XR drag reduction system, including recontoured wing leading edge, ailerons, flaps, outboard wing, tip fin cuff, inboard wing, engine pylon, engine nacelle and convergent- diverget nozzles. (LEARJET 25C all S/N) (LEARJET 24F s/n 25-206 thru 25-229)
Replacement Thrust Reverser Accumulator for the TR3000 Thrust Reverser System.
Installation of access doors in engine nacelle according to Drawing 375201, Revision A, dated 1/13/78, or later FAA approved revision.
Installation of Woodward Electronic Engine synchronizer system.
Installation of electronic engine synchronizer system.
Installation of Bizjet International Inlet Anti-ice Heat Blanket.