N712AX
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, 2009-05-30 – 2011-01-05.
Part: DOOR — CRACKED (E/E BAY) · airframe 61,337 hrs · 21,233 cycles
DURING ROUTINE C CHECK INSPECTION FOUND A CRACK UNDER OUTBOARD HYDRAULIC BAY DOOR AFT LOWER PIN RECEPTACALE AND PIN GOUGES IN CHANNEL UNDER AFT LOWER RECEPTACALE FORWARD OF AFT ONE. REPAIR WAS ACCOMPLISHED IAW SRM 51-30-01, 51-40-02, BORING PROCESS BAC 5946, AMES PROCESS STANDARDS MANUAL CH5 SEC 01, AND REA NUMBER B654-60306.
Part: CHANNEL — CRACKED (ZONE 100)
DURING ROUTINE C CHECK HEAVY MAINTENANCE INSPECTION EVENT FOUND A CRACK UNDER OUTBOARD HYDRAULIC BAY DOOR AFT LOWER PIN RECEPTACALE AND PIN GOUGES IN CHANNEL UNDER AFT LOWER RECEPTACALE FORWARD OF AFT ONE. REPAIR WAS ACCOMPLISHED IAW B767 SRM 51-30-01, 51-40-02, BORING PROCESS BAC 5946, AMES PROCESS STANDARDS MANUAL CH5 SEC 01, AND REA NUMBER B654-60306.
Part: STRUCTURE — DELAMINATED (LT MLG DOOR) · airframe 61,337 hrs · 21,233 cycles
DURING ROUTINE C CHECK INSPECTION FOUND DELAMINATION ON THE LEFT MAIN LANDING GEAR BODY DOOR AT AFT STOP PAD. REPAIR WAS ACCOMPLISHED IAW B767 SRM 52-00-02, 52-80-02 AND 51-70-5.
Part: UNKNOWN — UNKNOWN (UNKNOWN)
JUST AFTER ROTATION, A LOUD BANG WAS HEARD AND THE ACFT HAD A NOTICEABLE SHUDDER. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDING WAS UNEVENTFUL. SUSPECTED BIRD STRIKE.
Part: PANEL — CORRODED (FUSELAGE) · airframe 60,952 hrs · 21,155 cycles
FAYING SURFACE FOR PANEL 655 EB CORRODED AT LWR I/B FORWARD EDGE ON INNER SURFACE. REPAIRED LOWER CHORD IAW B767 SRM 51-70-02 FIG 1 PG 3.
Part: JACKSCREW — DAMAGED (HORIZ STAB) · airframe 60,952 hrs · 21,155 cycles
STAB TRIM ACTUATOR BALL NUT/SCREW (JACKSCREW) FAILED INSPECTION. REMOVED AND REPLACED JACK SCREW. P/N 251T4310-1 PITTING.
Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 60,952 hrs · 21,155 cycles
FWD SERVICE DOOR, CORNER SCUFF PLATES HAVE CORRODED STIFFENER CHANNELS. FABBED NEW STIFFENER CHANNELS FROM 7075 T6 .050 AND INSTALLED IAW B767 SRM 51-40-02.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 60,952 hrs · 21,155 cycles
RBL 25 NOSE WHEEL WELL VERTICAL CHORD STA 287 IS CRACKED ABOVE WL 159. REPAIRED VERTICAL CHORD NWW RBL 25 STA 287 ABOVE WL 159 IAW B767 SRM 51-70-12 FIG 1, .5 INCH CRACK.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,952 hrs · 21,155 cycles
CRACK INDICATION IN SKIN FS 1654.5 AT APPROX S3R VERIFIED WITH ET. REPAIRED IAW B767-200 SRM 53-80-01, 1 INCH CRACK.
Part: STIFFENER — CORRODED (TE FLAP) · airframe 60,952 hrs · 21,155 cycles
STIFFENER CORRODED ON RIGHT I/B FLAP FORWARD SPAR INBOARD END. REMOVED & REPLACED STIFFENER IAW B767 SRM 51-40-02.