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T-38 Aircraft > Limitations > Flashcards

Limitations Flashcards

0
Q

Engine Start - EGT

A

EGT: 925 C MAX

Abort Start if EGT Reaches 845 C

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1
Q

Minimum Crew

A

One, Must Be Flown From Front Cockpit

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2
Q

Maximum Continuous Thrust:
RPM
EGT

A

RPM - 98%

EGT - 630 degrees

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3
Q

Maximum Thrust

RPM

A

RPM - MAX or 100%

With MAX Afterburner

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4
Q 
Idle Thrust (Ground):
RPM
Nozzle
Fuel Flow
Oil Pressure
A

RPM: 46-50 %
Nozzle: 77-92 %
Fuel Flow: 400-600 lbs/hr (Standard Day)
Oil Pressure: 5-20 psi

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4
Q

Idle Thrust (Flight Steady State):
Fuel Flow
Oil Pressure

A

Fuel Flow: 200 Minimum (Standard Day)

Oil Pressure: 5 psi Minimum

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5
Q 
Military Thrust (Ground):
EGT
RPM
Nozzles
Fuel Flow
Oil Pressure
Time
A 
EGT:  630-645 Deg C
RPM:  99-101 %
Nozzles:  0-20 %
Fuel Flow:  2100-2700 lb/hr
Oil Pressure:  20-55 psi
Time:  5 Minutes
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7
Q 
Military Thrust (Flight Steady State):
EGT
RPM
Nozzles
Oil Pressure
Time
A 
EGT:  630-645 Deg C
RPM:  99-104 %
Nozzles:  0-20 %
Oil Pressure:  20-55 psi
Time:  30 Minutes
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9
Q 
Maximum Thrust (Ground):
EGT
RPM
Nozzles
Oil Pressure
Time
A 
EGT:  630-645 Deg C
RPM:  99-101 %
Nozzles:  50-85 %
Oil Pressure:  20-55 psi
Time:  5 Minutes
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10
Q

Maximum Allowable Transient RPM

A

107 %

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11
Q

Landing Gear Speeds

A

Gear down or extending with Gear Doors Open - 240 Knots

Gear Down and Doors Closed - 300 Knots

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12
Q

Nose Wheel Steering

A

Maximum 65 Knots

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13
Q

Canopy Open Speed

A

Maximum 50 Knots

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14
Q

Maximum Mach Number

A

Above FL290: Airframe
Below FL290: .91
Autopilot: .93

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15
Q

Prohibited Maneuvers

A

Vertical Stalls
Spins
Continuous Aileron Rolls limited to 1.0 G and 3/4 Stick Deflection.

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16
Q

Fuel system Limitations (Maximum Thrust)

A

Maximum Thrust Dives with less than 650 lbs of fuel in either fuel supply system
Maximum Thrust Power in zero G flight or at negative load factors exceeding 10 seconds at 10,000 feet or 30 seconds at 30,000 feet.

17
Q

Fuel Without Icing Inhibitor

A

Initial fuel Temperature:
Greater than 50 Deg F: Unrestricted
40 - 50 Deg F: -40 C Minimum SAT at Cruise Altitude
Less than 40 Deg F: Flight Not Recommended

18
Q

Engine Oil System:

Zero and Negative G flight?

A

Zero G flight 10 seconds maximum
Negative G flight 60 seconds maximum
CAUTION: If oil pressure does not recover within approximately 10 seconds, return to normal flight conditions

19
Q

Minimum Time Interval Between Full Stop Landings

A

Gear Retracted in Flight: 45 Minutes

Gear Extended in Flight: 15 Minutes

20
Q

Landing Gear Maximum Ground Speeds (Tire Speeds)

A

Nose Tires: 174 Knots

Main Wheels: 221 Knots

21
Q

Center of Gravity Limitation

A

During solo flight do not allow the Right (aft) system quantity to be more than twice the Left (forward) system fuel quantity

22
Q

EGT Limitations

A 
140 Deg C Minimum
140-630 Deg C Continuous Operation
630-645 Deg C MIL and MAX Thrust Range
645 Deg C Maximum Steady State
925 Deg C Maximum During Start or Acceleration, Momentary
23
Q

Oil Pressure:
Idle
Normal
Maximum

A

5 psi Minimum (idle)
20-55 psi Normal Operating Range
55 psi Maximum

24
Q

Engine Tachometer

A

83-98 % RPM Continuous
99.0 to 104 % RPM (MIL and MAX Thrust Range)
104 % RPM (MIL and MAX Thrust)

25
Q

Oxygen

A

50-120 psi Normal Range

26
Q

Hydraulic Pressure

A

1500 psi Minimum
2850-3200 psi Normal Range
3200 psi Maximum

27
Q

Flap Speeds

A

Flaps Extended 61-100%: 220 Knots
Flaps Extended 41-60%: 240 Knots
Flaps Extended 0-40%: 300 Knots

28
Q

Pod Limits:
Speed
Load

A

400 Knots Maximum with Pod Installed
350 Knot speedbrake limitation with Pod installed
140 lbs Maximum Load

29
Q

G Limitations

A
  • 2.3 to 5.6 G’s Fully Fueled

7. 33 G’s with 900 pounds or less fuel remaining

30
Q 
Maximum Thrust (Flight Steady State):
EGT
RPM
Nozzles
Oil Pressure
Time
A 
EGT:  630-645 Deg C
RPM:  99-104 %
Nozzles:  50-85 %
Oil Pressure:  20-55 psi
Time:  15 Minutes

T-38 Aircraft (3 decks)

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