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T38 Dash 1 - Section III > General Info > Flashcards

General Info Flashcards

1
Q

What is meant by “land as soon as possible”?

A

An emergency will be declared. A landing should be accomplished at the nearest suitable airfield considering the severity of the emergency, weather conditions, field facilities, ambient lighting, aircraft gross weight, and command guidance.

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2
Q

What is meant by “land as soon as practical”?

A

Emergency conditions are less urgent and, although the mission is to be terminated, the degree of the emergency is such that an immediate landing at the nearest adequate airfield may not be necessary.

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3
Q

What is a “general emergency procedure”?

A

All reasonably expected emergencies that could occur in two or more phases of operation or affect two or more systems or subsystems

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4
Q

What color is the “altitude” warning/caution, and what is indicated by it?

A

Red

Altitude below minimum altitude set on UFCP ALT Key Display

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5
Q

What color is the “gear” warning/caution, and what is indicated by it?

A

Red

  1. Landing gear not down and locked with
    a. Decelerating airspeed 210 KCAS or less
    b. Altitude below 10000’
    c. Both throttles below 96% rpm
  2. Landing gear handle up and doors not down and locked.
  3. Landing gear handle down and gear not down and locked.
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6
Q

What color is the “stall” warning/caution, and what is indicated by it?

A

Red

Landing gear extended and AOA at or above 0.80

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7
Q

What color is the “canopy” warning/caution, and what is indicated by it?

A

Red

Canopy not fully closed and locked

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8
Q

What is indicated by the ENG ANTI-ICE ON advisory?

A

ENG ANTI-ICE Switch is in the MAN ON position

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9
Q

What is indicated by the LEFT/RIGHT FUEL PRESS cautions? (6 things)

A
  • Low fuel pressure
  • Loss of boost pump (note - reset boost pump CB only one time)
  • Fuel leak
  • Fuel line leak
  • Generator phase failure
  • Surging of engine driven pump
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10
Q

What is indicated by the FUEL LOW caution?

A

Either fuel quantity indicator reads <250 lbs for 7.5 seconds

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11
Q

What is indicated by the LEFT/RIGHT GENERATOR cautions?

A
  • Designated generator offline

- Either generator can support the total aircraft electrical load

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12
Q

What is indicated by the FLIGHT/UTILITY HYDRAULIC cautions?

A

Hydraulic System

  • Fluid overtemperature or
  • Low pressure
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13
Q

What is indicated by the OXYGEN cautions?

A

Oxygen indicator reads 1 liter or less of LOX

Light may blink due to sloshing if system contains less than 3 liters

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14
Q

What is indicated by the XMFR RECT OUT cautions?

A

Failure of both TRUs

DC-powered systems supplied by aircraft battery

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15
Q

What is indicated by the AVIONICS caution?

A

Failure of avionics system listed on PFL

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16
Q

What is indicated by the BINGO caution?

A

Fuel below bingo bug setting

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17
Q

What is indicated by the CAUTION caution?

A

MASTER CAUTION light is lit

18
Q

What is indicated by the DESCEND caution?

A

Beginning of the descent phase of a Divert Profile in Emegency Divert Mode

19
Q

What is indicated by the ENGINE caution? (5 possible things)

A
  • Left/right RPM exceedance
  • Left/right oil pressure high or low caution
  • Latched left/right EGT overtemp
  • Latched left/right oil pressure high or low
  • Engine sensor failure
20
Q

What is indicated by the FLAPS caution?

A

Airspeed has approached or exceeded the allowable limit for current flap setting:

  • 290 for 6 to 50% flaps
  • 230 for 50 to 65% flaps
  • 210 knots for flaps > 65%
21
Q

What is indicated by the OVER G caution?

A

Aircraft G-load value exceeded 100% of Max G limit

22
Q

What is indicated by the “EGI Status Messages: WAIT, DEGRADED, FULL, NO GPS, NAV, LEVEL, ATT” advisory?

A

Current state of EGI

23
Q

What is indicated by the GEAR voice message

A

Landing gear is down and locked and the airspeed is greater than 240 KCAS

or the nose gear is down and locked and the airspeed is between 220 and 240 KCAS and increasing by 2 kts/sec and groundspeed is also increasing

24
Q

If you get an EED hot PFL what will happen?

A

Affected display dims 50% if in Day mode and EED hot is displayed. If the hot condition persists, the EED display blanks 1 minute after PFL is generated. Engine data continues to be reliable

25
Q

What PFL will you get if you don’t get RAIM?

A

GPS INTEGRITY FAILURE

26
Q

What PFL will you get if you don’t get PRAIM?

A

GPS APPROACH NOT AVAILABLE: LIMITED SATELLITE AVAILABILITY

27
Q

What color is brake fluid?

A

Red

28
Q

With a brake system malfunction (fluid venting), what is one thing you might want to try on landing roll that shouldn’t be attempted in flight?

A

Pumping the brakes

If brake failure is encountered on landing roll, braking action may be regained by repeatedly pumping the brakes. The pedals should be released to the full up position between strokes.

Do not pump the brakes in flight as this action could introduce air into the brake system which could result in complete brake failure.

29
Q

What should you do any time the aircraft departs a hard surface?

A

Immediately shut down both engines

30
Q

With a lost or damaged canopy, it is imperative to ___. Why?

A

Confirm the speed brake is closed?

The combined total drag of canopy and speed brake could require AB to sustain level flight.

31
Q

How much drag is generated due to a lost front canopy?

A

Approximately one-half the drag of a fully extended speed brake

32
Q

With a loss of canopy, what airspeed does minimum drag occur at?

A

225 KCAS

33
Q

What altitudes and airspeeds should the US16T-1 and US16T-2 provide safe escape at?

A

0-0 to basically any airspeed or altitude that the aircraft can fly at…

34
Q

During an ejection at sea level, “medium” forces will be exerted on the body up to what airspeed?

A

450 KCAS (0.7 Mach)

35
Q

During an ejection at sea level, “severe” forces will be exerted on the body between what airspeeds?

A

450 (0.7 Mach) and 600 KCAS (0.9 Mach)

36
Q

During an ejection at sea level, “excessive” forces will be exerted on the body above what airspeed?

A

600 KCAS (0.9 Mach)

37
Q

What weight of person is the ejection seat designed for without gear? With gear?

A

103 to 245 nude body weight

125 to 272 with flight gear

38
Q

What is the optimum speed for ejection?

A

200-300 KCAS

39
Q

Usually below ___ feet, automatic parachute deployment and aircrew/seat seperation sequence has occured unless the barometric controlled g switch has operated to delay parachute until speed and g forces are reduced

A

15000’

40
Q

If below ____, AGL and aircrew/seat separation has not occured automatically, initiate the separation manually.

A

12000’ AGL

41
Q

What is the recommended safe ejection altitude condition?

A

2000 to 4000 AGL

T38 Dash 1 - Section III (12 decks)

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