Section 1 Flashcards by Casey Walters

Wingspan

25 Feet 3 Inches

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HUD Field of View/Instantaneous FOV From Combat Eye and Design Eye

24 Degrees/ 17 Degrees/ 15 Degrees

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Gross Weight

12,700lbs

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MIL/MAX Static Thrust on STD day

2200 lbs and 3300 lbs

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Length of Ignition

30 Seconds (Indefinite if Button is Held)

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Avoid Throttle Bursts From IDLE to MIL in How Many Seconds

1 Second

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EED Displays at Max Brightness

If Battery Has Less Than 22 Volts

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T Button Held on EED Selects Calibration After How Many Seconds

15 Seconds

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RPM Indicator Range

0-110%

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EGT Indicator Range

0-1200 Degrees

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NOZ Indicator Range

0-99%

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Oil Indicator Range

0-80 PSI

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MAX Fuel Flow at Sea Level on Standard Day

7300lbs/hr

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Does Momentarily pressing the ENGINE START button again throttle toward idle. during a 30-second cycle does reset the ignition timer

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MAX Fuel Flow at Sea Level on Standard Day at Mach 1

11,400lbs/hr

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AC Generator Output

320-480 Cycles Per Second

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Gearbox Shift Range

65-75%

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Maneuvering Between __ and __ Increases Susceptibility to Stall/Flameout

28,000ft and 0.6 IMN

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Grey Area on Flameout Susceptibility Restrict Throttle Movements To How Quick

1 Inch in 3 Seconds

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EGT Droop Conditions

Low Altitude/500kts/3% Nozzle

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Idle Decay Prevention

Maintain 80% When Less Than 200 KCAS and Above 20,000ft

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Gravity Feed Provides Sufficient Fuel to MAX at What Altitude

25,000ft (6,000 Guaranteed/7,000 Occurrences)

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Fuel Low When EITHER System INDICATES

below 250 lbs For More Than 7.5 Seconds

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Fuel Imbalance Indications Begin at ___lbs With White and Greater Than ___lbs with Red

60lbs and >200lbs

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If One Fuel System Has Less Than ___ Boost Pump Output is Reduced ____

650 lbs and 40%

Voltage of AC System

115/200

Transformer Rectifier Amperage

50 amps

Voltage of Battery

24 Volts

Generator Cut-In Speed

43-48%

Oil System Contains ___qts of Oil, With Expansion of ___qts

4qts and 1qt

Oil May be Burnt Up to ___pints per Hour

1 Pint

Pressure of Hydraulic Systems

3,000 PSI Each

Hydraulic Lights Come on At ___ and Go Out at ___

1,500PSI and 1,800PSI

Landing Gear Extension/Retraction Time

6 Seconds

Landing Gear Warning System Activates When

210kts or Less, 10,000ft +-750ft, Both Throttles Below 96%

Landing Gear Warning Tones Don't Deactivate Until Accelerating Through

240kts

Landing Gear Alternate Release Handle Extension Length and Time

10 Inches; 15-35 Seconds

Nose Gear Extended __ Provides ___ Rudder Deflection (Both Answers)

- Less Than 3/4; 6 Degrees | - 3/4 or More; 30 Degrees

The Majority of Slab Compensation Occurs in the First ___ % of Flap Movement

35%

Pressurization Schedule

23,000 = Alt-6,000 / 2 +-2,000

Engine Anti Ice On/Off Schedule

Requires 80%, Turns on Below 65% Automatically

At Engine Speeds of __ Anti-Ice Increases EGT ___

94-98%; 15 Degrees

Loss Of Thrust at MIL and MAX Due to Anti-Ice

9% Loss in MIL; 6.5% Loss in MAX

All AOA Lights May Light, No Maintenance is Required Unless They Stay On For ___

2 Minutes

Birdstrikes at ___ Can Damage Windscreen and Hit the HUD

400kts

Avoid Opening the Canopy When Relative Wind Exceeds __

30 kts

Front Canopy Jettisons First Then __ Seconds Later the Rear Canopy With the D-Handle

1 Second

Aneroid Delays Parachute Opening Until Between

15,000ft and 11,500ft

Canopy is Jettisoned During Ejection Sequence After ____ Seconds

0.3 Seconds

Seat Can Be Adjusted __ Inches

5 Inches

Seat Kit is Automatically Released After a ____ Second Delay

4 Seconds

Oxygen Low Level Light Illuminates at ___, Blinking May Occur at ___ Due to Sloshing

1 Liter, 3 Liters

MDP Power Up Requires ___ Seconds

45 Seconds

MDP Warm Boot Requres ___ Seconds While a Cold Boot Requires ___ Seconds

10 Seconds/45 Seconds

Warm Boot Occurs If Power Loss is Between ___ and ___ Milliseconds

50 to 300

EED and HUD May Disagree on Fuel, When Greater Than ___ the EED is Correct

20lbs

ILS Commands are Optimized for GS Interception at ___ and ___ Ft Above Touchdown

6NM and 1800ft

Pitch Ladder on HUD Displayed at ___ the Pitch Angle

One - Half

RALT Readings Only Available Below ___

5,000

Low Altitude stall indications

- "bang" sound - Rapid RPM drop - High EGT - Bring throttle to IDLE/retard ASAP to prevent damage/overtemp and push engine start button

High altitude stall indications

- Rapid RPM drop - drop in EGT - Bring throttle to IDLE/retard ASAP to prevent damage/overtemp and push engine start button

Main Fuel Control does four things

- regulates engine min speed at idle and max speed for MIL/MAX - Limits fuel flow to safe lvls during starts and rapid throttle movements - fuel-air ratio for low pwr and engine start - correctly position inlet guide vanes/ bleed air

How is the engine oil cooled

Fuel-oil cooler system

what helps reduce the possibility of compressor stalls

Variable inlet guide vanes and air bleed valves

Above what altitudes and Indicated mach number with rapid throttle movements is prone to flameouts/stalls

above 28,000 | below 0.6 IMN

T 2 CUTBACK does what

controls fuel to auto reduce RPM and EGT to prevent over-px and high corrected speed conditions of striped area. the compressor at low CIT

The crossfeed valve is powered by

The T-38C is normally refueled by the single-point system provides a total of _____ lbs

3,906 lbs at 60 F

Usable fuel per side

- 1990 lbs right | - 1916 lbs in left

Manual refueling provides ______ lbs

3866 lbs

Low-pressure lights are only valid indications of boost pump output with crossfeed on or off?

Off

Fuel shutoff valves stop fuel flow in ____ seconds

1 sec without throttle

Keep fuel balance within _____ lbs to keep in CG limits

200 lbs

Taxi operations with less than ____ lbs can cause fuel starvation

150 lbs

If one generator fails how long may it take to auto transfer electrical load

2.5 Sec

Power protection of either bus with respective gen at ___VAC

90 Volt AC

How long could it take for the gen light to illuminate with a failure?

2.5 Sec

When will RECTIFIER FAILURE PFL appear for a TRU fail?

When the TRU falls below 25.5 V for more than 2 sec

Min battery voltage to close battery relays and will stay on until?

18 Volts min to connect and will remain on till 10 Volts

Static inverter converts which bus voltage to what?

DC bus volts to 115 Volts AC

Static inverter powers (3)

- First engine start on ground/in flight - operation of right engine autosyn (fuel/Oil) and left /right fuel amounts - O2 amount

Static inverter activated when

- Start button pressed - OXY/Fuel check switch used - Throttle moved into MAX