N748AX
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.
9 reports on file, 2006-10-17 – 2010-07-06.
Part: WINDOW — CRACKED (COCKPIT) · airframe 74,344 hrs · 34,630 cycles
DURING CLIMB OUT, L1 WINDOW CRACKED, THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED L1 WINDOW. OPS CHECK GOOD IAW AMM 56-11-01. ACFT WAS RETURNED TO SERVICE.
Part: MICROWAVE OVEN — DEFECTIVE (ZONE 900) · airframe 73,335 hrs · 34,186 cycles
DURING CRUISE, WHILE BEING USED THE MICROWAVE STARTED SPARKING AND EMITTED ELECTRICAL ODOR. THE CREW SHUT MICROWAVE OFF. LANDED WITHOUT FURTHER INCIDENT. MX REMOVED MICROWAVE, PULLED AND COLLARD CIRCUIT BREAKER IAW NEF 25-20-01-01. ACFT WAS RETURNED TO SERVICE.
Part: ACTUATOR — OUT OF ADJUST (THRUST REVERSER) · airframe 73,254 hrs · 34,147 cycles
DURING CRUISE, THE LT ENG REVERSE AMBER LIGHT REMAINED ON AFTER FWD THRUST SELECTED, THRUST LEVER COULD BE ADVANCED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FIM 78-36-00 AND FOUND THE CTR ACTUATOR OUT OF ADJUSTMENT. MX ADJUSTED CTR ACTUATOR. OPS CHECK GOOD IAW MM 78-36-00 PAGE 505-507. ACFT WAS RETURNED TO SERVICE.
Part: STARTER — UNKNOWN (NR 1 ENGINE) · airframe 69,789 hrs · 32,786 cycles
OUT OF SJO EN ROUTE TO MIA, THE NR 1 ENGINE OIL QUANTITY STARTED TO DECREASE. THE CREW ELECTED TO DIVERT TO GCM. CREW PULLED THE THROTTLE BACK TO IDLE AND MAINTAINED GOOD OIL PRESSURE. DID NOT HAVE TO SHUT THE ENGINE DOWN BUT DID DECLARE AN EMERGENCY. REMOVED STARTER AND FOUND O-RING CUT DUE TO A BURR ON THE STARTER THRUST LINK. REMOVED SHARP EDGE OF BURR AS REQUIRED. INSTALLED NEW PACKING AND REPLACED STARTER IAW AMM 80-11-01 AS PRECAUTION. SERVICED OIL TANK AS PER AMM 12-13-01. ACCOMPLISHED ENGINE RUN-UP FOR 10 MINUTES. NO LEAKS NOTED AS PER B767 AMM 71-00-00. (LEFT ENGINE)
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,749 hrs · 32,774 cycles
CRACK APPROXIMATELY 4 INCHES IN FUSELAGE SKIN AT AFT LOWER CORNER OF R1 DOOR. REPAIRED CRACK IN AFT LOWER CORNER OF R1 DOOR IAW REA B653-55002 MR.
Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 69,749 hrs · 32,774 cycles
STIFFENER CRACKED AT FORWARD LOWER CORNER OF PANEL 437 BL CUTOUT INSIDE. REPAIRED CRACKED STIFFENER IAW REA B654-54-930 MR.
Part: STRUCTURE — CRACKED (NACELLE) · airframe 69,749 hrs · 32,774 cycles
CRACKED STRUCTURE JUST BELOW PANEL 437BR OPENING AT FORWARD LOWER CORNER. REPAIRED AREA IAW REA B654-64932.
Part: BULKHEAD — CRACKED (BS 977) · airframe 69,749 hrs · 32,774 cycles
CRACK 3.5 INCH LONG AT FS 977 AFT SIDE WL 30 RIGHT ON CANTED BULKHEAD SKIN RUNNING LENGTH WISE ALONG STIFFENER. REPAIRED AREA IAW B767 SRM 53-50-51.
Part: STRUCTURE — CORRODED (LEFT WING) · airframe 69,749 hrs · 32,774 cycles
CORRODED WING UPPER SURFACE TIE APPROXIMATELY WS 190. REMOVED CORROSION AND REPAIRED AREA IAW REA B657-54918.