The is specifically titled the NATOPS Flight Manual Performance Charts for the Navy Model F/A-18A, F/A-18B, F/A-18C, and F/A-18D.
Basic aerodynamic tracking data for early variants equipped with standard powerplant models. A1-F18AC-NFM-210: High-Performance Engine Metrics
: Pay close attention to the Gross Weight charts. For example, the F/A-18 typically won't allow max G-loads until the weight drops below approximately 32,357 lbs Supplemental Nature
(A1-F18AC-NFM-000) is considered incomplete without these supplemental performance volumes. Aircraft Covered:
: Designates the specific airframe group, spanning the single-seat F/A-18A and F/A-18C variants, along with their two-seat counterparts, the F/A-18B and F/A-18D. NFM : Acronym for NATOPS Flight Manual . a1-f18ac-nfm-200 210
: Essential minimum wind-over-deck (WOD) matrices based on catapult engine pressures and aircraft launch weights.
While the standard NATOPS manual (A1-F18AC-NFM-000) covers normal and emergency procedures, systems descriptions, and general operating limits, the required for mission planning, combat maneuvering, and flight testing. Core Technical Differences: NFM-200 vs. NFM-210
: Stands for NATOPS Flight Manual (Naval Air Training and Operating Procedures Standardization).
: This could indicate a quantity, size, version number, or perhaps measurements related to the product. The space between "200" and "210" might imply a range or two separate specifications. The is specifically titled the NATOPS Flight Manual
The is the base NATOPS Flight Manual (Naval Air Training and Operating Procedures Standardization) for the F/A-18 A/B/C/D Hornet, covering procedures and systems. However, the performance data—charts, tables, and graphs determining acceleration, climb rates, turn performance, and fuel burn—is contained in specialized supplements.
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: Standard performance testing charts typically presume an airframe gross weight of 33,696 lbs , loaded with two AIM-9 Sidewinders and two AIM-7 Sparrows or AIM-120 AMRAAMs. 3. Powerplant Deviations (-200 vs -210) For example, the F/A-18 typically won't allow max
: The exact speed (typically between 320 to 360 knots for the Legacy Hornet) where the aircraft can turn continuously without losing airspeed or altitude.
If you have come across this code on a shelf or a digital asset management system, here is how to treat it:
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Charts mapping out the Climb Speed Schedule (CSS) and Peak Rate of Climb (PRC) to help pilots optimize their ascent to specific flight levels.