Dash 1 Flashcards
Gross weight with fuel and two souls
12,800lbs
One engine thrust, mil and Max
2200/3300
Fuel flow for one engine, Max at rest and Mach 1
7300/ 11,400lb/hr
Pushing start arms ignition circuit for
30sec
One engine normal oil capacity and air expansion space
4qt, 1 qt
Gravity flow guaranteed up to ____, Normal operation _____, flameouts have occurred at _____
6000, 25000, 7000
fuel cutoff switches operated by ____ and cut off fuel in ____
DC, 1 sec
fuel low light comes on after ____
7.5 sec and less than 250lbs
Gearbox shift occurs at ____
65-75%
Voltage of battery is ____ V and of DC rectifiers is _____
24, 28
AC system provides ____/____ V power
115/200
AC generators cut-in between ____
43-48%
Min battery voltage of ___ is required to close batt relay
18V
Left engine provides ____ psi for ____ system
3200 utility
right engine provides ____psi for ____ system
3200 flight controls
Rudder limited to ___ deg each side when nosegear out 3/4 or less
6 deg
landing gear extension/retraction takes approximately
6sec
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%
When accelerating, gear light may not go out until __
240kts
Landing gear alt release pulled out ____in, and requires ____sec
10in, 15-35sec
Rear canopy follows front by ____ after canopy jettison
1 sec
Fuel for left engine is ____ gal serviced/usable and ___lbs usable
293, 286 gal, 1916lbs
Fuel for right engine is ____ gal serviced/usable and ___lbs usable
305/297 gal, 1990
Total fuel for the engine is ____ gal serviced/usable and ___lbs usable
598/ 583 gal, 3906
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%
5
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
5
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
3
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
25
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
