N707AX
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.
18 reports on file, 2001-01-31 – 2011-09-30.
Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 80,471 hrs · 20,991 cycles
CORROSION AROUND NUTPLATE HOLES FOR DOOR LINER OF FLC DOOR. REPAIRED IAW SRM.
Part: CHANNEL — CRACKED (ZONE 400) · airframe 80,471 hrs · 20,991 cycles
CHANNEL CRACKED INSIDE NR 1 STRUT DOOR 437AR. REPAIRED NR1 PYLON CHANNEL IAW SRM.
Part: BEAM — CRACKED (ZONE 400) · airframe 80,471 hrs · 20,991 cycles
NR 2 PYLON OTBD LONGITUDINAL BEAM CRACKED. R & R BEAM IAW SRM.
Part: STIFFENER — CORRODED (ZONE 500) · corrosion level 2 · airframe 80,471 hrs · 20,991 cycles
LT WING T/E STIFFNER CORRODED AT WS 430. R & R STIFFNER IAW SRM.
Part: STRUCTURE — CRACKED (ZONE 100) · airframe 80,471 hrs · 20,991 cycles
NWW LT STA 287 CHORD CRACKED APPROX 11" FROM TOP OF CHORD. REPAIRED CHORD AT STA 287 LT IAW SRM.
Earlier reports · 2001–2008 · 13 reports
2008
Part: DOOR FRAME — CORRODED (AFT CARGO DOOR) · airframe 79,619 hrs · 20,506 cycles
AFT LOWER CARGO DOOR FRAME BELOW VENT DOORS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED CHORD DOOR BEAM IAW B767 SRM 51-40-02.
2005
Part: FITTING — CRACKED (LT WING SPOILER) · airframe 75,689 hrs · 18,788 cycles
LEFT WING SPOILER TORQUE TUBE HINGE FITTING CRACKED AT RSS 714.10. REMOVED AND REPLACED HINGE FITTING.
2004
Part: SEAL — TORN (L2 WINDOW) · airframe 74,817 hrs · 18,463 cycles
DURING R1 PREFLIGHT, DISCOVERED CAPTAINS NR 2 WINDOW CRANK BINDING TOWARDS CLOSE. FOUND L2 WINDOW SEAL TORN AND CATCHING ON WINDOW, REMOVED AND REPLACED L2 WINDOW SEAL IAW AMM 56-11-11-4.
Part: SCREW — DEFECTIVE (SLIDING WINDOW) · airframe 74,774 hrs · 18,447 cycles
DURING MAINTENANCE INSPECTION AT BFI, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT CLOSE. NR 2 L WINDOW. REPLACED NR 2 LT WINDOW BALL SCREW AND NUT ASSEMBLY IAW MM CHAP. 56-11-04-4.
2003
Part: WINDOW — STUCK (COCKPIT) · airframe 73,418 hrs · 17,960 cycles
FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED FIRST OFFICER'S WINDOW IAW B767 MM.
Part: SHROUD — DAMAGED (RT ENGINE) · airframe 71,827 hrs · 17,369 cycles
REVERSER ISOLATION VALVE EICAS MESSAGE AND REVERSER ISOLATION LIGHT ILLUMINATED AFTER LANDING WITH REVERSER LEVERS STOWED. RT ENGINE FAN EXIT DUCT, OUTER SHROUD, FAN STARTORS DAMAGED AND OUTER FAN SHROUD PANELS WERE MISSING. ENGINE AND TRHUST REVERSER CHANGED IAW B767 MM.
2002
Part: SLAT — MALFUNCTIONED (WING) · airframe 70,738 hrs · 16,986 cycles
FLT 407- THE CREW DECLARED AN EMERGENCY AND PERFORMED A GO-AROUND INBOUND TO ILN. EICAS MSG LE SLAT ASYM DISPLAYED. LEADING EDGE LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. COMPLETED FIM PROCEDURES IAW B767 FIM 27A-81-00. LIGHTS AND MESSAGE EXTINGUISHED DURING PROCEDURES. TESTED GOOD. CYCLED FLAPS AND SLATS. NO FURTHER FAULTS.
Part: BEARING — SEIZED (AILERON CONTROL) · airframe 70,728 hrs · 16,983 cycles
CAPTAIN'S AND FIRST OFFICER'S AILERON CONTROL WHEEL BINDING. COMPLIED WITH FIM 27A-11-00, FIG 106, BLOCK 1,2. FOUND BEARING ON LEFT WHEEL WELL QUADRANT CENTERING FORCE SEIZED. REPLACED BEARING IAW BOEING STANDARD OVERHAUL PRACTICES MANUAL 20-50-03. AILERONS OPERATED NORMALLY.
Part: BATTERY — DISCHARGED (CABIN) · airframe 70,529 hrs · 16,910 cycles
DURING MAINTENANCE INSPECTION, FOUND FLIGHT DECK REMOVABLE EMERGENCY EXIT SIGN BATTERIES LOW. REPLACED BATTERIES IAW B767 MM 33-51-01.
Part: MODULE — MALFUNCTIONED (COCKPIT) · airframe 70,427 hrs · 16,865 cycles
EICAS MESSAGE GEAR DISAGREE DISPLAYED AND GEAR AMBER LIGHT ILLUMINATED WITH GREEN DOWN LIGHTS ILLUMINATING. ACCOMPLISHED ABNORMAL PROCEDURE. ON FINAL, GPWS GAVE TOO LOUD GEAR WARNING. ACCOMPLISHED GO AROUND. WHEN GEAR EXTENDED AGAIN, INDICATIONS WERE NORMAL. REMOVED AND REPLACED THE LANDING GEAR LEVER MODULE IAW B767 AMM 32-31-01-4. OPS CHECKED GOOD.
Part: FCU — MALFUNCTIONED (NR 1 ENGINE) · airframe 69,896 hrs · 16,690 cycles
DURING CLIMB, THE NR 1 ENGINE STARTED TO ACCELERATE UNCOMMANDED. PULLED THE THROTTLE TO IDLE, ENGINE DID NOT RESPOND. THE NR 1 ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO ILN WHERE IT LANDED UNEVENTFULLY. REPLACED THE LEFT TT2 SENSOR AND THE LEFT FUEL CONTROL UNIT IAW B767 MM.
2001
Part: WARNING LIGHT — FALSE INDICATION (MLG) · airframe 67,142 hrs · 15,789 cycles
A DISAGREE MESSAGE WAS DISPLAYED AND A GEAR AMBER LIGHT ILLUMINATED WITH A GEAR GREEN DOWN INDICATION LIGHT. RECYCLED LANDING GEAR AND INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND PERFORMED A BITE CHECK. THE CHECK SHOWED NR 1 AND 2 GEAR LEVER SWITCH ON PSEU. MAINTENANCE CHECKED THE LANDING GEAR CONTROL MODULE IAW B767 MAINTENANCE MANUAL 32-31-01. NO DEFECTS WERE FOUND.
Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 67,142 hrs · 15,789 cycles
A DISAGREE MESSAGE WAS DISPLAYED AND A GEAR AMBER LIGHT ILLUMINATED WITH A GEAR GREEN DOWN INDICATION LIGHT. RECYCLED LANDING GEAR AND INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND PERFORMED A BITE CHECK. THE CHECK SHOWED NR 1 AND NR 2 GEAR LEVER SWITCH ON PSEU. MAINTENANCE CHECKED THE LANDING GEAR CONTROL MODULE IAW B767 MAINTENANCE MANUAL 32-31-01. NO DEFECTS WERE FOUND.