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T38 By the Numbers > Section 1 > Flashcards

Section 1 Flashcards

1
Q

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

A

24 Degrees/ 17 Degrees/ 15 Degrees

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2
Q

Gross Weight

A

12,800 lbs

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3
Q

MIL/MAX Thrust

A

2,050/2900lbs after PMP mod 2200/3300lbs

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4
Q

Length of Ignition

A

30 sec

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5
Q

Avoid Throttle Bursts From IDLE to MIL in How Many Seconds

A

1 sec

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6
Q

EED Displays at Max Brightness

A

If Battery Has Less Than 22 Volts

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7
Q

T Button Held on EED Selects Calibration After How Many Seconds

A

15 sec

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8
Q

RPM Indicator Range

A

0-110%

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9
Q

EGT Indicator Range

A

0-1200 Degrees

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10
Q

NOZ indicator range

A

0-99%

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11
Q

Oil indicator range

A

0-80 psi

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12
Q

MAX Fuel Flow at Sea Level on Standard Day

A

7300 lbs/hr

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13
Q

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

A

11,400 lbs/hr

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14
Q

AC Generator Output

A

320-480 Cycles Per Second

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15
Q

Gearbox Shift Range

A

65-75%

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16
Q

Grey Area on Flameout Susceptibility Restrict Throttle Movements To How Quick

A

1 Inch in 3 Seconds

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17
Q

EGT Droop Conditions and Indications

A

At low altitude and high airspeed (500 KCAS), EGT droop can occur with engine at military power when accompanied by 3% or less nozzle indication.

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18
Q

Idle Decay Prevention

A

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

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19
Q

Gravity Feed Provides Sufficient Fuel to MAX at What Altitude

A

25,000ft (6,000 Guaranteed/ 7,000 has occurred)

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20
Q

Fuel Low When EITHER System INDICATES

A

less than 250 For More Than 7.5 Seconds

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21
Q

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

A

60lbs and >200lbs

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22
Q

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

A

650lbs and 40%

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23
Q

Voltage of AC System

A

115/200

24
Q

Transformer Rectifier Amperage

A

50amps

25
Q

Voltage of Battery

A

24 Volts

26
Q

Generator Cut-In Speed

A

43-48%

27
Q

Oil System Contains ___qts of Oil, With Expansion of ___qts

A

4qts and 1qt

28
Q

Oil May be Burnt Up to ___pints per Hour

A

1 Pint

29
Q

Pressure of Hydraulic Systems

A

3,000 PSI Each

30
Q

Hydraulic Lights Come on At ___ and Go Out at ___

A

1,500PSI and 1,800PSI

31
Q

Landing Gear Extension/Retraction Time

A

6 Seconds

32
Q

Landing Gear Warning System Activates When

A
  • The airspeed is 210 KCAS or less.
  • The altitude is 10,000 feet or below.
  • Both throttles are below 96% RPM.
33
Q

Landing Gear Warning Tones Don’t Deactivate Until Accelerating Through

A

240kts

34
Q

Landing Gear Alternate Release Handle Extension Length and Time

A

10 Inches; 15-35 Seconds

35
Q

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

A
  • Less Than 3/4; 6 Degrees

- 3/4 or More; 30 Degrees

36
Q

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

A

35%

37
Q

Pressurization Schedule

A

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

38
Q

Engine Anti Ice On/Off Schedule

A

Requires 80%, Turns on Below 65% Automatically

39
Q

At Engine Speeds of __ Anti-Ice Increases EGT ___

A

94-98%

15 Degrees

40
Q

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

A

9% Loss in MIL

6.5% Loss in MAX

41
Q

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

A

2 Minutes

42
Q

Birdstrikes at ___ Can Damage Windscreen and Hit the HUD

A

400kts

43
Q

Avoid Opening the Canopy When Relative Wind Exceeds __

A

30 kts

44
Q

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

A

1 Second

45
Q

Aneroid Delays Parachute Opening Until Between

A

15,000ft and 11,500ft

46
Q

Canopy is Jettisoned During Ejection Sequence After ____ Seconds

A

0.3 Seconds

47
Q

Seat Can Be Adjusted __ Inches

A

5 Inches

48
Q

Seat Kit is Automatically Released After a ____ Second Delay

A

4 Seconds

49
Q

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

A

1 Liter, 3 Liters

50
Q

MDP Power Up Requires ___ Seconds

A

45 Seconds

51
Q

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

A

10 Seconds/45 Seconds

52
Q

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

A

50 to 300

53
Q

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

A

20lbs

54
Q

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

A

6NM and 1800ft

55
Q

Pitch Ladder on HUD Displayed at ___ the Pitch Angle

A

One - Half

56
Q

RALT Readings Only Available Below ___

A

5,000

T38 By the Numbers (3 decks)

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