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T-38 IP > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q 
Ground - Start
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
925 (Max 845)
-
-
360 (Max)
-
-
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2
Q 
Ground - Idle
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
-
46-50
77-92
400-600 (std day)
5-20
-
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3
Q 
Ground - Military
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
630-650
99-101
0-20
2100-2700 (Sea Level)
20-55
5
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4
Q 
Ground - (Max) / Afterburner
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
630-650
99-101
50-85
-
20-55
5
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5
Q 
Flight Steady State - Idle
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
-
-
-
200 (Min) (Std Day)
5 (Min)
-
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6
Q 
Flight Steady State - Military
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
630-650
99-104
0-20
-
20-55
30
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7
Q 
Flight Steady State - (Max) / Afterburner
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
630-650
99-104
50-85
-
20-55
15
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8
Q 
Fluctuation Limits - Idle
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
-
46-50
None Allowed
\+/- 25
\+/- 2
-
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9
Q 
Fluctuation Limits - MIL and AB (Ground)
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
-
99-101
\+/- 3
\+/- 50
\+/- 2
-
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10
Q 
Fluctuation Limits - MIL and AB (Flight)
EGT
RPM
Nozzle Posit
Fuel Flow
Oil Px
Time Dur
A 
-
\+/- 1
\+/- 3
\+/- 50
\+/- 2
-
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11
Q

EGT: Abort start if EGT reaches ___ to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ___.

A

845 degrees C

925 degrees C

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12
Q

RPM: Maximum allowable transient RPM ___.

A

107%

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13
Q

Nozzle Position: Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ seconds.

A

10

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14
Q

Fuel Flow: During engine start the indicated fuel flow may momentarily transit above ____ LB/HR after advancing the throttle to idle during engine sequence but should return to equal to or less than ____ LB/HR prior to EGT rise during actual engine start.

A

360

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15
Q

Oil Pressure: Do not advance throttle above idle without a positive (>0) indication of oil pressure. During cold weather, oil pressure may exceed limitations. This is normal indication as long as the oil pressure continues to decrease as engine oil warms. Do not exceed __ minutes in military power with oil pressure above ___ PSI. If a sudden change of ___ PSI or greater in oil pressure indication occurs at any stabilized RPM, follow engine oil system malfunction procedures in Section III of the DASH 1.

A

5 minutes
55 PSI
10 PSI

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16
Q

Max Airspeed: Flaps 1%-45%

A

300 KCAS

17
Q

Max Airspeed: Flaps 46%-60%

A

240 KCAS

18
Q

Max Airspeed: Flaps Over 60%

A

220 KCAS

19
Q

Max Airspeed: Canopy

A

50 KCAS

20
Q

Max Airspeed: Gear / Gear Doors

A

240 KCAS

21
Q

Max Airspeed: Nose Wheel Steering

A

65 Kts GS

22
Q

Max Airspeed: Main Wheel Tire

A

221 (14 ply) KtsGS

195 (12 ply) Kts GS

23
Q

Max Airspeed: Nose Wheel Tire

A

174 Kts GS

24
Q

Load Factor Limits: 3500 lbs
Max Sym G
Max Asym G

A

-2.3 to +5.7

0 to +4.1

25
Q

Load Factor Limits: 3000 lbs
Max Sym G
Max Asym G

A

-2.4 to +5.9

0 to +4.3

26
Q

Load Factor Limits: 2000 lbs
Max Sym G
Max Asym G

A

-2.6 to +6.5

0 to +4.7

27
Q

Load Factor Limits: 1000 lbs
Max Sym G
Max Asym G

A

-2.9 to +7.2

0 to +5.0

28
Q

Caution: Extension / retraction of landing gear at bank angles greater than ___ or at load factors greater than ___ can result in overstress failure of the main landing gear sidebrace trunnion.

A

45 degrees

1.5 G

29
Q

Hydraulic Pressure Min PSI

A

1500 PSI

30
Q

Hydraulic Pressure Max PSI

A

3200 PSI

31
Q

Hydraulic Pressure Normal Range

A

2850 PSI to 3200 PSI

32
Q

Oxygen Pressure Normal Range

A

50 PSI to 120 PSI

33
Q

WSSP Limitations:
Symmetrical Gs
Asymmetrical Gs
Normal Capacity

A

0 to +4.0
0 to +3.0
140 LBS

34
Q

Airspeed Limits:
Max
SB Open / Turbulence
Abrupt Control

A

400 KCAS
350 KCAS
240 KCAS

35
Q

DASH -1 Prohibited Maneuvers

A
  1. Vertical Stalls
  2. Intentional Spins
  3. Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.

T-38 IP (6 decks)

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