N769AF
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
5 reports on file, 2010-06-01 – 2018-03-26.
Part: BULKHEAD — CORRODED (FRAME 15) · airframe 9,863 hrs · 9,328 cycles
DURING ANNUAL INSPECTION, CORROSION WAS FOUND ON FORWARD PRESSURE BULKHEAD, LT AND RT SIDE OF FRAME 15. THE CORROSION ON THE LT SIDE WAS LOCATED JUST INBOARD OF THE PRESSURIZATION SAFETY VALVE ABOVE THE LOWER FLANGE. ON THE RT SIDE THE CORROSION WAS LOCATED WHERE THE ECS PNEUMATIC DUCT PASSES THROUGH FRAME 15. REPAIRED IAW SADD-12-0970, 2 SEPARATE REPAIRS. THE REPAIRS LT IAW RM-12-001093 AND RT IAW RM-12-001092 WERE COMPLETED AND THE AIRCRAFT WAS RELEASED FROM ANNUAL INSPECTION.
Part: INDICATOR — ODOR (EHSI) · airframe 8,258 hrs · 7,856 cycles
CREW REPORTED A BURNING ODOR COMING FROM LOWER EFIS TUBE AFTER BLANKING OUT. PERFORMED VISUAL INSPECTION OF EHSI WIRING IAW WDM 34-26-00, NO DEFECTS NOTED. IDENTIFIED BURNING ODOR WITHIN PILOTS EHSI. PERFORMED REPLACEMENT OF PILOT EHSI IAW AMM 12-A-34-26-02-00A-920A-A. OPS TEST OF EHSI GOOD IAW AMM 12-A-34-26-00-00A-903A-A. NO FAULTS FOUND AT THIS TIME.
Part: INDICATOR — FAILED (ZONE 200) · airframe 5,176 hrs · 5,073 cycles
DURING CLIMB-COPILOTS SIDE EHSI FAILURE ALONG WITH ELECTRICAL BURNING FUMES. CMPST MODE OK 2-3 MINUTES LATER, RETURNED TO NORMAL. THE COPILOTS EHSI, PN 066-03125-2500 WAS R & R IAW AMM 12-A-34-26-02-00A-920A-A NO DEFECTS NOTED. THE ACFT INSTRUMENTS, BEHIND INSTRUMENT PANEL, CIRCUT BREAKER PANEL, FLIGHT DECK AREA WIRING AND GROUND BLOCKS, UNDERFLOOR WIRING FOR DEFECTS OR ANY EVIDENCE OF BURNING, NONE FOUND. THE ACFT WAS RELEASED FOR A CHECK FLIGHT, ALL INDICATIONS NORMAL, NO DEFECTS NOTED DURING ANY PHASE OF FLIGHT.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,467 hrs · 3,398 cycles
FLAPS CAWS ILLUMINATED FOLLOWED BY FLAPS ASSEMETRY CALL OUT. FLAPS STOPPED AT AT 17 DEGREES. PUSHER ILLUMINATED SHORTLY AFTER. COMPLIED WITH FLAP CAWS "ON" PROCEDURE AND COMPLIED WITH FOR RELATED FWCU CODES AND RESET IAW AMM "FAULT ISOLATION PROCEDURE" DMC-12-A-27-50-00-00A-420A-A. COMPLIED WITH FLAP FUNCTIONAL CHECKS IAW AMM DMC-12-A-27-50-00-00A-903B-A, OPS AND FUNCTIONAL CHECKS GOOD.
Part: BRAKE DISC — BROKEN (ZONE 700) · airframe 2,709 hrs · 2,604 cycles
((5APR)) DURING A LINE CHECK THE LT BRAKE OTBD BRAKE DISC WAS DISCOVERED BROKEN INTO 4 PIECES. REMOVED DEFECTIVE BRAKE AND INSTALLED (CLEVELAND) MAIN WHEEL AND BRAKE CONVERSION KIT 199-241 ON BOTH MAIN GEAR IAW STC SA01376CH.