Good to know Numbers

Question 1

Gross weight with fuel and two souls

Answer 1

12,800 lbs

Question 2

One engine thrust, at rest, MIL and MAX

Answer 2

2200, 3300

Question 3

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

Answer 3

7,300, 11,400 pph

Question 4

Pushing start arms ignition circuit for ____

Answer 4

30s

Question 5

One engine normal oil capacity and air expansion space

Answer 5

4 qt, 1 qt

Question 6

Gravity flow guaranteed up to _____

Answer 6

6,000’ MSL

Question 7

Fuel cutoff switches is operated by ___ and cuts off fuel in ___

Answer 7

DC, 1s

Question 8

Fuel low level light comes on after ___ sec below ___

Answer 8

7.5s, 250lbs

Question 9

Gearbox shift occurs at ___ range

Answer 9

65 - 75%

Question 10

Voltage of battery is ___V and DC rectifiers are ___V

Answer 10

24, 28

Question 11

AC system provides ___/___V power

Answer 11

115/200

Question 12

AC generators cut-in between _____

Answer 12

43 - 48%

Question 13

Min battery voltage of ___ is required to close battery relay

Answer 13

18 V

Question 14

Left engine provides ___ psi for ___ system

Answer 14

3200, utility

Question 15

Right engine provides ___ psi for ___ system

Answer 15

3200, flight control

Question 16

UTILITY/FLIGHT HYDRAULICS comes on at ___ psi, and goes back out at ___ psi

Answer 16

1500, 1800

Question 17

Rudder limited to ___ deg each side when nosegear out 3/4 or less

Answer 17

6°

Question 18

Landing gear extension/retraction takes approx ___

Answer 18

6s

Question 19

Gear horn and warning light come on when gear not down and locked and ≤____
KCAS, altitude ≤___, and both throttles below ___

Answer 19

210, 10,000’, 96%

Question 20

When accelerating, gear light may not go out until ___

Answer 20

240KCAS

Question 21

Landing gear alt release pulled out ___ inches, and requires ___ sec

Answer 21

10, 15-35

Question 22

Rear canopy follows front by ___ after canopy jettison when pulling the outside D-handle

Answer 22

1 s

Question 23

Fuel for left engine is ___ gal serviced/usable and ___ lbs usable

Answer 23

293/286 gal, 1916 lbs

Question 24

Fuel for right engine is ___ gal serviced/usable and ___ lbs usable

Answer 24

305/297 gal, 1990 lbs

Question 25

Total fuel is ___ gal serviced/usable and ___ lbs usable

Answer 25

598/583 gal, 3906 lbs

Question 26

With single-engine and less than ___ in either system, leave both boost pumps on and crossfeed on

Answer 26

250 lbs

Question 27

A minimum of ___ RPM is required to achieve any engine fuel flow (during flight)

Answer 27

12-14%

Question 28

___% RPM is the heart of airstart envelope at any altitude:

Answer 28

18-20%

Question 29

Ignition must occur before fuel flow reaches ___

Answer 29

360 lbs/hr

Question 30

After aborted start, wait ___ min before attempting another start

Answer 30

2

Question 31

If EGT doesn’t rise w/in ___ sec of fuel flow indication, abort start

Answer 31

12

Question 32

Flaps should be +/- ___ of 60% position

Answer 32

5%

Question 33

Normal liftoff speed on initial takeoff is ___

Answer 33

165 KCAS

Question 34

Delay takeoff a min of ___ minutes behind large aircraft or helicopter and ___ behind heavy aircraft

Answer 34

2; 4

Question 35

With a xwind > __ knots, spacing behind large/heavy aircraft may be reduced

Answer 35

5

Question 36

Abort takeoff if either afterburner doesn’t light within ___ sec

Answer 36

5

Question 37

Final turn speed is ___ plus 1 knot per 100 lb over 1000 lb fuel

Answer 37

180 KCAS

Question 38

Final appr speed is ___ plus 1 knot per 100 lb over 1000 lb fuel

Answer 38

160 KCAS

Question 39

Touchdown speed is ___ plus 1 knot per 100 lb over 1000

Answer 39

135 KCAS

Question 40

Minimum Hydraulic pressure ___

Answer 40

1500 psi

Question 41

Each generator is ___ phase

Answer 41

3

Question 42

The O2 low light comes on at or below ___ liter, may blink at or below ___

Answer 42

1; 3

Question 43

Below __, the engine anti-ice is always open, regardless of switch position

Answer 43

65% RPM

Question 44

There are ___ rotating beacons, located where ___

Answer 44

2; top of vertical stabilizer and on the lower fuselage

Question 45

There are ___ position lights, located where ___

Answer 45

4; each wingtip, in the vertical stabilizer, and in the lower fuselage

Question 46

Battery energizes DC bus for ___

Answer 46

15 min

Question 47

The radio attenuation switch reduces UHF and VHF volume by ___

Answer 47

66%

Question 48

IDENT sends a pulse with transponder replies for ___ seconds

Answer 48

15

Question 49

Standby Al provides ___ deg climb, ___ deg dive, ___ deg roll capacity

Answer 49

92; 78, 360

Question 50

Standby AI provides ___ minutes of useful info within +/- ___ deg after DC failure

Answer 50

9; 6

Question 51

Due to oil supply restriction, zero G flight restricted to ___ sec

Answer 51

10

Question 52

Due to oil supply restriction, negative G flight restricted to ___ sec

Answer 52

30

Question 53

Rudder system failure may push rudder to ___ deg

Answer 53

30

Question 54

Stab aug system failure may push rudder to ___ deg

Answer 54

2

Question 55

Touchdown greater than ___ KCAS should not be attempted

Answer 55

200

Question 56

With asymmetric flaps, maintain ___ kts above final appr/touchdown speed

Answer 56

20

Question 57

Do not touchdown at less than ___ KCAS with asymmetric flaps

Answer 57

165

Question 58

On SE go-around, climb only as necessary until reaching ___ KCAS

Answer 58

200

Question 59

When landing with all gear up, touch down ___ kts faster than normal

Answer 59

10

Question 60

Maximum speed for nosewheel on runway

Answer 60

174 KCAS

Question 61

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

Answer 61

8.5; 5.5

Question 62

If flap-slab interconnect fails and flaps needed for landing, ___ % flaps
provides adequate control authority and controllable stick forces

Answer 62

30 - 45%

Question 63

Pressure reg. maintain cabin alt of ___ +/- ___ from ___ alt.to ___ alt

Answer 63

8,000’; 1,000’

8,000’; 23,000’

Question 64

Avoid Max thrust dives when below ___ lb in either fuel tank

Answer 64

650

Question 65

Increase final approach speed and touchdown speed by ___ gust factor

Answer 65

1/2

Question 66

Estimation for landing roll is ___ ft + fuel weight (not including 1000 ft down)

Answer 66

2,500

Question 67

Increase final turn, approach and touchdown by ___ KCAS for no flap

Answer 67

15

Question 68

Landing light retraction takes ___ sec

Answer 68

10

Question 69

AOA max range is ___. Max endurance/best angle of climb is ___

Answer 69

0.18; 0.3

Question 70

Nozzles should stabilize within ___ sec after rapid throttle movements

Answer 70

10

Question 71

Max allowable sink rates for landing: \_\_\_ fpm normal landing and \_\_\_\_ fpm
crab landing (full fuel); and \_\_\_\_, \_\_\_\_\_ for < 1700 lbs fuel

Answer 71

340; 200;

590; 395

Question 72

First 4½” of stick travel provides ___ aileron deflection. Next 1½” of stick travel provides ___ aileron deflection

Answer 72

1/2; full

Question 73

Crossfeed recommended with fuel imbalance of ___ or greater

Answer 73

200 lbs

Question 74

Holding airspeed

Answer 74

250 - 265 KCAS

Question 75

Radar pattern typically burns ___ fuel

Answer 75

325 lbs

Question 76

Turbulent air/thunderstorm penetration speed is ___ KCAS

Answer 76

280

Question 77

Climb possible at SETOS is ___ fpm

Answer 77

100 fpm

Question 78

Climb increased by ___ fpm each kt between SETOS and SETOS + 10 KCAS

Answer 78

8 - 50 fpm

Question 79

Gear retraction may take ___ when retracted between SETOS+ 10 and 200

Answer 79

1 min

Question 80

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

Answer 80

200 KCAS; 220 KCAS

Question 81

Optimum pitch for ejection zoom

Answer 81

20° NH

Question 82

With loss of canopy, slow to ___ KCAS; min drag occurs at ___ KCAS

Answer 82

300; 225

Question 83

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

Answer 83

35

Question 84

Controllability check should be accomplished at ___ or higher

Answer 84

6,000’ AGL

Question 85

Maintain ___ KCAS above min controllable airspeed in descent/landing approach

Answer 85

20

Question 86

Touchdown greater than ___ KCAS should not be attempted

Answer 86

200

Question 87

Use ___ knots as go/no-go for simple tire failure

Answer 87

100

Question 88

Normal rotation speed on initial takeoff is ___:

Answer 88

141 (rounded to 145)

Question 89

Maintain a minimum of ___ RPM to ensure effective anti-ice operation:

Answer 89

80%

Question 90

Landing roll approximately ___ for no flap landing:

Answer 90

Doubled

Question 91

If oil pressure is high in cold weather, should be in limits Win ___:

Answer 91

6 min

Question 92

Minimum/maximum engagement speed for a MA-1 or MA-1A:

Answer 92

60kts / 150kts

Question 93

Maximum engagement speed for BAK-15:

Answer 93

200 kts

Question 94

How long does it take to raise a BAK-15:

Answer 94

5 - 7 seconds