# N796AX: Boeing 767-281, registration cancelled 2021-09-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 29, 2021 - Exported to: Poland - Status when cancelled: Valid registration - Airframe: [Boeing 767-281](https://openairdocs.org/model/boeing-767-281) (registry code 1385129) - Engine: [GE CF6-80A](https://openairdocs.org/engine/ge-cf6-80a) (registry code 30093) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs) - Serial number: 23146 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 2, 2015 - Certificate issued: September 10, 2021 - Last registry action: September 10, 2021 - Mode S code: AACE65 - Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC) - Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N796AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=796AX - Page: https://openairdocs.org/deregistered/N796AX-2021-09-29 From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 767-281: https://openairdocs.org/model/boeing-767-281.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ABXA200910300060](https://openairdocs.org/sdr/ABXA200910300060), Oct 28, 2009: STRUCTURE. CRACKED. NOSE WHEEL WELL VERTICAL CHORD AT LBL 25 AND STA 287 IS CRACKED IN RADIUS APP .687 INCH IN LENGTH. LOCATED 11.5 INCHES BELOW W/W CEILING PNL. REPAIRED VERTICAL - [SDR ABXA200910300058](https://openairdocs.org/sdr/ABXA200910300058), Oct 28, 2009: JACKSCREW. CORRODED. AREA OF DISTORTION ON BALL SCREW THREAD AND SMALL SPOT OF CORROSION ON BOTTOM THREAD OF JACKSCREW. REMOVED AND REPLACED HORIZONTAL STAB JACKSCREW IAW B767 AMM 2 - [SDR ABXA200910300057](https://openairdocs.org/sdr/ABXA200910300057), Oct 28, 2009: FITTING. CRACKED. FORWARD LOWER CARGO DOOR CUTOUT CENTER HORIZONTAL ROLLER GUIDE FITTING CRACKED. CRACK LENGTH 4.5 INCH. ROLLER FITTING MISSING ALL 4 BOLTS (PUT TOGETHER WITH PIN - [SDR ABXA200910300056](https://openairdocs.org/sdr/ABXA200910300056), Oct 28, 2009: COWLING. CRACKED. NR 2 ENG O/B FAN COWL IS CRACKED ON EXTERIOR SURFACE AFT OF STATIC SENSE PORT. CRACK LENGTH 4 INCHES. REMOVED NR 2 ENG O/B COWL. REPAIRED ON WO 10074-0006. RE-I - [SDR ABXA080218](https://openairdocs.org/sdr/ABXA080218), Aug 9, 2008: BOLT. MISSING. LT MAIN LANDING GEAR TRUNNION DOOR FITTING ON TOP OF STRUT MISSING AFT BOLT AND ATTACHING HARDWARE. INSTALLED CORRECT HARDWARE PER IPC 32-12-01-5, SHEET 2 AND A - [SDR ABXA080110](https://openairdocs.org/sdr/ABXA080110), Mar 19, 2008: LIGHT. INOPERATIVE. MAINTENANCE AT ILN FOUND MAIN ENTRY DOOR EMERGENCY ESCAPE LIGHT LENS CRACKED AND LIGHT INOP. REMOVED AND REPLACED MAIN ENTRY DOOR EMERGENCY ESCAPE LIGHT ASSEMBL - [SDR ABXA080062](https://openairdocs.org/sdr/ABXA080062), Jan 29, 2008: DOOR FRAME. CORRODED. FORWARD LOWER CARGO DOOR FRAME UNDER VENT DOORS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED FORWARD LOWER CARGO DOOR FRAME IAW B767 SRM. - [SDR ABXA080061](https://openairdocs.org/sdr/ABXA080061), Jan 28, 2008: BEAM. CORRODED. I-BEAM DIRECTLY BELOW DEPRESSURIZATION VENTS ON AFT LOWER CARGO DOOR HEAVILY CORRODED. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-2. - [SDR ABXA060228](https://openairdocs.org/sdr/ABXA060228), Jul 6, 2006: STRAP. CORRODED. UPPER SPAR CAP STRAP AT RT WING STA 792 HAD INTERGRANULAR CORROSION. REPAIRED AREA IAW REA B657-54341. - [SDR ABXA060227](https://openairdocs.org/sdr/ABXA060227), Jul 6, 2006: SHEAR TIE. CORRODED. FRAME CORRODED AT STA 1219 BETWEEN S38-47R. REMOVED AND REPLACED SHEAR TIE IAW B767 SRM 51-40-02. - [SDR ABXA040050](https://openairdocs.org/sdr/ABXA040050), Jan 29, 2004: MODULE. LEAKING. CENTER HYDRAULIC QUANTITY DECREASED TO .13, SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ON APPROACH, COMPLETE LOSS OF CENTER HYDRAULICS. FOUND FLAP/SLAT SHUTOFF VA - [SDR ABXA030345](https://openairdocs.org/sdr/ABXA030345), Sep 3, 2003: DUCT. OUT OF ADJUST. MAINTENANCE COULD NOT OPEN R-2 WINDOW. FOUND WINDOW BINDING ON LOWER AC DUCT. ADJUSTED AND SECURED AC DUCT. WINDOW OPENED NORMALLY. - [SDR ABXA030194](https://openairdocs.org/sdr/ABXA030194), Jun 10, 2003: PANEL. GOUGED. DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REM - [SDR ABXA030193](https://openairdocs.org/sdr/ABXA030193), Jun 10, 2003: DOOR FRAME. CORRODED. AFT CARGO DOOR BEAM NR 5, CORROSION WAS FOUND ON THE INNER CHORD P/N 140T2605-3 UNDERNEATH PUMP. AFTER CORROSION REMOVED MINIMUM REMAINING THICKNESS WAS 0.082, - [SDR ABXA030192](https://openairdocs.org/sdr/ABXA030192), Jun 10, 2003: STRUT. GOUGED. DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REM - [SDR ABXA030198](https://openairdocs.org/sdr/ABXA030198), Jun 10, 2003: FRAME. CORRODED. RIGHT STA. 883.5 FRAME SEGMENT P/N 145T1003-2 FAIL SAFE FRAME AT STR. 18 RIGHT WAS FOUND CORRODED. THE ORIGINAL THICKNESS OF FRAME WAS 0.200 INCH AFTER BLENDED - [SDR ABXA030197](https://openairdocs.org/sdr/ABXA030197), Jun 10, 2003: SKIN. GOUGED. CARGO DOOR GOUGE WAS FOUND IN THE PART AT BULK CARGO DOOR INNER SKIN, STA. 1439, WL 131, P/N 146T6334-1, GOUGE ON INNER SKIN. REPAIRED AREA IAW REA MR. - [SDR ABXA030196](https://openairdocs.org/sdr/ABXA030196), Jun 10, 2003: STRINGER. CORRODED. RIGHT HORIZONTAL STAB. LOWER STRINGER NO. 10 LOWER HORZ. FLANGE RBL 56, P/N 181T4110-4, FOUND CORROSION DURING INSPECTION ON STRINGER P/N 181T4110-4 COMMON TO S - [SDR ABXA030195](https://openairdocs.org/sdr/ABXA030195), Jun 10, 2003: FITTING. ELONGATED. DURING INSPECTION, ON LEFT STRUT FORWARD UPPER SPAR FITTING, FOUND FOUR BOLT HOLES SHOULD BE .4375 INCH ARE ALREADY OVERSIZED TO 0.515 INCH AND BACB 30 MT8X ARE - [SDR ABXA030191](https://openairdocs.org/sdr/ABXA030191), Jun 10, 2003: FRAME. DAMAGED. NR 2 ENGINE RIGHT CORE COWL FRAME NAS STA. 304.60 AND NAC WL 73, DAMAGE WAS FOUND ON FRAME P/N 314T1210-333. REPAIRED AREA IAW REA B671-46254MR. - [SDR ABXA030285](https://openairdocs.org/sdr/ABXA030285), Jun 5, 2003: SUPPORT FITTING. DAMAGED. RIGHT WING TRAILING EDGE 113T1647-6 PANEL SUPPORT FITTING ASSEMBLY DAMAGED DOUBLE HOLE AND BLENDED AREA STA 1051 RIGHT BUTTLINE 97.4. REPAIRED AREA IAW REA B657 - [SDR ABXA030184](https://openairdocs.org/sdr/ABXA030184), Mar 16, 2003: WIRE. DAMAGED. APU GENERATOR FEEDER WIRE DAMAGE, CAUSED SHORT CIRCUIT TO GROUND, RESULTING ARCHING TO WIRE AND CLAMP AT STA 1788 RIGHT. REPLACED THE FEEDER WIRE FROM THE NEARB - [SDR ABXA030014](https://openairdocs.org/sdr/ABXA030014), Nov 20, 2002: FLOORBEAM. CORRODED. CABIN RIGHT SIDE STA 287 FLOORBEAM, RBL 73, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM, WL 199.5. PERFORMED FLOORBEAM UPPER CHORD REPAIR IAW SRM 53-00-51, FIG --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.