C-17 By The #’s Flash

Question 1

___ engine starts are permitted without a cooling period. A ___ minute cooling period is required prior to the 3rd attempt. Subsequent attempts require a ___ minute cooling period. Maximum of ___ start attempts per hour, then a ___ hour cooling period is required.

Answer 1

2 , 15 , 10 , 5 , 1

Question 2

Motor the engine for ___ seconds to clear the engine following stop start or shutdown. If disengaged, the starter may be re-engaged below ___ % N2 for clearing. For a subsequent start, delay starter engagement for at least ___ seconds after N2 rotation has stopped. When engine cooling is required, motor starter until EGT is less than ___ C.

Answer 2

30 , 20 , 40 , 190

Question 3

The engine may be motored (fuel/ignition off) for a Max of ___ minutes. Other than the Engine Clearing Procedure, if the engine is motored < ___ seconds, it will be considered one start attempt. For durations > ___ seconds, the starter should be cooled ___ minutes for each ___ seconds of operation up to a Max of ___ minutes.

Answer 3

15 , 90 , 90 , 5 , 30 , 40

Question 4

The N2 range for introducing fuel during engine start is ___ to ___ %.

Answer 4

18, 24

Question 5

The normal fuel flow for engine start is approximately ___ to ___ lbs/hr, but if you see ___ lbs/hr or greater the potential for hot start exists.

Answer 5

400, 500 ,700

Question 6

The Min recommended air pressure for and APU start is ___ psi, crossbleed is ___ psi, and external air is ___ psi.

Answer 6

20 , 25 , 30

Question 7

Starting the engines in IDLE REV is recommended for tailwinds exceeding ___ kts.

Answer 7

25

Question 8

___ minutes of time is required between APU starter cycles, with a maximum of ___ start attempts per hour.

Answer 8

5, 3

Question 9

___ minutes of time is required between APU starter cycles, with a maximum of ___ start attempts per hour.

Answer 9

51, 55

Question 10

The Max engine EGT during the engine start sequence is ___ C

Answer 10

495

Question 11

An engine is stabilized when N1 = ___ % and N2 = ___ %

Answer 11

24 +/-3

60 +/-5

Question 12

The Min engine oil temperature for takeoff is ___ C

Answer 12

50

Question 13

The normal operating engine oil quantity is ___ to ___ quarts, with a Min oil quantity of ___ quarts.

Answer 13

4, 23, 4

Question 14

The Min oil pressure on the ground is ___ psi; the Min oil pressure in-flight is ___ psi.

Answer 14

70, 80

Question 15

The Max engine EGT for continuous engine operation (MCT/INT) is ___ C, with operation above limited to ___ minutes.

Answer 15

625, 5

Question 16

The Max transient engine EGT for INT is ___ C for ___ seconds.

Answer 16

640, 5

Question 17

The Max engine EGT for MAX/DRT is ___ C for ___ minutes, or ___ minutes at MAX for engine failure or engine out go-around for obstacle clearance.

Answer 17

655 , 5 , 10

Question 18

Max static ramp weight is _____ lbs and Max weight for taxi is _____ lbs.

Answer 18

615,000 ; 586,000

Question 19

Max weight for takeoff/landing is _____ lbs.

Answer 19

585,000

Question 20

Max in-flight weight including air refueling is _____ lbs.

Answer 20

585,000

Question 21

Max Zero Fuel weight is _____ lbs.

Answer 21

447,400

Question 22

Max full flap landing weight is _____ lbs.

Answer 22

502,100

Question 23

Max ramp/takeoff/landing weight for a semi-prepared airfield with normal tire pressure is _____ lbs.

Answer 23

486,000

Question 24

Max fuel for ground operations on a semi-prepared surface with normal tire pressure is _____ lbs.

Answer 24

92,000

Question 25

Max fuel capacity (non-ER) is approximately _____ lbs; Max fuel capacity (ER) is approximately _____ lbs.

Answer 25

181,000 ; 245,000

Question 26

The Max allowable fuel imbalance between wings is _____ lbs.

Answer 26

8,000

Question 27

Max fuel capacity for normal brake operations at main gear touchdown is < _____ lbs or < _____ lbs total in ER tanks.

Answer 27

165,000 ; 4,000

Question 28

Max speed with less than 16,000lbs total fuel is _____ KCAS or _____ Mach.

Answer 28

300 , 0.825

Question 29

The normal hydraulic system quantities for system 1-4 are ___, ___, ___, ___ gallons respectively.

Answer 29

7.2 , 11.7 , 7.4 , 7.2

Question 30

The Min hydraulic system quantities for system 1-4 are ___, ___, ___, ___ gallons respectively.

Answer 30

4.9 , 9.4 , 4.9 , 4.9

Question 31

The normal hydraulic system pressure with all pumps operating is _____ psi.

Answer 31

4,000

Question 32

The Max hydraulic system pressure is _____ psi.

Answer 32

4,200

Question 33

The normal auxiliary hydraulic pump pressure is _____ psi.

Answer 33

3,850

Question 34

The primary and secondary hydraulic pump low pressure light comes when system pressure drops below _____ psi.

Answer 34

3,400

Question 35

The auxiliary hydraulic pump low pressure light comes on when system pressure drops below _____ psi.

Answer 35

2,200

Question 36

The Min hydraulic system temperature for takeoff is _____ C

Answer 36

7

Question 37

The Min brake pressure is ___ psi.

Answer 37

1,000

Question 38

The Caution brake temp range is ___ to ___ C. Fuse plugs may release causing potential damage to wheels and tires; takeoff is not recommended.

Answer 38

651 , 750

Question 39

The Max brake temp is ___ C. Above this temperature fuse plugs will release, fires are possible; takeoff is not permitted.

Answer 39

750

Question 40

The Max brake temp for training ALZ landing operations is ___ C.

Answer 40

150

Question 41

For every ___ consecutive landings, you must cool your gear; ___ minutes if you leave the gear down or ___ minutes if gear is retracted.

Answer 41

4 , 10 , 20

Question 42

The Max cabin pressure Delta P is ___ psi

Answer 42

7.8

Question 43

The normal crew oxygen pressure is ___ to ___ psi.

Answer 43

285 to 430

Question 44

The crew oxygen quantity low light comes on when pressure drops below ___ liters or ___ psi.

Answer 44

5 , 60 +/-5

Question 45

The passenger/auxiliary oxygen quantity low light comes on when system pressure drops below ___ liters or ___ psi.

Answer 45

7.5 , 60 +/-5

Question 46

The Max airspeed clean is ___ KCAS or ___ Mach.

Answer 46

350 , 0.825

Question 47

The Max airspeed to extend the slats is ___ KCAS or ___ Mach.

Answer 47

280 , 0.62

Question 48

The Max airspeed to retract the slats is ___ KCAS or ___ Mach.

Answer 48

270, 0.62

Question 49

The Max airspeed to lower the landing gear is ___ KCAS or ___ Mach.

Answer 49

250 , 0.62

Question 50

The Max airspeed to retract the landing gear is ___ KCAS or ___ Mach.

Answer 50

225 , 0.62

Question 51

The landing gear may not fully retract above ___ KCAS; if it does not, extend the gear, slow below ___ KCAS and retract the gear.

Answer 51

200 , 200

Question 52

The Max airspeed for 1/2 flaps is ___ KCAS or ___ Mach.

Answer 52

250 , 0.62

Question 53

The Max airspeed for 3/4 flaps is ___ KCAS or ___ Mach.

Answer 53

190 , 0.62

Question 54

The Max airspeed for full flaps is ___ KCAS or ___ Mach.

Answer 54

175 , 0.62

Question 55

At or near retract limit speed, or ___ KCAS above vMSR at any gross weight, the outboard slats may be slow to retract and/or retract asymmetrically.

Answer 55

20

Question 56

Anytime slats or flaps are extended, the abrupt rolling pushover/pull-up load limits are ___ to ___ g's.

Answer 56

1.6 to 0.4

Question 57

The Max airspeed for thrust reversers in-flight is ___ KCAS or ___ Mach; the Max on the ground is ___ KCAS.

Answer 57

350 , 0.825 , 182

Question 58

The Min airspeed to prevent the RAT from stalling when required for hydraulic pressure is ___ KCAS

Answer 58

130

Question 59

The Max airspeed for opening troop doors or cargo door/ramp is ___ KCAS or ___ Mach.

Answer 59

250, 0,62

Question 60

The Max airspeed for opening a pilot window is ___ KCAS or ___ Mach.

Answer 60

205 , 0.62

Question 61

The Max taxi speed on a prepared surface is ___ knots

Answer 61

40

Question 62

The Max taxi speed on a semi-prepared surface is ___ knots if aircraft weight is < = _____ lbs.

Answer 62

30 ; 435,000

Question 63

The Max taxi speed on a semi-prepared surface is ___ knots if aircraft weight is > _____ to < =_____ lbs.

Answer 63

20 ; 435,000 ; 447,000

Question 64

The Max taxi speed on a semi-prepared surface is ___ knots if aircraft weight is > _____ lbs.

Answer 64

15 ; 447,000

Question 65

The Max allowed nose wheel steering is ___ degrees when aircraft weight is > _____ lbs, or total fuel is > _____ lbs and taxi speed is > ___ knots or > ___ knots with asymmetric thrust.

Answer 65

20 , 490,000 ; 165,000 20 , 15

Question 66

The Min required runway length (without waiver) is _____ feet; or as required for CFL, landing distance, or ground roll +500 feet.

Answer 66

3,500

Question 67

The Min required runway width is _____ feet.

Answer 67

90

Question 68

The Min required taxiway width is _____ feet

Answer 68

50

Question 69

The Min required taxiway width for star turn is _____ feet.

Answer 69

90

Question 70

The Max headwind for takeoff or landing is ___ knots

Answer 70

40

Question 71

The Max crosswind for takeoff or landing is ___ knots.

Answer 71

30

Question 72

The Max tailwind for takeoff or landing is ___ knots.

Answer 72

10

Question 73

The Max crosswind for touch and go is ___ knots.

Answer 73

25

Question 74

The Max crosswind for NVG departure or approach on a 90 to 120 foot wide runway is ___ knots.

Answer 74

15

Question 75

The Max crosswind for NVG departure or approach on a > 120 foot wide runway (without waiver) is ___ knots

Answer 75

20

Question 76

The Max crosswind for NVG training departure or approach is ___ knots

Answer 76

15

Question 77

The Max crosswind for CAT II ILS approach in training is ___ knots and operational is ___ knots.

Answer 77

15, 10

Question 78

The level off from a tactical descent should be initiated approximately _____ feet above desired altitude

Answer 78

2,000

Question 79

The Max touchdown sink rate for a landing with aircraft weight > 502,100 lbs is ___ ft/min.

Answer 79

600

Question 80

The Max touchdown sink rate for a landing with aircraft weight < 502,100 lbs but > 435,800 is ___ ft/min.

Answer 80

660

Question 81

The Max touchdown sink rate for a landing with aircraft weight < 435,800 lbs is ___ ft/min.

Answer 81

750

Question 82

The Max outside air temperature (OAT) for takeoff is ___ C, but operations at ___ C or above may result in EFCS reversion to FROZEN GAINS

Answer 82

49, 43