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T38-1 > Section 1 > Flashcards

Section 1 Flashcards

1
Q

Wingspan

A

25 Feet 3 Inches

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2
Q

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

A

24 Degrees/ 17 Degrees/ 15 Degrees

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3
Q

Gross Weight

A

12,700lbs

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4
Q

MIL/MAX Static Thrust on STD day

A

2200 lbs and 3300 lbs

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5
Q

Length of Ignition

A

30 Seconds (Indefinite if Button is Held)

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6
Q

Avoid Throttle Bursts From IDLE to MIL in How Many Seconds

A

1 Second

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7
Q

EED Displays at Max Brightness

A

If Battery Has Less Than 22 Volts

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8
Q

T Button Held on EED Selects Calibration After How Many Seconds

A

15 Seconds

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9
Q

RPM Indicator Range

A

0-110%

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10
Q

EGT Indicator Range

A

0-1200 Degrees

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11
Q

NOZ Indicator Range

A

0-99%

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12
Q

Oil Indicator Range

A

0-80 PSI

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13
Q

MAX Fuel Flow at Sea Level on Standard Day

A

7300lbs/hr

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14
Q

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

A

No

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15
Q

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

A

11,400lbs/hr

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16
Q

AC Generator Output

A

320-480 Cycles Per Second

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17
Q

Gearbox Shift Range

A

65-75%

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18
Q

Maneuvering Between __ and __ Increases Susceptibility to Stall/Flameout

A

28,000ft and 0.6 IMN

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19
Q

Grey Area on Flameout Susceptibility Restrict Throttle Movements To How Quick

A

1 Inch in 3 Seconds

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20
Q

EGT Droop Conditions

A

Low Altitude/500kts/3% Nozzle

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21
Q

Idle Decay Prevention

A

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

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22
Q

Gravity Feed Provides Sufficient Fuel to MAX at What Altitude

A

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

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23
Q

Fuel Low When EITHER System INDICATES

A

below 250 lbs For More Than 7.5 Seconds

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24
Q

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

A

60lbs and >200lbs

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25
Q

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

A

650 lbs and 40%

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26
Q

Voltage of AC System

A

115/200

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27
Q

Transformer Rectifier Amperage

A

50 amps

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28
Q

Voltage of Battery

A

24 Volts

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29
Q

Generator Cut-In Speed

A

43-48%

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30
Q

Oil System Contains ___qts of Oil, With Expansion of ___qts

A

4qts and 1qt

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31
Q

Oil May be Burnt Up to ___pints per Hour

A

1 Pint

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32
Q

Pressure of Hydraulic Systems

A

3,000 PSI Each

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33
Q

Hydraulic Lights Come on At ___ and Go Out at ___

A

1,500PSI and 1,800PSI

34
Q

Landing Gear Extension/Retraction Time

A

6 Seconds

35
Q

Landing Gear Warning System Activates When

A

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

36
Q

Landing Gear Warning Tones Don’t Deactivate Until Accelerating Through

A

240kts

37
Q

Landing Gear Alternate Release Handle Extension Length and Time

A

10 Inches; 15-35 Seconds

38
Q

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

A
  • Less Than 3/4; 6 Degrees

- 3/4 or More; 30 Degrees

39
Q

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

A

35%

40
Q

Pressurization Schedule

A

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

41
Q

Engine Anti Ice On/Off Schedule

A

Requires 80%, Turns on Below 65% Automatically

42
Q

At Engine Speeds of __ Anti-Ice Increases EGT ___

A

94-98%; 15 Degrees

43
Q

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

A

9% Loss in MIL; 6.5% Loss in MAX

44
Q

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

A

2 Minutes

45
Q

Birdstrikes at ___ Can Damage Windscreen and Hit the HUD

A

400kts

46
Q

Avoid Opening the Canopy When Relative Wind Exceeds __

A

30 kts

47
Q

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

A

1 Second

48
Q

Aneroid Delays Parachute Opening Until Between

A

15,000ft and 11,500ft

49
Q

Canopy is Jettisoned During Ejection Sequence After ____ Seconds

A

0.3 Seconds

50
Q

Seat Can Be Adjusted __ Inches

A

5 Inches

51
Q

Seat Kit is Automatically Released After a ____ Second Delay

A

4 Seconds

52
Q

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

A

1 Liter, 3 Liters

53
Q

MDP Power Up Requires ___ Seconds

A

45 Seconds

54
Q

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

A

10 Seconds/45 Seconds

55
Q

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

A

50 to 300

56
Q

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

A

20lbs

57
Q

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

A

6NM and 1800ft

58
Q

Pitch Ladder on HUD Displayed at ___ the Pitch Angle

A

One - Half

59
Q

RALT Readings Only Available Below ___

A

5,000

60
Q

Low Altitude stall indications

A
  • “bang” sound
  • Rapid RPM drop
  • High EGT
  • Bring throttle to IDLE/retard ASAP to prevent damage/overtemp and push engine start button
61
Q

High altitude stall indications

A
  • Rapid RPM drop
  • drop in EGT
  • Bring throttle to IDLE/retard ASAP to prevent damage/overtemp and push engine start button
62
Q

Main Fuel Control does four things

A
  • 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
63
Q

How is the engine oil cooled

A

Fuel-oil cooler system

64
Q

what helps reduce the possibility of compressor stalls

A

Variable inlet guide vanes and air bleed valves

65
Q

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

A

above 28,000

below 0.6 IMN

66
Q

T 2 CUTBACK does what

A

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

67
Q

The crossfeed valve is powered by

A

DC

68
Q

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

A

3,906 lbs at 60 F

69
Q

Usable fuel per side

A
  • 1990 lbs right

- 1916 lbs in left

70
Q

Manual refueling provides ______ lbs

A

3866 lbs

71
Q

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

A

Off

72
Q

Fuel shutoff valves stop fuel flow in ____ seconds

A

1 sec without throttle

73
Q

Keep fuel balance within _____ lbs to keep in CG limits

A

200 lbs

74
Q

Taxi operations with less than ____ lbs can cause fuel starvation

A

150 lbs

75
Q

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

A

2.5 Sec

76
Q

Power protection of either bus with respective gen at ___VAC

A

90 Volt AC

77
Q

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

A

2.5 Sec

78
Q

When will RECTIFIER FAILURE PFL appear for a TRU fail?

A

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

79
Q

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

A

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

80
Q

Static inverter converts which bus voltage to what?

A

DC bus volts to 115 Volts AC

81
Q

Static inverter powers (3)

A
  • First engine start on ground/in flight
  • operation of right engine autosyn (fuel/Oil) and left /right fuel amounts
  • O2 amount
82
Q

Static inverter activated when

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

T38-1 (4 decks)

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