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T38-1 > Section 5-7 > Flashcards

Section 5-7 Flashcards

1
Q

Normal Thrust is Obtained at ___% or ___Degrees Whichever Occurs First

A

98% or 630 Degrees

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2
Q

MIL Thrust is Obtained at ___% RPM

A

100%

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3
Q

MAX Thrust is Obtained at ___% RPM With Afterburner Operating

A

100%

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4
Q

Afterburner Augmentation of power is ___ to ___%

A

5 to 40%

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5
Q

Flap Limits

A
  • 1-45 - 300
  • 46-60 - 240
  • > 60 - 220
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6
Q

Gear and Gear Doors Limiting Airspeed

A

240kts

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7
Q

Do Not Extend Gear at Bank Angles Greater Than ___ Degrees OR More Than ___g’s

A

45 Degrees and 1.5 Gs

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8
Q

Oxygen Pressure Operating Range

A

50-120 PSI

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9
Q

Hydraulic Pressure Operating Range

A

1500 Minimum; 2850-3200 Normal; 3200 Maximum

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10
Q

Abort Start if EGT Reaches ___ Degrees, Abort Jet if EGT Reaches ___ Degrees

A

845/925 Degrees

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11
Q

Total EGT Fluctuations of ___ Degrees Permitted, Mean within the Green

A

15 Degrees

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12
Q

Maximum Allowable Transient RPM

A

107%

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13
Q

Rapid Throttle Movements, Nozzle Should Stabilize Within ___ Seconds

A

10 Seconds

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14
Q

Nozzle Position May be Less Than ___ % When Operating in Less Than MAX AB

A

50%

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15
Q

During Cold Weather Starts, Run Engines at ___ For ___ Minutes

A

MIL and 5 Minutes

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16
Q

Oil Pressure Indication Change of ___PSI at Stabilized RPM, Reference Checklist

A

10 PSI

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17
Q

Nose Wheel Steering Limitation

A

65kts

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18
Q

Canopy Limitation

A

50kts

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19
Q

Symmetrical Flight Load Factors for 3500/3000/2000/1000

A
  • 2.3- +5.7
  • 2.4- +5.9
  • 2.6- +6.5
  • 2.9- +7.2
20
Q

Unsymmetrical Flight Load Factors for 3500/3000/2000/1000

A

0 to +4.1
0 to +4.3
0 to +4.7
0 to +5.0

21
Q

Continuous Aileron Rolls Can Only Be Accomplished At ___g and ___ or Less Stick Deflection

A

1.0g and 3.4 or Less

22
Q

Maximum G’s

A

7.33 and -3.0 Gs

23
Q

To Prevent Flameout Due to Fuel Starvation Avoid MAX Thrust Dives With Less Than ___lbs

A

650lbs

24
Q

To Prevent Flameout Due to Fuel Starvation Avoid MAX Thrust in Zero or Neg G Flight Exceeding ____

A

10 Seconds at 10,000ft

30 Seconds at 30,000ft

25
Q

Oil Supply and Pressure Requirements Restrict Zero G Flight to ___ Seconds and Neg G Flight to ___ Seconds

A

10 Seconds

60 Seconds

26
Q

After 0 or Neg G Flight, If Oil Pressure Does Not Recover Within ___ Seconds, Return to Normal Flight Conditions

A

10 Seconds

27
Q

Full Stop Landings Time Intervals if Gear is Retracted In Flight/if Gear is Left Extended

A

45 Minutes/15 Minutes

28
Q

Maximum Nosewheel Tire Speed

A

174kts

29
Q

Maximum Main Wheel Tire Speed

A

221 kts

30
Q

Sink Rates Should Not Exceed ___ for Normal and ___ for Crab When Less Than 1700lbs

A

590fpm and 395fpm

31
Q

Sink Rates Should Not Exceed ___ for Normal and ___ for Crab When Greater Than 1700lbs

A

340fpm and 200fpm

32
Q

WSSP Airspeed Limitations Normal/Severe Turbulence (SB)/Abrupt Control Movements

A

400
350
240kts

33
Q

WSSP G Limitations

A

0- +4 Symmetric

0- +3 Unsymmetric

34
Q

Ejection from a Spin Must be Accomplished if Recovery is Not Completed by ___ft AGL

A

15,000ft

35
Q

G Overshoot May Occur If Pulsing the Stick Between ___ and ___ Mach

A

0.80 and 0.95 Mach

36
Q

The First ___ Inches of Stick Travel Provide ___ Aileron Deflection

A

4.5 Inches and 1/2 Aileron Deflection

37
Q

Minimum Stick Forces Occur Per G at ___ Mach

A

0.9 Mach

38
Q

EED Fuel Quantity Displays Near Thunderstorms Vary Up to ___lbs

A

200lbs

39
Q

Thunderstorm Penetration Airspeed

A

280kts

40
Q

Do not exceed max allowable A/S of

A

710 Kts

41
Q

Engine Damage May Occur if ___Inches of Ice Accumulates on Engine Inlet Duct Lips

A

0.25 Inches

42
Q

Engine Anti-Ice Requires ___ % RPM

A

80%

43
Q

At Temperatures Below ___ Degrees, Allow Engines to Run at Idle for ___Minutes

A

-30 for 2 Minutes

44
Q

During Cold Weather Ops, Cycle Flight Controls ___ to ___ Times 4 to 6 Times

A

4 to 6 Times

45
Q

At Temperatures Below ___ Degrees, Low Idle RPM May be Observed, Increast RPM for Generators to Cut In

A
  • 16 F
46
Q

With Canopy Closed in Hot Weather, Cockpit Damage May Occur Above ___ Degrees

A

110 F

T38-1 (4 decks)

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