N746AX
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.
10 reports on file, 2007-08-26 – 2010-08-23.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,702 hrs · 34,479 cycles
SKIN BULGING AT RIVET AT STA 1544 STRINGER 36L. REMOVED AND REPLACED STRINGER SECTION STA 1550-1491 IAW B767 SRM 53-00-03 FIG 51-40-02.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 72,702 hrs · 34,479 cycles
RT STRINGER OUTBOARD OF DOOR NR 311AZ AT STA 1702, 1678 STRINGER ATTACH ANGLE CRACKED. REMOVED AND REPLACED STRINGER ATTACH ANGLES STA 1678 AND STA 1702 IAW B767 SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,330 hrs · 34,309 cycles
UPPER CARGO COMPARTMENT INTERCOSTAL STA 1043 HAS A CRACKED PRESSURE DECK PYLON FITTING ANGLE. REPLACED CRACKED FITTING IAW B767 SRM 51-40-02 AND 51-20-05.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 72,330 hrs · 34,308 cycles
EXTRUDED T-STIFFENER STA 826 ON KEEL BEAM IS CRACKED. REMOVED AND REPLACED STIFFENER IAW B767 SRM 51-40-2, P/N 145T8629-2.
Part: DISPLAY — BURNED OUT (COCKPIT) · airframe 71,617 hrs · 33,985 cycles
ON RAMP ELECTRIC SMOKE IN COCKPIT. EVACUATED AIRCRAFT. FOUND RT FMC CDU SHORTED OUT (BURNT) ALSO EQUIP COOLING BYPASS SW IN BY-PASS. RETURNED TO NORMAL POS. REMOVED AND REPLACED RT FMC CDU IAW AMM 34-61-02-2. OPS CHECKED NORMAL.
Part: WINDOW — CRACKED (COCKPIT) · airframe 71,578 hrs · 33,968 cycles
F/O'S WINDSHIELD CRACKED. AIR TURNBACK. CHANGED F/O'S WINDSHIELD ASSY.
Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 70,441 hrs · 33,472 cycles
MAIN CARGO DOOR LIGHT ON AFTER TAKEOFF, RETURNED TO DEPARTURE. ACCOMPLISHED MX PRACTICES ON DOOR OPERATION AND CHECKED ALL EXTERIOR DOOR LOCK INDICATOR'S ARE WHITE. DOOR LIGHTS OUT AND OPS CHECK GOOD IAW AMM 52-32-00-2.
Part: MOUNT — RUSTED (ENGINE) · airframe 70,236 hrs · 33,385 cycles
AFT ENGINE MOUNT WAS RUSTED AT LOWER RIGHT LUG. REMOVED AND REPLACED AFT MOUNT ASSEMBLY IAW B767 AMM 71-21-02-4. ENGINE REMOVED AND REINSTALLED ON JOB CARD 7010.
Part: METERING VALVE — DEFECTIVE (BRAKE) · airframe 69,666 hrs · 33,129 cycles
RT HYDRAULIC QUANTITY DECREASED TO .34 QTY. STABLE WITH EDP DEPRESSURIZED AND ACMP OFF. EVENT OCCURRED IN CRUISE, GEAR OFF, FLAPS UP. FOUND BRAKE METERING VALVE MODULE BYPASSING HYDRAULIC FLUID FROM RT TO CENTER SYSTEM. REMOVED AND REPLACED BRAKE METERING VALVE MODULE (MAIN) IAW AMM 32-41-03-4. SYSTEM OPS AND LEAK CHECKED GOOD. (S)
Part: UNKNOWN — ODOR (CABIN) · airframe 68,786 hrs · 32,730 cycles
SMELLED SMOKE IN FLIGHT AFTER TAKEOFF. SUSPECT HIGH PRESSURE VALVE STAYED OPEN WHEN COMMANDED TO CLOSE. VERIFIED ALL CIRCUIT BREAKERS TO BE NORMAL (NOT POPPED OUT). RAN ENGINE UP, NO ODOR PRESENT AS PER B767 AMM 71-00-00.