N819AA

ATA 2434

Part: STARTER GEN — FAILED (NR 1)

OKC- FLT 92269 - DUAL GEN FAIL; CAUSED BATTERIES TO TRIP OFF-LINE, NR 1 FAILED ON, NR 2 FAILED OFF. CREW LOST NR 2 GEN, ACCOMP SINGLE GEN FAIL CHKLIST, RESETTING GEN TWICE. 4 MINUTES LATER, LOST NR 1 GEN, BATTERIES KICKED OFF-LINE. ACCOMP DOUBLE GEN FAIL, BATTERY FAIL CHKLIST. CREW GOT BATTERIES BACK ON-LINE, DECLARED EMERG, REQUESTING EQUIP TO ROLL. ACFT MADE NORMAL LANDING OKC, TAXIED INTO AAR ON SHIPS BATTERY POWER. MAINT DISPATCHED FROM YIP MAINT BASE. FOUND NR 1 ENG WOULD NOT START. NR 1 STARTER/GEN SHOWED SIGNS OF INTERNAL FAILURE. NR 1 STARTER/GEN REPLACED. NR 1, NR 2 GEN CONTROL UNITS REPLACED. DC GEN SYS OPER CHKED ON GROUND IAW DA20 MM 24-30-00, PGS 501-505. ACFT RETURNED TO SERVICE.(X)

ATA 3260

Part: SWITCH — FAILED (RT MLG)

DSM - RIGHT MAIN GEAR GREEN LIGHT DID NOT COME ON DURING NORMAL EXTENSION. AIRCRAFT FLIGHT MANUAL EMERGENCY EXTENSION PROCEDURE USED TO EXTEND GEAR AT WHICH TIME GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT AT INTENDED DESTINATION AT DSM. NO OTHER EMERGENCY PROCEDURES REQUIRED. TROUBLESHOOTING DETERMINED THAT THE RIGHT GEAR DOOR ACTUATOR POSITION SWITCH WAS FAULTY AND PREVENTED THE RIGHT MAIN GEAR FROM SEQUENCING AND EXTENDING NORMALLY. THE GEAR DOOR ACTUATOR SWITCH WAS REPLACED AND THE LANDING GEAR CYCLED WITH NO DEFECTS NOTED. (M)

ATA 7200

Part: ENG — FLAMED OUT (RIGHT)

YIP - THE RT ENG FLAMED OUT DURING PERFORMANCE OF A MAX ALT ACCELERATION TEST. TEST FLT TO PERFORM THIS CHK ON THE RT ENG WAS BEING DONE TO DETERMINE IF PREVIOUS FLAME OUT PROBLEM HAD BEEN RESOLVED, REF MRR Y2PA-96-008. NO EMERG PROCEDURES REQUIRED. A/C RETURNED. REF ORIG MRR DATED 7-15-96 FOR PREVIOUS REWORK. STG 1/2 TURBINE AIR NOZZLE AND FAN NOZZLE WERE REPLACED WITH UNITS OF LARGER AREA. ENG GROUND RUN INDICATED MAIN FUEL CNTRL TRIMMING PROPERLY, RESULTING IN REPLACEMENT WITH .0 TSO MAIN FUEL PUMP AND MAIN FUEL CNTRL. ENG GRD RUN SUCCESSFUL AND RESULTING TEST FLT AS 35,000 FT TO PERFORM MAX ALT ACCELERATION TEST ALSO WAS SUCCESSFUL ON FALCON. NO PARTS DEFECT, ONLY RT COMB OF AREAS WERE NECESSARY. (M)

ATA 3414

Part: PITOT TUBE — BLOCKED (RT COCKPIT)

ELP - FLT 17945 - TAKEOFF ABORTED, NO EMERGENCY PROCEDURES NECESSARY. THIS IS A REPEAT INSTANCE OF PREVIOUS DIFFICULTY REPORTED ON MISR Y2PA-96-052, DATED 7-30-96. REPLACED COPILOT'S AIRSPEED INDICATOR. CHECKED SYSTEM PER FALCON MM 34-10-1. ALSO CHECKED MACH OVERSPEED WARNING SYSTEM IAW FALCON MM 34-10-4 WITH NO DEFECTS NOTED. ACFT ATTEMPTED DEPARTURE ON 8-1-96 AND REPORTED COPILOT'S AIRSPEED INDICATOR STUCK AT VARIOUS AIRSPEEDS. PROVIDED ERRONEOUS INDICATIONS. ACFT RETURNED TO ELP. NO EMERGENCY PROCEDURES NECESSARY. MAINTENANCE FOUND A RESTRICTION IN THE COPILOT'S PITOT TUBE. RESTRICTION WAS BLOWN OUT WITH NITROGEN. TESTED PITOT SYSTEM IAW FALCON MM 34-10-1 AND C/W PITOT/STATIC LEAK TEST IAW FAR 91-

ATA 3411

Part: PITOT DRAIN — RIGHT (PLUGGED)

ON CLIMB-OUT, V2 120 KTS ON LT SIDE, RT SIDE SHOWED 20 KTS LWR. AS ALT INCREASED, A/S DIFFERENTIAL INCREASED AND EPR DECREASED SIGNIFICANTLY, FL 310 A/S ON RT SHOWED 400 KTS PLUS AND MACH O/S WARN SOUNDED. ALL OTHER GAUGES SHOWED NORM, INCLUDING PILOTS A/S IND. ON DESCENT A/S DIFFERENTIAL DECREASED AND EPR STARTED TO SHOW NORM. A/C RETURNED. NO EMERG PROCEDURES NECESSARY. FOUND FOREIGN OBJECT IN PITOT DRAIN BLOCK FROM RT PITOT TUBE. REMOVED ALL DEBRIS, PRESS CHK'D AND LEAK CHK'D RT PITOT/STATIC SYS IAW FALCON MM 34-10-1. OP CHK'D MACH O/S WARN SYS IAW FALCON MM 34-10-4 WITH NO DEFECTS NOTED. PERFORMED PWR ASSURANCE RUN OF BOTH ENG'S IAW FALCON 20 MX INSPECT PROCEDURES MANUAL W/NO DEFECTS NOTED. (M)

ATA 5311

Part: SKIN — DENTED (FUSELAGE)

YIP - DENT IN LEFT FORWARD FUSELAGE SKIN, 45 INCHES AFT OF FRAME NR ZERO (1 INCH BY 1 INCH). REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER F20 SRM 51-10-21 AND USA JET ENGINEERING AUTHORIZATION NR 96-53-03. PART TOTAL CYCLES, 9,307. (X)