The F-15 A/B Eagle with F100-PW-220 Engines
    and without conformal or external fuel tanks,
    has the following flight characteristics
    Length:  19.43 m  (63.75 ft)
    Wingspan:  13.05 m  (42.81 ft)
    Height:  5.63 m  (18.46 ft)
    Maximum Mach: 2.2
    Maximum Altitude:  18,181 m  (60,000 ft) (Cabin Pressure Control System Limitation)
    Basic Operating Weight:  12,387 kg  (27,500 lb)
    Full Internal Fuel Weight: 5,338 kg  (11,850 lb).
    Aircraft Gross Weight = 17,725 kg  (39, 350 lb)
       with full internal fuel
    Maximum Allowable Gross Weight:  25,225 kg  (56,000 lb)
    Maximum Payload:  7,260 kg  (16,000 lb)
    Forward Center of Gravity Limit: 22% MAC (gear down)
    Aft Center of Gravity Limit:  29.9% MAC
    Centerline Store Acceleration Force Factor Limit (Store Weight x Maximum G Allowed) [ Example uses weight
    of full centerline fuel tank multiplied by G limit]:
         4581 lbs. x 6.5 G  =  29, 776 lbs (13, 412 Kg).
    Centerline Store Maximum Dimensions:
    Undercarriage width limit:  1.45 m  (4 ft, 10 in.)
    Undercarriage vertical clearance:  1.35m    (4.5 ft)
    Undercarriage length limit:  8.1 m (27.0 ft) {Nose gear door to tail hook housing}

    The F-15, a fourth generation long-range air superiority fighter, was introduced in 1976 with approximately
    410 F-15A/B model aircraft produced.  In 1979, U.S. production proceeded to more advanced models, with foreign production continuing
    until the present time.  A total of 1,286 F-15s were produced for the
    United States. They still operate within the USAF and ANG today, as well as in selected foreign nations.
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