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AOA 0 to 14° (AOA tone) (1)
Bank angle 90° max
15° max during flap selection (HALF or FULL from
AUTO) with a HI AOA advisory
Acceleration Symmetrical 0.0 to +2.0g
Rolling +0.5 to +1.5g
NOTE:
1. Transitory excursions above 14° may be seen during catapult launch.
Figure 4-8. Limitations with Flaps HALF or FULL
4.1.8 Refueling Limitation. Maximum refueling pressure, inflight or on the ground, is 55 psi.
4.1.9 Prohibited Maneuvers
Environmental -
1. Flight in lightning or thunderstorms.
Systems -
1. Takeoff with a FADEC DEGD indication (dual channel line outs).
2. Takeoff with a FCS A or FCS B DEGD.
3. Pulling any FCS circuit breaker inflight except as directed by NATOPS.
4. Use of RALT mode below 500 feet AGL.
5. Use of the auto sever/redeployment function of the ALE-50.
6. Landing with autopilot modes engaged except for the following:
a. Coupled Mode 1 ACLS landings to AN/SPN-46 systems with the FLAP switch in FULL. Mode
1A approaches are permitted with the FLAP switch in HALF.
b. Field landings with FPAH/ROLL engaged.
7. Coupled ACLS approaches to shore based AN/SPN-42 systems. Practice Mode II approaches to
shore based AN/SPN-42 systems are permitted only during day VMC with a backup guidance source
such as ICLS.
A1-F18EA-NFM-000
I-4-8 ORIGINAL
Departure/Spin -
1. Zero airspeed tailslides.
2. Intentional departures/spins.
3. Yaw rates over 40 degrees/second (yaw tone).
4. Holding roll inputs (lateral stick or rudder pedal) past 360° of bank angle change.
5. Inflight selection of RCVY on the SPIN switch.
Selection of manual spin recovery mode (SPIN switch in RCVY) seriously
degrades controllability and prevents recovery from any departure
or spin.
Fuel and Engine Oil -
1. Zero 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).
Loads -
1. Field, FCLP, T&G, and carrier landings with lens settings greater than 4.0 degrees.
2. Pushing beyond -1g above 700 KCAS and below 10,000 feet MSL.
3. Holding lateral stick inputs past 180° of bank angle change when pushing between 0.0 and -1.0g.
4. Abrupt, full aft stick inputs (full aft stick in less than 0.25 seconds) are prohibited with less than
3,500 lb fuel. Under this aft CG condition, full aft stick inputs may exceed the g-limiter's capacity
to prevent an over-g and/or structural loads exceedence.
5. If lateral weight asymmetry exceeds 6,000 ft-lbs, due to either a 2,000 lb-class store or a wing
mounted external fuel tank above half-full, the aircraft is limited to one-half lateral stick in the
direction of the heavy wing when above 400 KCAS.
6. AUX release of external fuel tanks or aerial refueling store.
Flutter -
1. Flight without LAU-127A/A wingtip launcher rails (with power supply and nitrogen bottle
installed).
Flying Qualities -
1. Single-ship takeoffs with 90° crosswind component over 30 knots.
2. Section takeoffs with any of the following conditions:
A1-F18EA-NFM-000
I-4-9 ORIGINAL
a. 90° crosswind component over 15 knots.
b. Asymmetric loading over 9,000 ft-lb not including wingtip missiles or pods.
c. Dissimilar loading except pylons, FLIR, LDT, fuselage missiles, wingtip missiles or pods,
CVERS, MERS, or TERS.
3. Flight with GAIN ORIDE selected above 10° AOA or above 350 KCAS (flaps AUTO), 200 KCAS
(flaps HALF), or 190 KCAS (flaps FULL).
With GAIN ORIDE selected (fixed FCS gains), the aircraft is uncontrollable
above approximately 450 KCAS.
4. Single-ship landings with 90° crosswind component over 30 knots.
5. Section landings with 90° crosswind component over 15 knots.
6. Aerobraking during landing rollout.
4.2 EXTERNAL STORES LIMITATIONS
External stores limitations for external fuel tanks are shown in figure 4-9. For other external stores
limitations, refer to the Tactical Manual, A1-F18EA-TAC-020 (NWP 3-22.5-F/A18 VOL IV). Only
those stores shown in the Tactical Manual may be carried and/or released.
A1-F18EA-NFM-000
I-4-10 ORIGINAL
LIMITATIONS
Sta 6 480-gal Carriage Sta 4/8 480-gal Carriage Sta 6 ARS Carriage
(Stowed and Feathered)
>1,600 lb fuel £ 1,600 lb fuel > 500 lb fuel £ 500 lb fuel > 500 lb fuel £ 500 lb fuel
Altitude (feet MSL) LON 0 to 40,000
Airspeed
(KCAS / IMN)
LON > 15,000 feet MSL
700 KCAS £ 15,000 feet MSL
500/1.3 > 12,000 feet
MSL
500/0.86 £ 12,000 feet
MSL
635 / 1.25 500 / 0.92 575 / 0.92
Nz (g) Symmetrical -2.0 to +6.0 LON -3.0 to +3.0 LON -1.0 to +6.0 -3.0 to +6.0
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本文链接地址：
NATOPS Flight Manual 飞行手册 1(124)
