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Transient (MIL/MAX) N2
102%
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Transient (MIL/MAX) N1
103%
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Transient (MIL/MAX) EGT
976
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Steady state MIL Nozzle
0 - 45
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Steady state MIL Oil Press
80- 150
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-
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Steady state MAX Nozzle
50 - 100
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Steady state MAX Oil Press
80 - 150
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Ground IDLE EGT
250 - 590
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Ground IDLE Nozzle
77 - 83
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Ground IDLE Oil Press
35 - 90
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Start Oil Press
- *min 10 in 30 seconds
- *180 max after 2.5 min
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-
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Speed Tires Nosewheel
195
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-
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-
-
-
-
-
-
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G limit during Gear Ext/Ret
0.0 - 2.0 symmetrical
0.5 - 1.5 rolling
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AOA less than 6K Asymmetry Subsonic
unrestricted
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AOA less than 6K Asymmetry Supersonic
Unrestricted
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AOA 6-8K Asymmetry Subsonic
Unrestricted
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AOA 6-8K Asymmetry Supersonic
-6 to +15 deg
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AOA 8-13K Asymmetry Low or Slow
Unrestricted
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AOA 8-13K Asymmetry High and Fast
<= +30 deg
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AOA 8-13K Asymmetry Supersonic
-6 to +15 deg
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AOA 13-26K Asymmetry Subsonic
- -6 to +15 deg
- single axis input only
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AOA 13-26K Asymmetry Supersonic
- -6 to +15 deg
- single axis inputs only
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Prohibited Maneuvers Systems
1. T/O with an FCS A or FCS B DEGD
2. Pulling and FCS circuit breaker in flight except as directed by NATOPS
3. Use of RALT hold below 500ft AGL
- 4. Landing with autopilot engaged except for the following
- a. Mode 1 ACL
- b. Field landings with FPAH/ROLL
5. Takeoffs and landings while using any LEP device
6. Selection of MAN with the ECS MODE switch
7. Selection of AEA PRECOOL mode
- 8. Flight in RVSM with any of the following
- a. Mach >0.9
- b. AOA >15
- c. Load factor >1.5g
- d. Initial engagement of BALT when above Mach 0.9
- e. BALT not engaged when level at assigned altitude
- f. Refueling probe extended
- g. GAIN ORIDE selected
- h. Suspected AOA or pitot-static probe damage
- i. Baro altitude displayed with an "X"
9. In-flight Memory Inspect of FCC addresses greater than 6 digits long
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G Limits Symmetrical maneuvers
*+7.5 to -3.0g at a weight of 42,097lb
*above 57,405lb G-limiter is fixed at +5.5g
*overshoots of up to +0.5 or -0.2g do not consititute an over-g
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G Limits Rolling maneuvers
*+6.0 to -1.0g at a weight of 42,097lb
*above 57,405lb G-limiter is fixed at +4.4g
*overshoots of up to +0.5 or -0.2g do not consititute an over-g
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Limits with flaps HALF or FULL AOA
0 - 14 (AOA Tone)
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Limits with flaps HALF or FULL Bank Angle
*90 deg Max
*15 deg Max during flap selection with a HI AOA advisory
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Limits with flaps HALF or FULL Symmetrical Acceleration
0.0 - 2.0g
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Limits with flaps HALF or FULL Rolling Acceleration
0.5 - 1.5g
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Prohibited Maneuvers Departure/Spin
1. 0 airspeed tailslide
2. Intentional departures/spins
3. Yaw rates over 40 deg/second (yaw tone)
4. Holding roll inputs past 360 deg bank angle change
5. Inflight selection of RCVY on the SPIN switch
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Prohibited Maneuvers Fuel and Engine Oil
1. 0 g except transient (over 2 seconds between +0.2 and -0.2g)
2. Negative g for more than 10 seconds (30 seconds required between negative g maneuvers)
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Prohibited Maneuvers Loads
1. Field full stop, FCLP, or T&G with lens settings greater than 3.25 deg
2. Carrier arrestment or T&G with lens setting of greater than 4.0 deg
3. Flight above 650 KCAS and below 18,000 feet MSL
4. Holding lateral stick inputs past 180 deg of bank angle change when pushing between 0.0 and -1.0g
5. Abrupt, full aft stick inputs (full aft stick in less than 0.5 seconds) with less than 3,500 lb of fuel
6. Any rudder input when the aircraft load factor is more negative than -1.2g
7. Use of rudder trim above 400 KCAS to intentionally induce unbalanced flight
- 8. Lateral and directional trim inputs. Use of lateral and/or directional trim in combination with lateral stick inputs above certain airspeeds may result in the exceedance of aircraft structural load limits due to a/c imbalance.
- a. Roll off tendency >5 deg/sec without lateral trim
- - Pushing beyond -1.2g when a/s above 500 KCAS
- - More than half lateral stick deflection when airspeed >600 KCAS or Mach >1.1 below 24,000 ft MSL, or a/s >500 KCAS above 24,000 ft MSL
- b. Lateral weight asymmetry for air-to-ground store >6,000 ft*lb and <= 26,000 ft*lb
- - Pushing beyond -1.2g when a/s is above 500 KCAS
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Prohibited Maneuvers Flying Qualities
1. Single-ship takeoffs with 90 deg crosswind component over 30 knots
- 2. Section takeoffs with any of the following
- a. 90 deg crosswind over 15 knots
- b. Asymmetric loading over 9,000 ft*lb
- c. Dissimilar loading except pylons and fuselage missiles
3. Flight with GAIN ORIDE selected above 10 deg AOA or above 350 KCAS (flaps AUTO), above 200 KCAS (flaps HALF), or above 190 KCAS (flaps FULL)
4. Single-ship landings with 90 deg crosswind above 30 knots
5. Section landing with 90 deg crosswind above 15 knots
6. Aerobraking with crosswind greater than 5 knots, pitch attitude greater than 10 deg, airspeed less than 80 KCAS, GAIN ORIDE selected, FCS AIR DAT caution or FLAP SCHED caution
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Prohibited Maneuvers Flutter
ALQ-218 pod shall include all of the internal and external components defined below
1. Structural assembly with shock-mounted equipment trays installed, and including 4 upper surface fins
2. WRA-1,2,3,4/AU-1,2,3,4 (antenna preselector unit and SBI array) in the forward and aft equipment tray
3. AU-10/11 (left/right mid-band SBI array) in the center position of the outboard-facing ground plane
4. AU-17/19 (left/right forward low band antenna) in the forward position of the outboard-facing ground plane
5. AU-18/20 (left/right aft low band antenna) in the aft position of the outboard-facing ground plane
6. Forward and aft RF-compatible radomes
7. Side RF-compatible radome
8. Pod air inlet scoop
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AESA Radar must cease operation when within ____ nm of ____ during ____
10 nm of PAR and ACLS facilities during IMC/Case III conditions
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