9 % - Repeat/Recur Rate - Percentage of repeats or recurs divided by total of pilot-reported discrepancies.18 % - Cannibilization Rate - Percentage of cannibalizations (parts taken from one aircraft to fix another) divided by number of sorties.
F 15A COCKPIT CODE
75 % - Fix Rate - Percentage of Code 3 aircraft fixed in eight-hour period.Code 3 is an aircraft not mission capable until problem is fixed. Code 2 is an aircraft with a problem but is still mission capable. Different aircraft codes indicate mission capability upon completion of a sortie: Code One is mission capable. 19 % - Break Rate - Number of Code 3s divided by total number of sorties flown.6 % - Abort Rate - Rate of aircraft that cannot fly sorties due to ground or air abort.9 % - Not Mission Capable for Supply - Percentage not mission capable for supply reasons.15 % - Not Mission Capable for Maintenance - Percentage not mission capable for maintenance reasons.81 % - Mission Capapble - Percentage of aircraft readily available to do the mission.AN/APG-82 AESA X-band pulsed-Doppler radar Ĭlose to $100 million (including spares and support) for export customers.AN/ALR-56 radar warning receiver (RWR).AN/ALQ-135(V) internal countermeasures system.AN/APG-70 X-band pulsed-Doppler radar.AN/APG-63 V3 AESA X-band pulsed-Doppler radar.AN/APG-63 V2 AESA X-band pulsed-Doppler radar.AN/APG-63 X-band pulsed-Doppler radar.Up to three 610-US gal (2309-liter~ drop tanks ģ,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks.ģ,100 nm (3,570 miles 5745 km) ferry range with CFTs and drop tanksĢ,400 nm (2,765 miles 4445 km) with drop tanksġ,000 nm (1,150 mi 1,853 km) Max Combat RadiusĦ85 nm (790 miles 1270 km) combat radius Two Pratt and Whitney FIOO-P-220 turbofans each rated at 14,670 lb st (65.26 kN) dry and 23,830 lb st (106.0 kN) with afterburning or,Īfter August 1991, two FlOO-PW-229 each rated at 17,800 lb st (79.18 kN) dry and 29,100 lb st (129.45 kN) with afterburning ġ,433 kt (1,6 km/h) maximum level speed 'clean' at high altitudeĤ95 kt (570 mph 917 km/h) cruising speed at optimum altitude Two Pratt & Whitney F100-PW-100 turbofan engines with afterburners, each rated at 25,000 pounds engine ( 11,250 kilograms) Boeing (McDonnell Aircraft and Missiles Systems)
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