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T-38 Ops Limits
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Terms in this set (38)
Airpseed
Flaps 1% - 45% (KCAS)
300
Airpseed
Flaps 46% - 60% (KCAS)
240
Airpseed
Flaps Over 60% (KCAS)
220
Airspeed
Canopy (KCAS)
50
Airspeed
Gear / Gear Doors (KCAS)
240
Airspeed
Nose Wheel Steering (Kts GS)
65
Airspeed
Main Wheel Tire (14 Ply) (Kts GS)
221
Airspeed
Main Wheel Tire (12 Ply) (Kts GS)
195
Airspeed
Nose Wheel Tire (Kts GS)
174
Load Factor
Max Sym G 3500 ( ___ - ___ )
-2.3, +5.7
Load Factor
Max Asym G 3500 ( ___ - ___ )
0, +4.1
Load Factor
Max Sym G 3000 ( ___ - ___ )
-2.4, +5.9
Load Factor
Max Asym G 3000 ( ___ - ___ )
0, +4.3
Load Factor
Max Sym G 2000 ( ___ - ___ )
-2.6, +6.5
Load Factor
Max Asym G 2000 ( ___ - ___ )
0, +4.7
Load Factor
Max Sym G 1000 ( ___ - ___ )
-2.9, +7.2
Load Factor
Max Asym G 1000 ( ___ - ___ )
0, +5.0
Hydraulic Pressure
Min PSI
1500
Hydraulic Pressure
Max PSI
3200
Hydraulic Pressure
Normal Range _____ PSI to _____ PSI
2850, 3200
Oxygen Pressure
Normal Range ___ PSI to ___ PSI
50, 120
WSSP Limitations
Sym ___ to ___
0, +4.0
WSSP Limitations
Asym ___ to ___
0, +3.0
WSSP Limitations
Normal Capacity (LBS)
140
Airspeed Limitations
Max (KCAS)
400
Airspeed Limitations
SB Open / Turbulence (KCAS)
350
Airspeed Limitations
Abrupt Control (KCAS)
240
Prohibited Maneuvers
1.
Vertical Stalls
Prohibited Maneuvers
2.
Intentional Spins
Prohibited Maneuvers
3.
Continuous aileron rolls (more than one complete roll) will be accomplished only at 1.0 G and 3/4 or less stick deflection.
EGT
Abort Start if EGT reaches ___°C to preclude exceeding temperature limits.
845
EGT
Abort aircraft during ground start if EGT Exceeds ___°C momentarily.
925
*EGT* Total fluctuations in EGT of ___°C (±___ °C) are acceptable if the average
EGT
EGT
Total fluctuations in EGT of ___°C (±___ °C) are acceptable if the average *EGT* is between ___°C and ___ °C.
15, 7.5, 630, 650
RPM
Maximum allowable transient RPM ___ %
107
Nozzle Position
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ seconds.
10
Fuel Flow
During engine atart the indicated fuel flow mayu 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.
360, 360
Oil Pressure
Do not exceed ___ minutes in military power with oil pressure above ___ PSI.
5, 55
Oil Pressure
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.
10
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