T-38 DASH-1 SECTION I (OVERVIEW/ENGINES) Flashcards

1
Q

The T-38C aircraft, originally produced by _____, and upgraded by _____, is a ___-place, twin-_____ _____ trainer.

A

originally produced Northrop Corp, upgraded by The Boeing Co., two-place twin-turbojet supersonic trainer

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2
Q

Each cockpit contains an individual _____ canopy and _____.

A

jettisonable canopy and ejection seat

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3
Q

What conditions and pressurizes the air in both cockpits?

A

A cabin air conditioning and pressurization system

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4
Q

The fuselage is an ____ shape, with moderately ____ wings and empennage.

A

area-rule (coke bottle), moderately swept-back

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5
Q

The aircraft is equipped with an all-moveable?

A

horizontal tail

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6
Q

A speed brake is located?

A

on the lower surface of the fuselage center section

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7
Q

The tricycle landing gear has a _____ nosewheel

A

steerable

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8
Q

All flight control surfaces are fully powered by ______?

A

two independent hydraulic systems

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9
Q

The aircraft has a ___º total field-of-view Heads Up Display

A

24º

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10
Q

What is the length of the T-38?

A

46 feet 4 inches

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11
Q

What is the wingspan of the T-38?

A

25 feet 3 inches

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12
Q

What is the height of the T-38?

A

12 feet 11 inches

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13
Q

What is the tread of the T-38?

A

10 feet 9 inches

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14
Q

What is the wheelbase of the T-38?

A

19 feet 5 inches

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15
Q

The gross weight of the aircraft fully serviced with two aircrew is approximately?

A

12,800 pounds

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16
Q

As part of the Propulsion Modernization Program (PMP), the aircraft is powered by two _____ engines.

A

General Electric J85-GE-5R/S engines

17
Q

The General Electric J85-GE-5R/S are ___-stage, ____-flow, ____ engines.

A

eight-stage
axial-flow
turbojet engines

18
Q

Sea level, standard day, static thrust for an installed engine is approximately _____ pounds at MIL power and approximately _____ pounds at full MAX power.

A

2200 pounds MIL
3300 pounds MAX

19
Q

Where does air enter the engine and and where does it to?

A

Air enters through the variable inlet guide vanes, which direct the flow of air into the compressor

20
Q

What assists in regulating compressor airflow to maintain stall-free compressor operation?

A

The automatic positioning of the inlet guide vanes and air bleed valves

21
Q

What are mounted on the same shaft?

A

Two turbine wheels and the compressor rotor stages

22
Q

The exhaust gases are discharged through?

A

a variable area exhaust nozzle

23
Q

What system varies the nozzle area to maintain EGT (Exhaust Gas Temperature) within limits at both MIL and MAX throttle positions?

A

An exhaust gas temperature (T5) sensing system

24
Q

Engine starts require _____, _____ power to energize the ignition holding relay, and ____ power for ignitor firing.

A

compressor motoring (low-pressure air supply), Direct Current (DC) power for the ignition holding relay, and Alternating Current (AC) for ignitor firing

25
Q

For ground starts, a manually operated diverter valve, mounted _____, is positioned by the ground crew to direct the flow of air to the selected engine during the start cycle.

A

mounted on the left engine

26
Q

How many engine start buttons are there and where are they located?

A

Two ENGINE START buttons are located in the left subpanel of each cockpit

27
Q

Momentarily pushing the ENGINE START button for the selected engine arms the ignition circuit (ignition timer and holding relay) for approximately ____ seconds

A

30 seconds

28
Q

What 2 things does moving the throttle to IDLE do during engine start?

A

-energizes the ignition exciter (firing main and afterburner igniters)

-allows starting fuel flow to the engine

29
Q

What does any delay in moving the throttle to IDLE after pushing the ENGINE START button do?

A

Decreases the available ignition time from the 30-second cycle by an equal amount

30
Q

If you were to press the ENGINE START button again during a 30-second cycle, what would it do?

A

Momentarily pressing the ENGINE START button again during a 30-second cycle does NOT reset the ignition timer and start another cycle since the first actuation locks in the cycle (holding relay energized) until the timer expires

31
Q

Without pressing the ENGINE START button, how could you energize the main and afterburner igniters for a 30-second cycle?

A

By moving the throttle to the MAX range.

However, retarding the throttle out of the MAX range at any time during the 30-second cycle stops the igniters from firing and resets the time (the throttle must be retarted from MAX to below MIL)

…more on this in the -1

32
Q

With the throttle at IDLE or above, the igniters can be energized at any time for longer than 30 seconds by?

A

selecting and holding the appropriate ENGINE START button

33
Q

AC power from a ______ can be used for engine starts. For battery starts, the _____ supplies AC power to circuits that provide the right ____ and ____ indications during start cycle

A

battery-operated static inverter; static inverter; fuel flow and oil pressure