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T-38 > EP stuff > Flashcards

EP stuff Flashcards

1
Q

When does the Hydraulic CWS panel light come on?

A

Pressure below 1500 (out at 1800) or high temperature

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2
Q

BAK-15 engagement speeds

A

0-200 knots

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3
Q

MA-1A/MA-1 engagement speeds

A

60-150 knots

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4
Q

When can you expect gear failure when engaging the MA-1A/MA-1 heavyweight?

A

Above 120 knots

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5
Q

What will cause issues when engaging the MA-1A barrier?

A

WSSP installed or Speedbrake Open

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6
Q

If a dual engine failure occurs, attempt to start which one first?

A

Right engine

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7
Q

A compressor stall may be recovered prior to flameout by doing what?

A

Rapidly bringing the throttles to idle and pressing the start button

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8
Q

Heavyweight SSE go-around, what to retract flaps until what airspeed?

A

220 KCAS

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9
Q

Min drag airspeed with a loss of canopy

A

225 KCAS

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10
Q

Touchdowns as high as ___ KCAS have been recorded

A

200 KCAS

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11
Q

How much time will you have if one Hydraulic system fails due to bleed-over

A

35 minutes

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12
Q

Takeoff is prohibited when:

A

RCR is less than 10
Takeoff roll is greater than 80% runway for singleship takeoffs
Takeoff roll is greater than 70% runway for element takeoffs

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13
Q

Rolling takeoffs are only authorized when:

A

Daylight hours

TOLD has been calculated for 300 feet less

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14
Q

Chase formation parameters

A

30-60 degree cone, out to 1,000’

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15
Q

Minimum low approach altitude for chase aircraft

A

300 ft AGL

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16
Q

Can you taxi single engine or with a single generator out?

A

No

17
Q

Abort the start if EGT doesn’t rise within how many seconds after Fuel Flow?

A

12 seconds

18
Q

Abort takeoff if AB doesn’t light in how many seconds?

A

5 seconds

19
Q

When do you retract gear on SSE Go?

A

Final apprach airspeed and when you know you’re not going to hit the ground

20
Q

When do you retract flaps on SSE Go?

A

200 KCAS

21
Q

How to engage a barrier

A

3-point attitude, perpendicular, in a 3-point attitude

22
Q

If flap-slab interconnect fails on takeoff, _____

A

Lighter than normal backstick pressure will be required for rotation
Less stick travel will be required for rotation
Significant forward stick pressure will be required until flaps are retracted

23
Q

Spin recovery procedures

A

1) Full aileron into the direction of the spin with aft stick
2) Rudder full opposite of spin
3) Neutralize controls after recovery

24
Q

Fuel Shutoff Switch Delaty

A

1 second

25
Q

Left AC Bus

A 
RALLFS
Rudder Trim Control
AOA vane heater
Landing/Taxi Lights
Low Fuel Light
Fuel Boost Pump
SAS
26
Q

Right AC Bus

A 
HAMBEFT
HUD
A/C
MDP
Boost Pump
Engine Anti-Ice
Flaps
Trim Control and Light
27
Q

Left Essential DC Bus

A 
CFAST
Crossfeed Valves
Flap Control
AAP
Speed Brake
Transponder
28
Q

Right Essential DC Bus

A 
FUMIN GEAA
Fire Detect Circuits
UHF Radio
MFD
Ignition
Nosewheel Steering
Gear
EED
ADC
Afterburner
29
Q

Non-Essential DC Bus

A 
TUVV
TCAS
UFCP
VTR
VHF Radio
30
Q

LT/RT FUEL PRESS light comes on, and turning on crossfeed extinguishes it, it is probably ______

A

Fuel Leak or Sensor Failure

31
Q

LT/RT FUEL PRESS light comes on, and turning on crossfeed but the light stays on, it is probably ______

A

Boos Pump Failure

32
Q

Compressor Stall Indications (low altitude/high airspeed)

A

Pop, bang, or buzz. Rapid RPM drop or high EGT

33
Q

Compressor Stall Indications (high altitude/low airspeed)

A

Audible chug or pop, decreasing RPM and decreasing EGT

34
Q

Min altitude for Controllability Check

A

6000’ AGL

35
Q

If structural damage is suspected, what airspeed do you fly?

A

20 KCAS above min controllable airspeed

36
Q

Not aerobraking could increase landing roll by how much?

A

50%

37
Q

Where do you land if suspected brake failure but no other indications?

A

Center of runway

38
Q

Max airspeed without canopy

A

300 KCAS

T-38 (10 decks)

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