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38: Quick Thinking > T38 Good To Know Numbers > Flashcards

T38 Good To Know Numbers Flashcards

1
Q

Gross weight with fuel and two sounds?

A

12,800 lbs

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2
Q

Thrust produced by a single engine in MIL and MAX?

A

2200

3300

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3
Q

Fuel flow for one engine, MAX at rest and at Mach 1 at sea level?

A

Rest: 7300 lb/hr

Mach 1 Sea Level: 11,400 lb/hr

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4
Q

How long does pushing the start button arm the ignition circuit for?

A

30 seconds

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5
Q

Normal oil capacity and air expansion space?

A

4 qt

1 qt

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6
Q

Gravity flow guarantees flow up to what altitude?

A

6000’

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7
Q

How fast can the fuel shutoff switches shut off fuel flow?

A

1 sec

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8
Q

Fuel low light comes on after ____ seconds below ____?

A

7.5 seconds

250 lbs

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9
Q

Gearbox shift range

A

65-75%

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10
Q

Battery voltage

A

24 V

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11
Q

Voltage produced from the TRUs

A

28 V

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12
Q

AC power voltage

A

115-200V

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13
Q

Generator cut in speed

A

43-48%

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14
Q

Minimum voltage required to close battery relay?

A

18V

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15
Q

Hydr Pressure light comes on at ______ PSI

It goes out at _____ PSI

A

1500 PSI

1800 PSI

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16
Q

Rudder is limited to 6 deg when?

A

When nosegear is out 3/4 or less

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17
Q

Landing gear extension /retraction takes approx ____?

A

6 seconds

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18
Q

Gear horn and warning light comes on when gear is not down and locked and:

A
  • Less than 210 knots
  • Below 10,000 ft
  • Both throttles below 96%
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19
Q

How far do you have to pull out the alternate gear release?

A

10 inch

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20
Q

How long does an alternate gear extension take ?

A

15-35 seconds

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21
Q

Rear canopy follows the front canopy by _____ after canopy jettison?

A

1 sec

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22
Q

Aneroid delays parachute opening until between?

A

15,000’ and 11,500’

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23
Q

Seat ejections occurs ____ after canopy jettison?

A

0.3 sec

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24
Q

Fuel left engine is ____ gal serviced/usable and _____ lbs useable

A

293/286

1916 lbs

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25
Q

Fuel right engine is ____ gal serviceable/useable and ______ lbs useable

A

305/297

1990 lbs

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26
Q

Total fuel ______ gal serviceable/useable and ____ lbs useable?

A

598/583 gal

3906 lbs

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27
Q

With single-engine and less than ___ in either system, leave both boost pumps _____ and cross feed ____

A

250 lbs
On
On

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28
Q

Minimum RPM to achieve any engine fuel flow?

A

12-14%

29
Q

Heart of the airstart RPM envelope?

A

18-20%

30
Q

Ignition must occur before fuel flow reaches ____

A

360 lb/hr

31
Q

After an aborted start, wait ______ before another attempted start

A

2 min

32
Q

Normal rotation speed is

A

141 knots (rounded to 145)

33
Q

Delay a minimum of _____ behind a large aircraft and _____ behind a heavy aircraft

A

2 minutes

4 minutes

34
Q

At _____ knots of crosswind, you can reduce spacing behind large/heavy aircraft

A

5 knots

35
Q

Abort takeoff if either afterburner doesn’t light within _____ seconds

A

5

36
Q

Below ____ RPM, the engine anti-ice is always on, regardless of switch position

A

65%

37
Q

How many rotating beacons are there and where are they located?

A

2

Tail and lower fuselage

38
Q

How many position lights are there and where are they located?

A

4

Tail, lower fuselage, each wing

39
Q

Battery energizes the DC bus for how long?

A

15 mins at 80% charge

40
Q

If the oil pressure is high in cold weather, how long should it take for it to be within limits

A

6 minutes

41
Q

The radio attenuation switch reduces UHF and VHF volume by ____

A

66%

42
Q

How long does IDENT send a pulse for?

A

15 secnods

43
Q

Standby ADI provides useful info for ____ and within _____ after a DC failure

A

9 minutes

+/- 6 degrees

44
Q

Minimum engine RPM for effective anti ice operation

A

80%

45
Q

Restrict zero G flight to ____

A

10 seconds

46
Q

Restrict negative G flight for ____

A

30 sec

47
Q

Stab Augmentor can change rudder position by _____ deg

A

2 deg

48
Q

Touchdown greater than _____ knots should not be attempted

A

200 KCAS

49
Q

Maintain ____ knots above final approach speed with an asymmetric flap failure

A

20 knots

50
Q

Do not touchdown less than ______ knots with an asymmetric flap failure

A

165 knots

51
Q

On a SE-Go around, climb only as necessary until _____ knots

A

200 knots

52
Q

Touchdown _______ knots faster during a gear up landing

A

10 knots

53
Q

Anti-ice will cause a loss of _____ % thrust in MIL and ____ % in MAX

A
  1. 5% in MIL

5. 5% in MAX

54
Q

Pressure regulator maintains cabin altitude of _____ +/- ______ from _______ alt to ______ alt

A

8,000’ +/- 1000’

8,000’ to 23,000’

55
Q

Avoid max thrust dives when below _____ in either tank

A

650 lbs

56
Q

How long does it take for full parachute deployment?

A

3.42 seconds

57
Q

Landing light retractions takes ___ seconds

A

10

58
Q

Max range AOA

A

0.18

59
Q

Max endurance AOA

A

0.3

60
Q

Crossfeeding is recommended for fuel imbalances of _____ or greater

A

200 lbs

61
Q

Holding airspeed

A

250 to 265 kts

62
Q

Typical fuel burn in a radar pattern

A

325 lbs

63
Q

Turbulent air penetration speed

A

280 kts

64
Q

If unable to retract gear, best climb at _____ for 60% and _____ for 0% flaps

A

200 kts

220 kts

65
Q

Optimum pitch for ejection zoom

A

20 degrees nose high

66
Q

With loss of canopy, slow to _____ knots; minimum drag occurs at _____

A

300 knots slow to

225 knots minimum drag

67
Q

If one hydr system reads zero, hydr system transfer may occur, and flight time could be limited to ___ mins

A

35

68
Q

Controllability check should be accomplished at ______ AGL or higher

A

6,000 ft

69
Q

Maintain ____ knots above min controllable airspeed in descent/landing approach

A

20 knots

38: Quick Thinking (7 decks)

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