G WITH AVIONICS RAMP CHECK FOUND BOTH NAV RCVR#S SELF-TESTINHIBITED. Resolution: DUE TO UNAVAILABILITY OF UPDATED WIRING DIAGRAMS, TRACED WIRE FROM NUTCRACKER CB 3I7CB47 For detailed description of the work complied with see the Work Order Detail report Unless otherwise indicated, all financial values lis

G WITH AVIONICS RAMP CHECK FOUND BOTH NAV RCVR#S SELF-TESTINHIBITED. Resolution: DUE TO UNAVAILABILITY OF UPDATED WIRING DIAGRAMS, TRACED WIRE FROM NUTCRACKER CB 317CB47 TO APU PWR #143 CBS 314CB254, 314CB252, AND 314CB324. IT WAS DETERMINED THAT IN ORDER FOR THE NUTCRACKER HARNESS SWITCH TO RECEIVE DC PO

LOT, 24 Electrical Power, 32 LANDING GEAR; HONEYWELL CORP. Maintenance Manual for the SPZ-8000 INTEGRATED FLIGHT MANAGEMENT SYSTEM; GREYHOUND CORP. NUTCRACKER RIGHT MAIN DC AND/OR ESSENTIAL DC MODIFICATION, ELECTRICAL DhU. No. 32122589, dated 12-25-89. see DER APPROVED FAA Form 8110-3 dated January 10, 19

est and Code 276001 Ground Spoiler System - Functional Test and noted no abnormal operation. Note: Disconnecting ASC94P901B is the same as removing NUTCRACKER RELAY It: Disconnecting ASC94P902B is the same as removing NUTCRACKER RELAY 46; Disconnecting ASC94P903B is the same as removing POWER LEVER IDLE R

STREAM AEROSPACE CORPORATION DWG.#'1159RDF631 REPAIR V. FIN R. BEAM DEV. TO ASC 231 SP 50G DEV. AV 25006 DEV. TO ASC 294 , DEV. AOA W.D. LOG. NUTCRACKER W.O. STALL BARRIER SYSTEM SE 21318004-01 A.F.M.S. REQUIRED G -IIB -82-001 RETRACTABLE LANDING LITES G -IIB -82 -003 SIX PANEL SPEED BRAKES 4111