Dash 1 Flashcards by Nate Berndt

Gross weight with fuel and two souls

12,800lbs

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One engine thrust, mil and Max

2200/3300

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

7300/ 11,400lb/hr

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Pushing start arms ignition circuit for

30sec

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One engine normal oil capacity and air expansion space

4qt, 1 qt

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Gravity flow guaranteed up to ____, Normal operation _____, flameouts have occurred at _____

6000, 25000, 7000

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fuel cutoff switches operated by ____ and cut off fuel in ____

DC, 1 sec

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fuel low light comes on after ____

7.5 sec and less than 250lbs

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Gearbox shift occurs at ____

65-75%

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Voltage of battery is ____ V and of DC rectifiers is _____

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

18V

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Left engine provides ____ psi for ____ system

3200 utility

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right engine provides ____psi for ____ system

3200 flight controls

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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 approximately

6sec

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

210kts, 10,000ft, 96%

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When accelerating, gear light may not go out until __

240kts

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Landing gear alt release pulled out ____in, and requires ____sec

10in, 15-35sec

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Rear canopy follows front by ____ after canopy jettison

1 sec

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Fuel for left engine is ____ gal serviced/usable and ___lbs usable

293, 286 gal, 1916lbs

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Fuel for right engine is ____ gal serviced/usable and ___lbs usable

305/297 gal, 1990

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Total fuel for the engine is ____ gal serviced/usable and ___lbs usable

598/ 583 gal, 3906

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With single-engine and less than ____ in either system, leave both boost pumps on and crossfeed on:

250lbs

A minimum of ____ RPM is required to achieve any engine fuel flow _____% RPM is the heart of airstart envelope at any altititude

12%, 18-20%

Ignition must occur before fuel flow reaches

360lb/hr

After aborted start, wait ____min before attempting another start

2min

If EGT doesn't rise within ___sec of fuel flow indications, abort start

12sec

Flaps should be +/- ____ of 60%

Normal rotation speed on initial T/O is ____, lift off speed is ___

145 KIAS rounded (141 actually), 165KIAS

Delay takeoff a min of ___min behind large and ____ behind heavy

2, 4

With a Xwind >____ knots, spacing behind large/heavy aircraft can be reduced

Abort T/O if either afterburner doesnt light within

5sec

Touchdown speed is ____ plus 1 Knot per 100lbs over 1000lbs

135

Min hydraulic pressure is

1500psi

each generator is ___ phase

The O2 light comes on at or below ___ liter, may blink at or below ___

1, 3 liters

There are ____ rotating beacons, located where

2, tail/ lower fuselage

There are ____ position lights, located where

4, tail/ lower fuselage, each wing

Battery energizes DC bus for ___

15min at 80% charged

If oil pressure is high in cold weather, should be in limits within ____ min

6min

The radio attenuation switch reduced UHF and VHF volume by ____

66%

IDENT sends a pulse with transponder replies for ____ sec

15sec

Standby AI provides _____ deg climb, ___ deg dive, ____ deg roll capacity and provides ____ minutes of useful info within ___ deg after DC failure

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

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

80%

Due to oil supply restriction, zero G flight restricted to ___sec

10sec

Due to oil supply restirction, negative G flight restricted to ___

30sec

Rudder system failure may push rudder to ___deg and stag failure may push rudder____ deg

30deg, 2 deg

Touchdown greater than ____KCAS, should not be attempted

200KTS

With Asymmetric flaps, maintain ____ KTS above final appr/ touchdown speed and touchdown with no less than ___Kts

20 kts/ 165 kts

Max speed for Nosewheel

174

Estimation for landing roll is ___+ fuel (not including 1000ft down), No-flap ____ landing roll,

2500, doubles

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 will provide adequate control authority and controllable stick forces

30-45%

Pressure reg, maintain cabin alt ___ +/- 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

100kts

increase final approach and touchdown speed by ___ the gust factor

1/2

Landing light retraction takes ___

10sec

AOA max range is ____, endurance/best angle of climb is ____,

.18, .3

Nozzles should stabilize within ____ sec after rapid throttle movements

10 sec

First 4 1/2 of stick travel provides ____ aileron deflection

50%

Next 1 1/2 of stick travel provides ___ aileron deflection

Full

Crossfeed recommended with fuel imbalance of ____ or greater

200

Holding airspeed

250-265

Radar pattern typically burns

325lbs

Turbulent air/thunderstorms penetration speed is ___

280kts

Climb possible at SETOS is ____fpm

100fpm

Climb increased by ___fpm each kt between SETOS and SETOS +10

8-50fpm

Gear retraction may take ____ when retracted between SETOS and SETOS + 10

1 min

If unable to retract gear, best climb at ___ for 60% flaps, ____ for 0% flaps:

200, 220

Optimum pitch for ejection is

20 NH

With loss of canopy slow to ___kts; min drage occurs at ____KTS

300, 225

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

35min

Maintain ___KTS above min controllable airspeed in descent/ landing approach

20kts

Max crosswind for dry, wet, and icy or standing water

30, 20, 10

Max crosswind for touch and go

Max crosswind for solo students

15/ 10 wet rwy

Minimum rwy length for takeoff / landing

8000ft

low level min and max airspeed is

300, 420

Perform all aerobatic maneuvers above

8000ft AGL

stall and slow flight must be performed between

8000ft - FL 200

Min power setting for stall and slow flight

80%

Nose high recoveries must be accomplished below

FL 240

Do not perform supersonic flight below ____ unless in an authorized airspace

FL 300

Solo students will not perform patterns and landing with ___ fuel

2500lbs

Normal minimum fuel for solo students is

800

minimum fuel is

600

emergency fuel is

400

Min taxi interval is ___ staggered ____ in trail

150, 300ft

REstricted low approach must be initiated by ____ unless otherwise directed

500ft AGL

Chase aircraft can low approach down to

300ft

Begin close pull up with a min of ____ kts, maintain min of ___

240, 200

Rolling T/O may increase takeoff distance by

150-300ft

Dash 1 Flashcards

(95 cards)