T-6 By The Numbers Section VI

Question 1

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

Answer 1

9 lbs/G

Question 2

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

Answer 2

12 lbs/G

Question 3

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

Answer 3

8 lbs

Question 4

Maximum allowable fuel imbalance (lbs)

Answer 4

50 lbs

Question 5

Maximum flap operating speed (KIAS)

Answer 5

150 KIAS

Question 6

Aileron Roll recommended entry speed (KIAS)

Answer 6

180 – 220 KIAS

Question 7

Wingover/Lazy Eight recommended entry speed (KIAS)

Answer 7

200-220 KIAS

Question 8

Barrel Roll recommended entry speed (KIAS)

Answer 8

200-220 KIAS

Question 9

Clover leaf recommended entry speed (KIAS)

Answer 9

200 – 220 KIAS

Question 10

Chandelle recommended entry speed (KIAS)

Answer 10

200-250 KIAS

Question 11

Loop recommended entry speed (KIAS)

Answer 11

230 – 250 KIAS

Question 12

Cuban Eight recommended entry speed (KIAS)

Answer 12

230 – 250 KIAS

Question 13

Immelmann recommended entry speed (KIAS)

Answer 13

230-250 KIAS

Question 14

Split-S recommended entry speed (KIAS)

Answer 14

120-140 KIAS

Question 15

Inverted flight recommended entry speed (KIAS)

Answer 15

180 – 200 KIAS

Question 16

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

Answer 16

2 G

Question 17

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

Answer 17

½ stick

Question 18

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

Answer 18

180 deg

Question 19

Best glide speed, clean configuration (KIAS)

Answer 19

125 KIAS

Question 20

Best glide sink rate, clean (fpm)

Answer 20

1350 fpm

Question 21

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

Answer 21

105 KIAS

Question 22

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

Answer 22

1500 fpm

Question 23

Turbulent air penetration speed, Vg (KIAS)

Answer 23

195 KIAS

Question 24

Severe windshear airspeed changes (KIAS)

Answer 24

> 15 KIAS

Question 25

Severe windshear vertical speed changes (fpm)

Answer 25

>500 fpm

Question 26

Microburst duration (mins)

Answer 26

2-5 mins

Question 27

Microburst area diameter (miles)

Answer 27

2 miles

Question 28

Microburst downdraft velocity (fpm)

Answer 28

In excess of 6000 fpm

Question 29

Zero thrust power setting (% torque)

Answer 29

4 – 6% torque

Question 30

Stick shaker activation speed above stall (KIAS)

Answer 30

5 – 10 KIAS

Question 31

Natural stall warning speed above stall (KIAS)

Answer 31

3 KIAS

Question 32

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

Answer 32

45 deg NH

Question 33

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

Answer 33

60 % toque

Question 34

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

Answer 34

30 deg NH

Question 35

Maximum sustained heavy buffet G loading (G)

Answer 35

3 G’s

Question 36

Wings-level stall altitude loss (ft)

Answer 36

100 ft

Question 37

Length of incipient spin phase (# of turns)

Answer 37

Approximately 2 turns

Question 38

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

Answer 38

4500 ft

Question 39

Spiral airspeed (KIAS)

Answer 39

Increasing through 160 KIAS

Question 40

Increasing through 160 KIAS

Answer 40

80 KIAS

Question 41

Maximum spin entry pitch attitude (deg)

Answer 41

50 deg NH

Question 42

Minimum spin altitude (ft PA)

Answer 42

10,000 ft MSL

Question 43

Propeller stressed (% Np)

Answer 43

40 psi

Question 44

Minimum spin oil pressure, pcl idle (psi)

Answer 44

40 psi

Question 45

Nose pitch in erect spins (deg)

Answer 45

Approximately 60 deg NL

Question 46

Near steady-state turns (#)

Answer 46

3

Question 47

Erect spin stabilized rotation rate (sec/turn)

Answer 47

2 to 3 sec/turn

Question 48

Erect spin altitude loss (ft/turn)

Answer 48

400 to 500 ft/turn

Question 49

Erect spin angle of attack (units AOA)

Answer 49

18+ units AOA

Question 50

Erect spin stabilized airspeed (KIAS)

Answer 50

120 – 135 KIAS

Question 51

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

Answer 51

3

Question 52

of turns for progressive spin reversal (# of turns)

Answer 52

1.5 to 2 turns

Question 53

Progressive spin airspeed during reversal (KIAS)

Answer 53

175 (KIAS)

Question 54

Aggravated spin pitch attitude (deg)

Answer 54

Approximately 70 deg NL

Question 55

Aggravated spin roll rate (deg/sec)

Answer 55

280 deg/sec

Question 56

Maximum aggravated spin turns (#)

Answer 56

2

Question 57

Aggravated spin testing conducted to (# of turns)

Answer 57

4

Question 58

Inverted spin entry pitch attitude (deg)

Answer 58

60 – 90 deg NH

Question 59

Inverted spin entry speed (KIAS)

Answer 59

50 KIAS

Question 60

Inverted spin stabilized turn rate (deg/sec)

Answer 60

120 deg/sec

Question 61

Inverted spin number of turns until stabilized (#)

Answer 61

2

Question 62

Inverted spin pitch oscillations about (deg)

Answer 62

30 deg NL

Question 63

Inverted spin airspeed (KIAS)

Answer 63

40 KIAS

Question 64

Normal inverted spin acceleration (G)

Answer 64

-1.5 G

Question 65

Inverted spin AOA (units AOA)

Answer 65

0 units AOA

Question 66

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

Answer 66

50 lbs

Question 67

Spinning ceases after applying controls (# of turns)

Answer 67

1.5 turns

Question 68

Spin altitude loss (ft/turn)

Answer 68

1500-2000 ft

Question 69

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

Answer 69

Within 2 additional turns

Question 70

Dive recovery reaction time (seconds)

Answer 70

3 seconds