Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

F-16C BL42 PW220 > F-16 by the numbers > Flashcards

F-16 by the numbers Flashcards

1
Q

Length

A

49’ 5.2”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Width

A

32’ 10”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Amount of PW220 stages

A

13 stages (3 fans and 10 rear compressors)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

F-16C GW (w. Fuel)

A

19,700 lbs (26,900 lbs)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

PW220 MAX thrust

A

25,000 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

PW220 MIL thrust

A

14,000 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Amount of LOD restart attempts

A

3

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

MLG speed limit

A

225 GS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

NLG speed limit

A

217 GS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Cable Arrest limit

A

150 kts (routine) or 160 kts (emergency)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Engage HOOK ___ ft prior to arrest cable

A

1500 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Canopy Open/Transit limit

A

70 kts (incl. wind velocity)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

LG Extended/Transit (airspeed)

A

300/0.65, whichever is less

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

LG Retraction/Extension (G symmetric and asymmetric)

A

2.0/0.0 and 2.0/0.0

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

LG Extended (G symmetric and asymmetric)

A

4.0/0.0 and 2.0/0.0

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

ENGINE Warning light illuminates when

A

2 sec after FTIT exceeds 1000 degrees or below 55 %

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

OVERHEAT LOOP activates

A

100 degrees celcius below FIRE LOOP

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

If zoom results in altitude below ___ AGL = ejection

A

5000’ AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

If zoom results in altitude between ___ - ___ AGL = 1 airstart

A

5000-10,000’ AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Final Approach Airspeed @ 11 AOA C/D model

A

142/144 (C/D) + 4 kts per every 1000 lbs fuel and stores

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

FLCS BIT takes approximately

A

45 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Speedbrake normal

A

60 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Speedbrake w. GR/DN

A

43 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Continuous toe braking will deplete JFS/brake accumulator within

A

Approximately 75 sec (fully charged)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Height canopy can reach during jettison

A

26 ft (C) or 17 ft (D)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Low altitude for engine malfunction is considered

A

<10,000’ AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

With engine malfunction below 350 kts

A

Initiate 3 G pull and 30 degree pitch

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

AB-related fire should extinguish after

A

30-45 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

If autotransfer to SEC occurs below ___ MSL, set a minimum of ___ RPM

A

15,000’ MSL, 70 % RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

Engine flameout in MIL with use of FUEL MASTER takes

A

6 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Engine flameout in IDLE with use of FUEL MASTER takes

A

45 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

With missing nozzles, level flight above ___ MSL in PRI is not possible

A

8000’ MSL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

With missing nozzles, level flight above ___ MSL in SEC is not possible

A

5000’ MSL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

If unable to maintain ___ above MSEA (Minimum Safe Ejection Altitude) in PRI, select SEC

A

1000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

(TO 1F-16CM-1) During nozzle loss/failure/malfunction SEC operation above ___ degrees is likely to cause engine fire/failure in little as ___.

A

850 degrees, 5 min.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

An AB (no light) initial attempt and 3 subsequent attempts takes

A

Approximately 20 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

Expect ___ the computed ground roll on a flameout landing

A

Twice (8000’ recommended)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

Max Endurance Airspeed

A

170 KCAS + 5 kts per every 1000 lbs fuel/stores over 1000 (C) or 0 (D) lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

Max Range Airspeed

A

200 KCAS + 5 kts per every 1000 lbs fuel/stores over 1000 (C) or 0 (D) lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

Spooldown airstart RPM (OFF to IDLE)

A

50-25 RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

Recommended spooldown airspeed PRI/SEC

A

Minimum 250 kts / 275 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
42
Q

Airspeed for JFS-assisted airstart PRI/SEC

A

Max Range or maximum endurance airspeed (200 knots minimum for SEC)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
43
Q

Minimum airspeed for SEC airstart (JFS ON)

A

200 KCAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
44
Q

JFS will motor engine at minimum

A

22 % RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
45
Q

MFP does not supply sufficient fuel flow below ___ RPM for airstart

A

12 % RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
46
Q

___ kts or more is required to stay above ___ % RPM

A

350 kts, 12 % RPM

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
47
Q

___ - ___ kts for ___ - ___ sec may regain ___ % RPM

A

400-450 kts, 20-25 sec, 12 %

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
48
Q

When below ___’ MSL and ___ kts, activate the JFS during airstart

A

20,000’ MSL / 400 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
49
Q

If FTIT is above ___ degrees celcius, expect HOT start

A

700 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
50
Q

Maximum range AOA

A

0.7 AOA

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
51
Q

Maximum range airspeed based on which GW

A

20,000 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
52
Q

In case of dual AOA malfunction, FLCC selects

A

11 AOA

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
53
Q

STBY Gains LG UP

A

600 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
54
Q

STBY Gains LG DN

A

230 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
55
Q

LEF in STBY Gains w. LG UP + ALT FLAPS NORM

A

0 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
56
Q

LEF in STBY Gains w. LG DN + ALT FLAPS EXTEND

A

15 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
57
Q

During STBY Gains maintain below ___ kts

A

650 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
58
Q

During STBY Gains maintain ___ kts until LG DN

A

240 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
59
Q

LEF’s should remain symmetrical within ___ degrees

A

10 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
60
Q

PROBE HEAT should flash ___ - ___ times per sec

A

3-5 times

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
61
Q

During ALT GEAR Extension maintain

A

Lowest practical airspeed below 190 kts. NLG may not indicate down until airspeed is reduced below 190 knots. Time above 190 knots should be minimized in case there is a leak in the pneumatic lines.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
62
Q

SFO aimpoint

A

1/3 down RWY

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
63
Q

High Key altitude

A

7-10,000’ AGL. The recommended high key altitude is (C) 7000, (D) 7500 feet AGL plus 500’ per every 1000 lbs of fuel/stores weights.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
64
Q

Low Key altitude

A

3-5000’ AGL. The recommended low key altitude is (C) 3000, (D) 3250 feet AGL plus 250’ per every 1000 lbs of fuel/stores weights.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
65
Q

Base Key altitude

A

Minimum 2000’ AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
66
Q

Optimum LG DN airspeed

A

10 kts less than Max Range

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
67
Q

Minimun LG DN airspeed

A

20 kts less than Max Range

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
68
Q

Optimum angle of bank (LG UP/DN)

A

50/55 degrees

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
69
Q

EPU quantity below ___ @ High Key (___ w. JFS) is not recommended

A

25 % / 20 %

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
70
Q

Initial aimpoint ___ below horizon before LG DN on Straight-In

A

11-17 degrees on pitch ladder

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
71
Q

EPU fuel required for non-standard approach is approximately

A

15 % per min.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
72
Q

Main AC GEN

A

60 kva

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
73
Q

STBY AC GEN

A

10 kva

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
74
Q

Emergency AC GEN

A

5 kva

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
75
Q

Max time for Main PWR in BATT or MAIN PWR

A

Only 5 min

76
Q

Max time for EXT PWR attached

A

30 min

77
Q

ACFT BATT TO FLCS illuminated during total GEN failure

A

BATT supplies FLCS operations for 3-14 min

78
Q

FLCS PMG + EPU PMG + ACFT BATT TO FLCS + battery buses

A

BATT supplies FLCS operations for 3-14 min

79
Q

ACFT BATT FAIL light

A

20V or less

80
Q

FLCS RLY light ON

A

Voltage on one or more of the four FLCC branches is below 20V, or one or more FLCC branches are not connected to the aircraft battery.

81
Q

BATT voltage required for HOOK DN and operational

A

Approximately 5VDC

82
Q

ELEC SYS and ACFT BATT FAIL

A

BATT failure

83
Q

MAIN GEN light illuminates below

A

45 % RPM

84
Q

Tower Shaft Failures is indicated by

A

0 % RPM, 0 psi OIL, ENGINE light, SEC light and engine flameout due to fuel starvation

85
Q

Hydraulic system pressure

A

3000 psi

86
Q

HYD Light ON

A

Pressure below 1000 psi

87
Q

HYD Light OFF

A

Pressure above 1000 psi

88
Q

Pulling ALT GEAR with normal System B pressure may fail System ___ within ___ min

A

System B within 15 min

89
Q

System A supplies pressure to

A

SB, FFP, LEF and FLCS

90
Q

System B supplies pressure to

A

LEF, FLCS, NWS, normal braking, JFS, AR door operation, gun operation and normal LG extension

91
Q

During DUAL HYDR MALF, EPU automatically provides pressure to

A

System A

92
Q

Amount of fuel tanks

A

7 (Internal wing L/R, FWD/AFT reservoir, F1, F2, A1)

93
Q

Fuel QTY L/R Internal Wing

A

550 lbs +/- 100

94
Q

Fuel QTY F1, F2 and FWD RES

A

3250 lbs +/- 100

95
Q

Fuel QTY A1 and AFT RES

A

2810 lbs +/- 100

96
Q

Fuel QTY FWD and AFT RES

A

480 lbs +/- 30

97
Q

Fuel QTY L/R External Wing (370 gal)

A

2420 lbs +/- 100

98
Q

Fuel QTY Centerline

A

1890 lbs +/- 100

99
Q

Total Fuel QTY Internal

A

7160 lbs +/- 300

100
Q

Total Fuel QTY External (370 gal)

A

6730 lbs +/- 300

101
Q

C FWD/AFT FUEL LOW light

A

400/250 lbs in reservoir

102
Q

D FWD/AFT FUEL LOW light

A

250/400 lbs in reservoir

103
Q

If fuel imbalance between external wing exceeds ___ lbs refer to ASYMMETRIC STORES (LANDING)

A

1700 lbs

104
Q

Normal Recovery fuel

A

1200 lbs

105
Q

Minimum fuel

A

1000 lbs

106
Q

Emergency fuel

A

800 lbs

107
Q

Total amount of oil

A

28 pints (14 quarts)

108
Q

(OIL) HYD/OIL PRESS light illuminates when ___. The light goes out when oil pressure exceeds approximately ___ psi.

A

Pressure below 10 psi +/- 2 for >30 sec / 20 psi

109
Q

CABIN PRESS illuminates

A

Cockpit pressure >27,000’

110
Q

Backup Oxygen System (BOS) supplies oxygen for C / D (both) / D (solo)

A

3-5 min / 2-3.5 min / 4-7 min

111
Q

Emergency Oxygen System (EOS) supplies oxygen for

A

8-12 min

112
Q

EPU operation time on hydrazine only

A

10 min

113
Q

Closed pattern airspeed

A

250-300 KCAS

114
Q

Closed Downwind airspeed (rollout)

A

200-250 KCAS

115
Q

Taxi spacing on centerline

A

300 ft

116
Q

Taxi spacing if staggered

A

150 ft

117
Q

Disengage NWS at ___ KCAS

A

70 KCAS

118
Q

Rotation speed @ MIL power

A

10 kts below takeoff speed

119
Q

Rotation speed @ MAX power

A

15 kts below takeoff speed

120
Q

Pitch attitude after T/O

A

8-12 degrees

121
Q

Aborting at or above 100 KCAS

A

Lower hook

122
Q

Aborting at or above 120 KCAS

A

Suspect hot brakes

123
Q

Airspeed at which T/O should be continued with tire failure

A

100 KCAS

124
Q

GX airspeed

A

400 KCAS

125
Q

G-warmup

A

4-5 G’s and 90 degrees of turn. Starting LAB and ending in trail

126
Q

G-awareness

A

5-7 G’s and 90 degrees of turn for A2G or 180 degrees of turn for A2A.

127
Q

Alternate braking reduces braking

A

25-30 %

128
Q

Differential braking greater than ___ % will degrade braking to pulsating mode

A

15 %

129
Q

Pulsating braking is ___ % as effective as antiskid braking

A

50 %

130
Q

Restrict engine operation without corrosion inhibitor to ___ consecutive hours.

A

10 hours

131
Q

If brake energy absorption is in the danger zone, wheel fusible plugs release tire pressure within ___ - ___ minutes after stop

A

3-15 minutes

132
Q

The maximum allowable fuel flow with one reservoir empty is ___ pph.

A

25,000 pph

133
Q

Negative G flight with both reservoir tanks full is limited to:

AB thrust:
MIL thrust or below:

A

AB thrust: 10 sec

MIL thrust or below: 30 sec

134
Q

Maximum operating airspeed is ___ knots from sea level to 30,000’ MSL.

A

800 knots

135
Q

Above 30,000’ MSL, the maximum airspeed is ___ mach.

A

2.05 mach

136
Q

Do not operate with CAT III loadings below ___ knots unless in takeoff or landing gains.

A

200 knots

137
Q

The maximum allowable GW for ground handling, taxi, takeoff, in-flight and landing is ___ lbs

A

42,300 lbs

138
Q

Full aft stick maneuvers started above ___ KCAS are more susceptible to over-g.

A

500 KCAS

139
Q

Transfer to SEC when subsonic below 40,000’ MSL should be performed with the THR at ____ or above

A

Midrange

140
Q

(JFS) Continuous motoring of the engine shall not exceed ___ minutes. After ___ minutes of continuous motoring, a normal engine start may be initiated after ___ minutes of cooling.

A

4 minutes, 4 minutes, 5 minutes

141
Q

(JFS) A minimum wait of ___ minute is required after each JFS start attempt to allow fuel drainage from the JFS.

A

1 minute

142
Q

(JFS) Motor until FTIT is below ___ degrees celcius during hot start of engine.

A

200 degrees celcius.

143
Q

(JFS) Motoring is defined as JFS rotating the engine with the THR in OFF @ ___ RPM.

A

22 % RPM

144
Q

AR Door Opening/Closing

A

400/0.85, whichever is less

145
Q

AR Door Open

A

400/0.95, whichever is less

146
Q

Flight in Severe Turbulence (+/- 3 g)

A

500

147
Q

Max Bank Angle change for Max Roll Maneuver (CAT I + III)

A

360 degrees

148
Q

To prevent possible aft structure and tail overloads, rudder travel has been limited. When not in takeoff and landing gains, rudder travel is reduced ___ % at ___ knots, and the reduction increases linearly to ___ % at ___ knots.

A

50 % at 300 knots, 70 % at 500 knots

149
Q

(C) The most aft CG occurs with approximately ___ lbs of internal fuel remaining.

A

2000 lbs

150
Q

(D) With external fuel tanks, the most aft CG occurs when the external fuel tanks have just emptied/started giving fuel?

A

Emptied

151
Q

During Nose Low Recovery, if airspeed is below ___ knots, altitude loss is minimized by selecting/maintaining MIL/AB.

A

350 knots

152
Q

If airspeed is ___ knots or above, selecting/maintaining IDLE thrust and opening Speedbrake minimize altitude loss.

A

350 knots

153
Q

Airspeed should be maintained below ___ knots/___ mach while in DBU

A

500 knots/0.9 mach

154
Q

Do not exceed ___ degrees AOA with the LEF’s inoperative.

A

12 degrees

155
Q

One complete pitch rocking cycle takes approximately ___ sec, during which time the aircraft descends ___-___ ft.

A

6 sec and 1000-1500’

156
Q

AOA indicator displays a maximum of ___ degrees and a minimun of ___ degrees.

A

+ 32 degrees and -5 degrees

157
Q

If AOA exceeds ___ degrees, the yaw rate limiter provides antispin commands to the rudder, flaperons, and horizontal tails. Pilot roll abd rudder commands are inhibited and pitch stick commands are ineffective without use of MPO switch.

A

35 degrees

158
Q

If AOA is below ___ degrees and airspeed is less than ___ knots, the yaw rate limiter provides antispin commands to the rudder.

A

-5 degrees and 170 knots

159
Q

Recommended holding airspeed is ___.

A

Maximum endurance

160
Q

Penetrations are normally flown at ___ knots, speedbrake as required, and throttle at ___RPM minimum.

A

300 knots and 70 % RPM

161
Q

A typical straight-in penetration and approach require approximately ___ lbs of fuel (drag index 0) and ___ lbs of fuel (drag index 200)

A

400 lbs and 600 lbs

162
Q

(GCA) Entry/Downwind airspeed is ___-___ knots

A

200-250

163
Q

A typical GCA pattern requires approximately ___ lbs (drag index 0) and ___ lbs (drag index 200).

A

400 lbs and 700 lbs

164
Q

TS penetration speed is ___ knots or optimum cruise airspeed, whichever is lower.

A

300 knots

165
Q

Icing is possible under the following conditions:

Ambient temperature between ___ degrees F (-7 degrees C) and ___ degrees F (7 degrees C) with precipitation (rain, fog, sleet or snow)

A

20 degrees F and 45 degrees F

166
Q

If probe icing is evident or suspected, turn the PROBE HEAT switch to PROBE HEAT at least ___ min prior to accomplishing the FLCS BIT.

A

2 minutes

167
Q

Turn probe heat on at least ___ min prior to takeoff anytime icing of probes is possible.

A

2 minutes

168
Q

The local climb schedule is ___ KCAS until ___ Mach

A

350 KCAS / 0.85 Mach

169
Q

___ KCAS is the optimum idle descent during a divert

A

205 KCAS

170
Q

The warning light [in LG handle] also illuminates when all LG are not ___ and ___, airspeed is less than ___ kts, altitude is less than ___ ft, and a rate of descent is greater than ___ fpm.

A

Down and locked / 190 kts / 10,000 ft / 250 fpm

171
Q

OXY LOW warning light illuminates when oxygen pressure is below ___ psi or quantity is below ___ liter.

A

42 psi / 0.5 liter

172
Q

A JFS RUN light flashing ___ per second indicates a ___ failure in the JFS system. If the JFS operates normally for engine start, the mission may be continued. Notify maintenance after flight.

A

Once / noncritical

173
Q

A JFS RUN light flashing ___ per second indicates a ___ failure in the JFS system. The JFS will not operate. Place the MAIN PWR switch to OFF and notify maintenance.

A

Twice / critical

174
Q

The oil must be checked by maintenance within ___ min after engine shutdown to be a valid reading.

A

30 min

175
Q

With the LG handle down, the TEFs are ___ down until ___ kts. Above ___ kts, the TEFs reduce deflection based on airspeed until they are fully retracted at ___ kts.

A

20 degrees / 240 kts / 240 kts / 370 kts

176
Q

(SEC) Approximately ___ sec response time from IDLE to MIL.

A

5 sec

177
Q

(SEC) Idle thrust in SEC = ___ idle thrust in PRI

A

Twice

178
Q

After takeoff, ARI is activated within ___ sec after the LG handle is raised.

A

2 sec

179
Q

The low speed warning horn also sounds when AOA is greater than ___ degrees with the LG handle down or the ALT FLAPS switch in EXTEND.

A

15 degrees

180
Q

F-16D GW (w. Fuel)

A

20,400 lbs (26,300 lbs)

181
Q

The fire detection loops are routed through the ___ compartment.

A

Engine

182
Q

The overheat detection loops are routed through the ___ compartment, ___, ___ , and ___.

A

Engine compartment. MLG wheel wells, ECS bay and EPU bay. (Acronym: WEEE)

183
Q

Things required to recharge brake/JFS accumulators

A

12 % rpm and System B hydraulics for 40-60 sec (hot/cold)

184
Q

Flameout Str-in altitudes:

Clean glide - ___ ft AGL min at ___ NM.

Lower gear - ___ ft AGL at ___ NM.

A

7000’ AGL min at 8 NM

4000-8000’ AGL at 4 NM

185
Q

Min EPU fuel quantity without (with) JFS running:

Overhead approach at high key - ___ (___) %.

Straight-in approach:
8 NM - ___(___) %.
4 NM - ___(___) %.

A

25 (20) %

45 (40) %

25 (20) %

186
Q

PTO shaft failure is indicated by:

A

Hydraulic system B failure, MAIN GEN and STBY GEN lights, EPU run light and FLCS PMG light.

187
Q

While subsonic in SEC, throttle movement is unrestricted between ___-___ feet MSL and AB operation is inhibited.

A

15,000-40,000’ MSL

F-16C BL42 PW220 (15 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions