 kts

Radar pattern typically burns ___ fuel:

325 lbs

Turbulent air/thunderstorm penetration speed is ___ kts:

280 kts

Climb possible at SETOS is ___ fpm:

100 fpm.

Climb increased by ___ fpm each kt between SETOS - SETOS + 10:

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 kts, 220 kts

Optimum pitch for ejection zoom:

20 deg

With loss of canopy, slow to ___ kts; min drag occurs at ___ kts:

300, 225 kts

If one hydr system reads zero, hydr system transfer may occur, and flight time could be limited to ___ min:

35 min

Controllability check should be accomplished at ___ AGL or higher:

6,000 ft

Maintain ___ kts above min controllable airspeed in descent/landing approach:

20 kts

Best glide speed is ___ kts + I knot/ 100 lbs fuel:

230

Multiply altitude in thousands of feet by ___ for glide distance in NM:

1.7

Max crosswind, dry runway (dash-1):

30 kts

Max crosswind, wet runway:

20 kts

Max crosswind, icy or standing water:

10 kts

Gross weight with fuel and two souls

12,800 lbs

Dash 1 Ch 1 Flashcards

(96 cards)