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F-16 BL 42 > Transition Phase > Flashcards

Transition Phase Flashcards

1
Q

always adjust the ______ prior to battery power to prevent inadvertently bleeding the ________

A

rudder pedals, JFS accumulators

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2
Q

always complete the VERIFY checklist prior to _________

A

applying battery power

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3
Q

after applying battery power, wait _____ to start the JFS to complete the ______ check

A

30 seconds, HYD/OIL warning light

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4
Q

hot wx ops: start with canopy _____ open, until idle

A

6 inches

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5
Q

motor engine with the JFS for _______

A

1 minute

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6
Q

EPU check: the EPU must run on AIR for _____ to be valid

A

5 seconds

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7
Q

the guard ramp is ________

A

uncontrolled

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8
Q

taxi speed ramp / congested area should not exceed _____

A

10 kts

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9
Q

Max taxi speed uncontested areas

A

25 kts

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10
Q

Max taxi speed when making sharp turns

A

10 kts

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11
Q

monitor GS on

A

list 6 / INS page

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12
Q

after Landing do not use ______

A

parking brake

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13
Q

MIL power Takeoff: check nozzle ____ or less within ____ and oil pressure at least ____ psi above idle value

A

30%, 5 seconds, 15

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14
Q

disengage NWS when rudder become effective at _____

A

70 kts

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15
Q

takeoff: rotate to a ______ attitude at takeoff speed

A

8-12 degree

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16
Q

gear speed limit

A

300 kts / M0.65

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17
Q

AB Takeoff: cancel AB at ______ or ______ whichever comes LAST

A

end of runway, 300 kts

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18
Q

local climb schedule is _____ KCAS until ______ mach

A

350, 0.85

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19
Q

Tucson minimum fuel:

A

1000 lbs

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20
Q

Tucson emergency fuel:

A

800 lbs

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21
Q

initial at Tucson int. is flown at ______ msl and ____ kts

A

4000, 300

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22
Q

overhead break: _____ bank and ____ g pull

A

70 degrees, 3 g pull

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23
Q

overhead: roll out on downwind with _____ kcas with the wingtip missile rail on _____

A

200-220, the rwy

24
Q

Max AOA on downwind is

A

13 AOA

25
Q

exceeding _____ AOA should not be a common part of the final turn

A

13 AOA

26
Q

With gear down, the low speed warning horn comes on at ______

A

15 AOA

27
Q

Roll out on final approx at ____ AGL and ____ mile with _____ glidepath

A

300’, 1 mile, 2.5-3.0 degree

28
Q

hard touchdown between _____ can damage the aircraft

A

13-15 AOA

29
Q

final approach is normally flown at _____

A

11 AOA

30
Q

g limit for gear in transition

A

2.0 G

31
Q

high key altitude

A

7.000-10.000’ AGL

32
Q

low key altitude

A

3.000-5.000’ AGL

33
Q

base key altitude

A

2.000’ AGL MINIMUM

34
Q

SFO speeds

A

200 kts clean
190 kts LG DN
180 MINIMUM

add 5 kts per 1000 lbs > 1000 lbs (C) and 0 lbs (D)

35
Q

SFO optimum bank angles

A

50 gear up

55 gear down

36
Q

on SFO’s execute low approach at _____

A

20-50’ AGL

37
Q

HUD groundspeed also changes the HUD __________

A

magnetic heading to magnetic groundtrack

38
Q

unusual attitudes: use _____ KCAS as a guide determine off idle or MIL power

A

350

39
Q

________ is the primary instrument navaid

A

TACAN

40
Q

Max holding speed above 14.000 MSL
from 14.000 to 6.000 MSL
AND 6.000 MSL and below

A

265 KCAS
230 KCAS
200 KCAS

41
Q

use ____ % of your groundspeed to determine _____

A

1%, turn radius

42
Q

fly a penetration at _____ and ______ rpm min

A

300 KCAS, 70 %

43
Q

instrument patterns is normally flown at _____ kcas

A

250

44
Q

F-16 is category _____

A

E

45
Q

min taxi interval _____ staggered and _____ in trial

A

150’, 300’

46
Q

standard formation is

A

1 NM max separation and no further than 100’ alt difference

47
Q

min take-off spacing in MIL and AB

A

10 secs, 15 secs

48
Q

Line up with ____ wingtip clearance

A

10’

49
Q

All wingmen will notify flightlead when

A

tanks dry, joker, bingo

50
Q

fingertip reference

A

front portion of missile rail aligned with a point halfway between ECS duct and intake
AIM-9: forward fins
AIM-120: warhead section

51
Q

route formation:

A

same as fingertip, 2-shipwidths (66’) - 500’

52
Q

a standard rejoin is flown to _______ formation

A

route

53
Q

Safety chase parameters

A

30-60 degree cone
300’-1000’
match other aircrafts confiq

54
Q

Line abreast parameters

A

0-30 degrees aft
4.000’ - 18.000’
(6000-9000’ desired)

stack +/- 2000’

55
Q

fighting wing parameters

A

30-70 degrees aft
500’-3000’ spacing

extended fighting wing: 3000-6000’

56
Q

wedge parameters

A

30-70 degrees aft
6.000’ - 18.000’ spacing
(6000-9000’ desired)

57
Q

Max distance from flight lead in visual formation

A

3 NM

F-16 BL 42 (4 decks)

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