Transition Phase Flashcards
always adjust the ______ prior to battery power to prevent inadvertently bleeding the ________
rudder pedals, JFS accumulators
always complete the VERIFY checklist prior to _________
applying battery power
after applying battery power, wait _____ to start the JFS to complete the ______ check
30 seconds, HYD/OIL warning light
hot wx ops: start with canopy _____ open, until idle
6 inches
motor engine with the JFS for _______
1 minute
EPU check: the EPU must run on AIR for _____ to be valid
5 seconds
the guard ramp is ________
uncontrolled
taxi speed ramp / congested area should not exceed _____
10 kts
Max taxi speed uncontested areas
25 kts
Max taxi speed when making sharp turns
10 kts
monitor GS on
list 6 / INS page
after Landing do not use ______
parking brake
MIL power Takeoff: check nozzle ____ or less within ____ and oil pressure at least ____ psi above idle value
30%, 5 seconds, 15
disengage NWS when rudder become effective at _____
70 kts
takeoff: rotate to a ______ attitude at takeoff speed
8-12 degree
gear speed limit
300 kts / M0.65
AB Takeoff: cancel AB at ______ or ______ whichever comes LAST
end of runway, 300 kts
local climb schedule is _____ KCAS until ______ mach
350, 0.85
Tucson minimum fuel:
1000 lbs
Tucson emergency fuel:
800 lbs
initial at Tucson int. is flown at ______ msl and ____ kts
4000, 300
overhead break: _____ bank and ____ g pull
70 degrees, 3 g pull
overhead: roll out on downwind with _____ kcas with the wingtip missile rail on _____
200-220, the rwy
Max AOA on downwind is
13 AOA
exceeding _____ AOA should not be a common part of the final turn
13 AOA
With gear down, the low speed warning horn comes on at ______
15 AOA
Roll out on final approx at ____ AGL and ____ mile with _____ glidepath
300’, 1 mile, 2.5-3.0 degree
hard touchdown between _____ can damage the aircraft
13-15 AOA
final approach is normally flown at _____
11 AOA
g limit for gear in transition
2.0 G
high key altitude
7.000-10.000’ AGL
low key altitude
3.000-5.000’ AGL
base key altitude
2.000’ AGL MINIMUM
SFO speeds
200 kts clean
190 kts LG DN
180 MINIMUM
add 5 kts per 1000 lbs > 1000 lbs (C) and 0 lbs (D)
SFO optimum bank angles
50 gear up
55 gear down
on SFO’s execute low approach at _____
20-50’ AGL
HUD groundspeed also changes the HUD __________
magnetic heading to magnetic groundtrack
unusual attitudes: use _____ KCAS as a guide determine off idle or MIL power
350
________ is the primary instrument navaid
TACAN
Max holding speed above 14.000 MSL
from 14.000 to 6.000 MSL
AND 6.000 MSL and below
265 KCAS
230 KCAS
200 KCAS
use ____ % of your groundspeed to determine _____
1%, turn radius
fly a penetration at _____ and ______ rpm min
300 KCAS, 70 %
instrument patterns is normally flown at _____ kcas
250
F-16 is category _____
E
min taxi interval _____ staggered and _____ in trial
150’, 300’
standard formation is
1 NM max separation and no further than 100’ alt difference
min take-off spacing in MIL and AB
10 secs, 15 secs
Line up with ____ wingtip clearance
10’
All wingmen will notify flightlead when
tanks dry, joker, bingo
fingertip reference
front portion of missile rail aligned with a point halfway between ECS duct and intake
AIM-9: forward fins
AIM-120: warhead section
route formation:
same as fingertip, 2-shipwidths (66’) - 500’
a standard rejoin is flown to _______ formation
route
Safety chase parameters
30-60 degree cone
300’-1000’
match other aircrafts confiq
Line abreast parameters
0-30 degrees aft
4.000’ - 18.000’
(6000-9000’ desired)
stack +/- 2000’
fighting wing parameters
30-70 degrees aft
500’-3000’ spacing
extended fighting wing: 3000-6000’
wedge parameters
30-70 degrees aft
6.000’ - 18.000’ spacing
(6000-9000’ desired)
Max distance from flight lead in visual formation
3 NM
