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ENJJPT > T-6 By The Numbers Section VI > Flashcards

T-6 By The Numbers Section VI Flashcards

1
Q

Pitch force during maneuvering flight conditions, aft CGs (lbs/G)

A

9 lbs/G

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2
Q

Pitch force during maneuvering flight conditions, fwd CGs (lbs/G)

A

12 lbs/G

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3
Q

Pull force w/ PCL idle & full nose up trim (lbs)

A

8 lbs

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4
Q

Maximum allowable fuel imbalance (lbs)

A

50 lbs

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5
Q

Maximum flap operating speed (KIAS)

A

150 KIAS

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6
Q

Aileron Roll recommended entry speed (KIAS)

A

180 – 220 KIAS

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7
Q

Wingover/Lazy Eight recommended entry speed (KIAS)

A

200-220 KIAS

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8
Q

Barrel Roll recommended entry speed (KIAS)

A

200-220 KIAS

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9
Q

Clover leaf recommended entry speed (KIAS)

A

200 – 220 KIAS

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10
Q

Chandelle recommended entry speed (KIAS)

A

200-250 KIAS

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11
Q

Loop recommended entry speed (KIAS)

A

230 – 250 KIAS

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12
Q

Cuban Eight recommended entry speed (KIAS)

A

230 – 250 KIAS

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13
Q

Immelmann recommended entry speed (KIAS)

A

230-250 KIAS

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14
Q

Split-S recommended entry speed (KIAS)

A

120-140 KIAS

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15
Q

Inverted flight recommended entry speed (KIAS)

A

180 – 200 KIAS

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16
Q

Greatest yawing tendency, uncoordinated rolling pullouts G loading (G)

A

2 G

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17
Q

Uncoordinated rolling pull out, roll input limit with greater than +2 G (stick deflection)

A

½ stick

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18
Q

Maximum bank angle change for uncoordinated rolling maneuvers at -1 G (deg)

A

180 deg

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19
Q

Best glide speed, clean configuration (KIAS)

A

125 KIAS

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20
Q

Best glide sink rate, clean (fpm)

A

1350 fpm

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21
Q

Best glide speed, landing gear down, flaps/speed brake up (KIAS)

A

105 KIAS

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22
Q

Best glide sink rate, gear down, flaps/speed brake up (fpm)

A

1500 fpm

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23
Q

Turbulent air penetration speed, Vg (KIAS)

A

195 KIAS

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24
Q

Severe windshear airspeed changes (KIAS)

A

> 15 KIAS

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25
Q

Severe windshear vertical speed changes (fpm)

A

> 500 fpm

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26
Q

Microburst duration (mins)

A

2-5 mins

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27
Q

Microburst area diameter (miles)

A

2 miles

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28
Q

Microburst downdraft velocity (fpm)

A

In excess of 6000 fpm

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29
Q

Zero thrust power setting (% torque)

A

4 – 6% torque

30
Q

Stick shaker activation speed above stall (KIAS)

A

5 – 10 KIAS

31
Q

Natural stall warning speed above stall (KIAS)

A

3 KIAS

32
Q

Pitch possible during entry to wings-level stall and 100% torque (deg)

A

45 deg NH

33
Q

Full right rudder and right aileron above ___ % torque may not prevent left roll-off at stall

A

60 % toque

34
Q

Inverted stall pitch nose above horizon, 100% torque (deg)

A

30 deg NH

35
Q

Maximum sustained heavy buffet G loading (G)

A

3 G’s

36
Q

Wings-level stall altitude loss (ft)

A

100 ft

37
Q

Length of incipient spin phase (# of turns)

A

Approximately 2 turns

38
Q

Altitude loss during typical steady-state, 6-turn spin (ft)

A

4500 ft

39
Q

Spiral airspeed (KIAS)

A

Increasing through 160 KIAS

40
Q

Increasing through 160 KIAS

A

80 KIAS

41
Q

Maximum spin entry pitch attitude (deg)

A

50 deg NH

42
Q

Minimum spin altitude (ft PA)

A

10,000 ft MSL

43
Q

Propeller stressed (% Np)

A

40 psi

44
Q

Minimum spin oil pressure, pcl idle (psi)

A

40 psi

45
Q

Nose pitch in erect spins (deg)

A

Approximately 60 deg NL

46
Q

Near steady-state turns (#)

A

3

47
Q

Erect spin stabilized rotation rate (sec/turn)

A

2 to 3 sec/turn

48
Q

Erect spin altitude loss (ft/turn)

A

400 to 500 ft/turn

49
Q

Erect spin angle of attack (units AOA)

A

18+ units AOA

50
Q

Erect spin stabilized airspeed (KIAS)

A

120 – 135 KIAS

51
Q

Roll and yaw oscillations in spins after ___ (# of turns)

A

3

52
Q

of turns for progressive spin reversal (# of turns)

A

1.5 to 2 turns

53
Q

Progressive spin airspeed during reversal (KIAS)

A

175 (KIAS)

54
Q

Aggravated spin pitch attitude (deg)

A

Approximately 70 deg NL

55
Q

Aggravated spin roll rate (deg/sec)

A

280 deg/sec

56
Q

Maximum aggravated spin turns (#)

A

2

57
Q

Aggravated spin testing conducted to (# of turns)

A

4

58
Q

Inverted spin entry pitch attitude (deg)

A

60 – 90 deg NH

59
Q

Inverted spin entry speed (KIAS)

A

50 KIAS

60
Q

Inverted spin stabilized turn rate (deg/sec)

A

120 deg/sec

61
Q

Inverted spin number of turns until stabilized (#)

A

2

62
Q

Inverted spin pitch oscillations about (deg)

A

30 deg NL

63
Q

Inverted spin airspeed (KIAS)

A

40 KIAS

64
Q

Normal inverted spin acceleration (G)

A

-1.5 G

65
Q

Inverted spin AOA (units AOA)

A

0 units AOA

66
Q

Push force required to move stick well forward of neutral (lbs)

A

50 lbs

67
Q

Spinning ceases after applying controls (# of turns)

A

1.5 turns

68
Q

Spin altitude loss (ft/turn)

A

1500-2000 ft

69
Q

Controls neutral spin recovery spin rotation ceases (# of turns)

A

Within 2 additional turns

70
Q

Dive recovery reaction time (seconds)

A

3 seconds

ENJJPT (4 decks)

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