Limitations and Prohibited Maneuvers

Question 0

Engine Core Vibration

Answer 0

2.2 ips max

Question 1

Engine Fan Vibration

Answer 1

1.6 ips max

Question 2

CG Limitations

Answer 2

16.8 to 31.8% MAC

Question 3

Transient (MIL/MAX) N2% Limitations

Answer 3

102%

Question 4

Transient (MIL/MAX) N1% Limitation

Answer 4

103%

Question 5

Transient (MIL/MAX) EGT Limitation

Answer 5

967 C

Question 6

Steady State N2% Limitation
MAX
MIL

Answer 6

100%

Question 7

Steady State N1% Limitation
MAX
MIL

Answer 7

100%

Question 8

Steady State EGT Limitation
MAX
MIL

Answer 8

952 C

932 C

Question 9

Steady State Nozzle % Limitation
MAX
MIL

Answer 9

50-100%

0-45%

Question 10

Steady State Oil Press (psi) Limitation
MAX
MIL

Answer 10

80 to 150 psi (warm oil)

Question 11

Ground Idle N2% Limitation

Answer 11

Greater than or equal to 61%

Question 12

Ground Idle N1 % Limitation

Answer 12

Greater than or equal to 32%

Question 13

Ground Idle EGT Limitation

Answer 13

250 to 590 C

Question 14

Ground Idle Nozzle % Limitation

Answer 14

77 to 83%

Question 15

Ground Idle Oil Press (psi) Limitation

Answer 15

35 to 90 psi (warm oil)

Question 16

Start N2% Limitation

Answer 16

Greater than or equal to 10%

Question 17

Start EGT Limitation

Answer 17

871 C

Question 18

Start Oil Press (psi) Limitation

Answer 18

Min 10 within 30 sec

180 max after 2.5 min

Question 19

Refueling Probe Limitations

Answer 19

Extension/Retraction
-300 KCAS
Extended
-400 KCAS

Question 20

Landing Gear Limitations

Answer 20

Extension/Restraction/Extended
-250 KCAS
Emergency Extension
-170 KCAS

Question 21

Trailing Edge Flaps Limitation

Answer 21

HALF/FULL

-250 KCAS

Question 22

Tires Limitations

Answer 22

Nose Gear
-195 KGS
Main Gear
-210 KGS

Question 23

Wingfold Limitation

Answer 23

Spread/Fold

-60 Kts

Question 24

Canopy Limitation

Answer 24

Open | -60 Kts

Question 25

Field Takeoff/In Flight Weight Limitation

Answer 25

66,000 lbs | 68,000 lbs (5 wet tanker only)

Question 26

Field Takeoff/In Flight Asymmetry Weight Limitation

Answer 26

29,000 lbs (FLY)

Question 27

Field Landing/FCLP/T&G Weight Limitation

Answer 27

50,600 lbs

Question 28

Field Landing/FCLP/T&G Asymmetry Limitation

Answer 28

33,000 lbs (LAND)

Question 29

Catapult Weight Limitation

Answer 29

66,000 lbs | 66,800 lbs (5 wet tanker only)

Question 30

Catapult Asymmetry Limitation

Answer 30

29,000 lbs (FLY) | 30,800 lbs (LAND)

Question 31

Carrier Landing/T&G/Barricade Weight Limitation

Answer 31

44,000 lbs

Question 32

Carrier Landing/T&G/Barricade Asymmetry Limitation

Answer 32

30,800 lbs (LAND)

Question 33

Flaps HALF or FULL Acceleration Limitations

Answer 33

Symmetrical - 0.0 to +2.0 G Rolling - +0.5 to +1.5 G

Question 34

AOA Limitation with Flaps HALF or FULL

Answer 34

0 to 14 (AOA tone)

Question 35

Fuel and Engine Oil Prohibited Maneuvers

Answer 35

- Zero G except transient (over 2 seconds between +0.2 and -0.2 G) - Negative G for more than 10 seconds (30 second required between negative G maneuvers)

Question 36

Flying Qualities Prohibited Maneuvers

Answer 36

1) Single-ship takeoff with 90 deg crosswind component over 30 kts 2) Section takeoffs with any of the following conditions: - 90 deg crosswind component over 15 kts - Asymmetric loading over 9,000 ft-lb not including wingtip missiles or pods - Dissimilar loading except pylons, FLIR, LDT, fuselage missiles, wingtip missiles or pods, CVERS, MERS, or TERS 3) Flight with GAIN ORIDE selected above 10 deg AOA or above 350 KCAS (flaps AUTO), 200 KCAS (flaps HALF), or 190 KCAS (flaps FULL) 4) Single-ship landings with 90 deg crosswind component over 30 kts 5) Section landing with 90 deg crosswind component over 15 kts 6) Aerobraking on landing rollout with crosswind greater than 5 kts, pitch attitude greater than 10 deg, airspeed less than 80 KCAS, GAIN ORIDE selected, FCS AIR DAT caution or FLAP SCHED caution