# N791AX: 1985 Boeing 767-281, registration cancelled 2024-07-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 3, 2024
- Exported to: Democratic Republic of the Congo
- 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: 23141
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 6, 2013
- Certificate issued: December 4, 2012
- Last registry action: July 1, 2023
- Mode S code: AABBD2
- 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/N791AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=791AX
- Page: https://openairdocs.org/deregistered/N791AX-2024-07-03

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 (87, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IXXA20240212005](https://openairdocs.org/sdr/IXXA20240212005), Feb 12, 2024: BATTERY. NO TEST. DURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED EMERGENCY FLASHLIGHT INOPERATIVE. EMERGENCY FLASHLIGHT REMOVED AND REPLACED. OPERATIONAL CHECK GOOD. NO A
- [SDR IXXA20231207001](https://openairdocs.org/sdr/IXXA20231207001), Dec 7, 2023: SKIN. CRACKED. FOUND CRACK IN FWD SKIN ON #1 PYLON DURING EIGINE CHANGE.
- [SDR IXXA20231120083](https://openairdocs.org/sdr/IXXA20231120083), Nov 19, 2023: UNKNOWN. UNKNOWN. #2 FLIGHT DECK EMERGENCY DESCENT DEVICE BLUE GROMET SEAL BROKEN. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM (DMI)-46872 IAW ATI B767 MINIMUM EQUIPMENT LIST 
- [SDR IXXA20231120082](https://openairdocs.org/sdr/IXXA20231120082), Nov 19, 2023: UNKNOWN. UNKNOWN. #1 FLIGHT DECK EMERGENCY DESCENT DEVICE BLUE GROMET SEAL BROKEN. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM (DMI)-46870 IAW ATI B767 MINIMUM EQUIPMENT LIST 
- [SDR IXXA20230802002](https://openairdocs.org/sdr/IXXA20230802002), Jul 6, 2023: UNKNOWN. UNKNOWN. FOUND CRACK ON REPAIR R/H FWD BULKHEAD OUTER CORD FS 1809.5 FROM TOP AS PER SERVICE BULLETIN 767-53A0078 REV G.
- [SDR IXXA20220820126](https://openairdocs.org/sdr/IXXA20220820126), Aug 16, 2022: MEC. FAILED. DESCENDING FROM 11,500 TO 7000 FT, LEFT ENGINE OIL PRESSURE FOLLOWED BY LEFT ENGINE BLEED OFF EICAS MESSAGE. OIL PRESSURE WAS INDICATING 8 PSI EVENTUALLY GOING 
- [SDR IXXA20220612117](https://openairdocs.org/sdr/IXXA20220612117), Jun 9, 2022: EICAS. FAULT MESSAGE. ENROUTE FROM KTPA TO KCVG RIGHT PACK AND TEMP EICAS MESSAGE DISPLAYED. RIGHT PACK INOPERATIVE WITH LEFT PACK ON ACTIVE DEFERRAL. IN COMPLIANCE OF ATI QUICK REFE
- [SDR IXXA20211007052](https://openairdocs.org/sdr/IXXA20211007052), Sep 30, 2021: BULKHEAD. CRACKED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT. IN COMPLIANCE OF TASK CARD ATI-54-812-00-02, MAINTENANCE IDENTIFIED 3 INCH CRACK TO THE #2 PYLON BULK
- [SDR IXXA20211007058](https://openairdocs.org/sdr/IXXA20211007058), Sep 20, 2021: NONE. NONE. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT. MAINTENANCE IDENTIFED #1 ENGINE INBOARD THRUST REVERSER LOWER INNER AIR BYPASS DUCT LOWER FAIRING IS 
- [SDR IXXA20211007062](https://openairdocs.org/sdr/IXXA20211007062), Sep 19, 2021: NONE. CORRODED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT IN COMPLIANCE OF ATI TASK CARD 53-556-00-01 MAINTENANCE IDENTIFIED CORROSION AT AFT LOWER CARGO DOOR C
- [SDR IXXA20211007053](https://openairdocs.org/sdr/IXXA20211007053), Sep 15, 2021: FORMER. CRACKED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT. IN COMPLIANCE OF TASK CARD ATI-57-810-00-01 MAINTENANCE IDENTIFIED CORROSION AND A 1 INCH CRACK ON NO
- [SDR IXXA20211007063](https://openairdocs.org/sdr/IXXA20211007063), Sep 14, 2021: SPLICE. CRACKED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT IN COMPLIANCE OF ATI TASK CARD 53-30-F28C1 MAINTENANCE IDENTIFIED CORROSION FS 436 STR 31L LOWER SURFA
- [SDR IXXA20211007055](https://openairdocs.org/sdr/IXXA20211007055), Sep 12, 2021: NONE. CORRODED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT. IN COMPLIANCE OF TASK CARD ATI-53-556-00-01, IDENTIFIED CORROSION AT AFT LOWER CARGO LOWER DOOR CUTOU
- [SDR IXXA20211007064](https://openairdocs.org/sdr/IXXA20211007064), Sep 10, 2021: SKIN PANEL. DELAMINATED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT MAINTENANCE IDENTIFIED DELAMINATION ON THE UPPER LEFT HORIZONTAL STABILIZER SKIN PANEL LOCATED ON THE 
- [SDR IXXA20211007061](https://openairdocs.org/sdr/IXXA20211007061), Sep 8, 2021: DOOR. GOUGED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT IN COMPLIANCE OF ATI TASK CARD 52-410-00-01 MAINTENANCE IDENTIFIED AFT LOWER CARGO DOOR EXTERNAL SURFA
- [SDR IXXA20211007050](https://openairdocs.org/sdr/IXXA20211007050), Sep 8, 2021: SKATE ANGLE. CHAFED. AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE C CHECK VISIT#2 PYLON FORWARD EDGE OF SKATE ANGLE IS CHAFFED AT 447AR PANEL.CHAFE BEYOND LIMITS IAW BOEING STRUCTURE
- [SDR IXXA20180717031](https://openairdocs.org/sdr/IXXA20180717031), Jul 16, 2018: TRANSMITTER. ERRATIC. ON APPROACH INTO DFW CREW DECLARED AN IFE FOR A TRAILING EDGE FLAP DISAGREE EICAS MSG. LANDING WAS CONTINUED SUCCESSFUL. MAINTENANCE COMPLETED FIM 27-51 FT 809.
- [SDR IXXA20171031323](https://openairdocs.org/sdr/IXXA20171031323), Oct 26, 2017: CABLE. DETERIORATED. ON DESCENT INTO KCVG, LT ENG STUCK AT IDLE AND WOULD NOT ACCELERATE AS COMMANDED. EMERGENCY DECLARED. IN ACCORDANCE WITH ENGINE FAILURE CHECKLIST, COMPLIED WITH
- [SDR IXXA20171031322](https://openairdocs.org/sdr/IXXA20171031322), Oct 26, 2017: BELLCRANK. BROKEN. ON DESCENT INTO DESTINATION STATION KCVG, LT ENG STUCK AT IDLE AND WOULD NOT ACCELERATE AS COMMANDED. EMERGENCY DECLARED. IN ACCORDANCE WITH ENGINE FAILURE CHEC
- [SDR IXXA20170807266](https://openairdocs.org/sdr/IXXA20170807266), Jul 19, 2017: FAILSAFE. CRACKED. IN COMPLIANCE OF TASK CARD S53-050-04-1/AD 2012-09-04, THE FOLLOWING FINDING WERE NOTED, LOWER WHEEL WELL BS 955 FAILSAFE STRAP HAD A CRACK INDICATION AT LOWER 
- [SDR IXXA20170807272](https://openairdocs.org/sdr/IXXA20170807272), Jun 19, 2017: STRUT. CORRODED. NUMBER ONE SLAT INBOARD AUX TRACK ATTACH FITTING INBOARD LOWER STRUT CORRODED AROUND NUTPLATE. REMOVED AND REPLACED STRUT IAW DRAWING 114T2226. AIRCRAFT GROUNDE
- [SDR IXXA20170802256](https://openairdocs.org/sdr/IXXA20170802256), Jun 19, 2017: STRAP. CORRODED. LEFT WING FRONT SPAR LOWER STRAP CORRODED, 7 INCHES OUTBOARD OF PYLON. REMOVED AND REPLACED LOWER STRAP IAW SRM 51-90-02 REA 4727REA04. AIRCRAFT GROUNDED.
- [SDR IXXA20170802264](https://openairdocs.org/sdr/IXXA20170802264), Jun 8, 2017: SPAR WEB. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FRONT SPAR WEB HAS CORROSION AT THE BOTTOM FASTENER ROWS LES 418. REPAIRED CORRODED AREA IAW ENGINEERING 47273REA06.
- [SDR IXXA20170807271](https://openairdocs.org/sdr/IXXA20170807271), Jun 7, 2017: STRAP. CORRODED. THE LEFT WING FRONT SPAR LOWER STRAP CORRODED 7 INCHES OUTBOARD OF PYLON. REMOVED AND REPLACED THE STRAP IAW SRM 51-90-02. AIRCRAFT GROUNDED
- [SDR IXXA20170807270](https://openairdocs.org/sdr/IXXA20170807270), Jun 5, 2017: FRAME. CRACKED. DURING ACCOMPLISHMENT OF EO 53-767-5353 FOUND THE FRAME AT BS 859.5 CRACKED. REPAIRED THE FRAME EO 53-767-5353, REVISION 3. AIRCRAFT GROUNDED
- [SDR IXXA20170802262](https://openairdocs.org/sdr/IXXA20170802262), Jun 5, 2017: FLOOR SUPPORT. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. BULK CARGO FLOOR PANEL ATTACH CHANNEL AT BS 1518, LBL 30 FOUND CRACKED. REMOVED THE DAMAGE. FABRICATED A REPAIR CHANNEL
- [SDR IXXA20170801255](https://openairdocs.org/sdr/IXXA20170801255), Jun 2, 2017: FRAME. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FRAME INNER CHORD AT RIGHT SIDE RBL 89 STA 883.5 CRACKED. FRAME CHORD REPAIRED IAW ENGINEERING ORDER 53-767-5353.
- [SDR IXXA20170802263](https://openairdocs.org/sdr/IXXA20170802263), May 31, 2017: SKIN. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON INBOUND SKIN HAS A CHAFE MARK AT THE UPPER CONTACT POINT WITH THE WING LEADING EDGE. REMOVED AND REPLACED TH
- [SDR IXXA20170802260](https://openairdocs.org/sdr/IXXA20170802260), May 25, 2017: TRACK. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. CORROSION AROUND NUTPLATE ON NR 8 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. REMOVED CORROSION AROUND NUTPLATE ON NR 
- [SDR IXXA201708070268](https://openairdocs.org/sdr/IXXA201708070268), May 24, 2017: SKIN. CRACKED. LEFT FUSELAGE SKIN CRACKED BETWEEN RIVETS BS 1654.5 BETWEEN STRINGERS 4L-5L. REPAIRED THE SKIN. AIRCRAFT GROUNDED.
- [SDR IXXA20170726254](https://openairdocs.org/sdr/IXXA20170726254), May 24, 2017: FRAME. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FRAME INNER CHORD AT RIGHT SIDE STA-859.5 CRACKED. REPAIRED IAW ENGINEERING ORDER 53-767-5353 REVISION 03.
- [SDR IXXA20170802261](https://openairdocs.org/sdr/IXXA20170802261), May 19, 2017: STRINGER. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER 12L CRACKED AT BS 676. SPLICED IN REPLACEMENT SECTION IAW SRM 53-00-03, FIG 201, REPAIR 1 AND SB 368-53-038.
- [SDR IXXA20170802259](https://openairdocs.org/sdr/IXXA20170802259), May 18, 2017: BEAM. CORRODED. VERTICAL PANEL ON WING LEADING EDGE BETWEEN NR 9 SLAT INBOARD AND OUTBOARD AUX TRACKS CORRODED AROUND NUTPLATE AT LES .595. BLENDED CORROSION AND FOUND TO BE OU
- [SDR IXXA20170802258](https://openairdocs.org/sdr/IXXA20170802258), May 11, 2017: SKIN. CRACKED. EXTERNAL SKIN CRACKED AROUND FASTENER HEAD AT BS 1725.5 RIGHT SIDE. REPAIRED THE SKIN IAW SRM 53-80-01. REPAIR 6. ACFT GROUNDED.
- [SDR IXXA20170802257](https://openairdocs.org/sdr/IXXA20170802257), May 10, 2017: TRACK. CORRODED. NUMBER 1 SLAT INBOARD AUX TRACK ATTACH FITTING INBOARD LOWER STRUT CORRODED AROUND NUTPLATE. REMOVED AND REPLACED STRUT IAW B767 DRAWING 114T2226. AIRCRAFT GROU
- [SDR IXXA20160725042](https://openairdocs.org/sdr/IXXA20160725042), Jul 20, 2016: BATTERY PACK. INOPERATIVE. DURING DAILY CHECK, FOUND ALL EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT GROUNDED. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M736. OPS SATISFACTORY IAW AMM
- [SDR IXXA20160725041](https://openairdocs.org/sdr/IXXA20160725041), Jul 20, 2016: BATTERY PACK. INOPERATIVE. DURING DAILY CHECK FOUND ALL EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOPERATIVE. AIRCRAFT GROUNDED. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IN POSITI
- [SDR IXXA20160512025](https://openairdocs.org/sdr/IXXA20160512025), May 12, 2016: BRACKET. CORRODED. CORRODED BRACKETS IN ACCESS PANELS OF APU DOOR ACTUATOR. FOUR CLIPS WERE FABRICATED IAW SRM DIAGRAM 353T0115 REV D. INSTALLED CLIPS IAW SRM 51-40-02. NO FURTHER
- [SDR IXXA20160525038](https://openairdocs.org/sdr/IXXA20160525038), May 10, 2016: BATTERY PACK. DISCHARGED. THREE EMER LAMPS DO NOT ILLUMINATE DURING TEST, INSIDE ENTRYWAY CEILING CTR & TWO LT OVERHEAD FIXTURES.
- [SDR 2016F00059](https://openairdocs.org/sdr/2016F00059), Jan 31, 2016: MECHANISM. MISWIRED. THE LATERAL TRIM ACTUATOR,(PART OF THE ELEVATOR FEEL MECHANISM ASSEMBLY) RUNS THE OPPOSITE OF THE DIRECTION COMMANDED WHEN OPERATED. SDR WAS FILED PER THE REQUE
- [SDR IXXA20151103082](https://openairdocs.org/sdr/IXXA20151103082), Nov 1, 2015: ESCAPE ROPE. DISLODGED. WHILE PERFORMING MX ON EMER DESCENT DEVICE IN NR 1 POSITION, NR 5 DESCENT DEVICE DEPLOYED. REMOVED & INSTALLED EMERGENCY DESCENT DEVICE IAW AMM 25-61-03. NO ADD
- [SDR IXXA20151103081](https://openairdocs.org/sdr/IXXA20151103081), Nov 1, 2015: ESCAPE ROPE. DISLODGED. ONE EACH DESCENT DEVICE DISLODGED FROM HOLDER. DEFERRED MX ITEM INITIATED IAW AMM 25-61-01-01, CAT C. REMOVED & INSTALLED EMER DESCENT DEVICE IAW AMM 25-61-03. 
- [SDR IXXA20151102080](https://openairdocs.org/sdr/IXXA20151102080), Oct 29, 2015: ESCAPE ROPE. DISLODGED. DURING THE LANDING TWO DESCENT DEVICE DISLODGED FROM EMER ESCAPE. R & R TWO DISLODGED & ACTIVATED EMER DESCENT DEVICES IAW AMM 25-61-03. NO ADDITIONAL DEFECTS N
- [SDR IXXA20151102079](https://openairdocs.org/sdr/IXXA20151102079), Oct 29, 2015: ESCAPE ROPE. DISLODGED. DURING LANDING, TWO DESCENT DEVICES DISLODGED FROM EMER ESCAPE. R & R TWO DISLODGED EMER DESCENT DEVICES IAW AMM 25-61-03. NO ADDITIONAL DEFECTS WERE NOTED, ACF
- [SDR IXXA140708ILN020S](https://openairdocs.org/sdr/IXXA140708ILN020S), Jul 18, 2014: STOP FITTING. CORRODED. OUTBOARD AILERON AT GND STOP ON AIRPLANE GND POINT SIDE CORRODED. OTBD AILERON FITTING R & R IAW SRM 51-40-02.
- [SDR IXXA20140718019](https://openairdocs.org/sdr/IXXA20140718019), Jul 18, 2014: BEAM. CRACKED. NUMBER 1 PYLON INBOUND LOWER BEAM INSIDE ACCESS DOOR 437BL IS WORN THROUGH AT FWD END & FASTENER HOLES ARE WORN. NR 1 PYLON INBOUND LOWER BEAM R & R IAW DWG 313
- [SDR IXXA201407017](https://openairdocs.org/sdr/IXXA201407017), Jul 14, 2014: SKIN. CRACKED. UPPER RT SIDE OF FUSELAGE SKIN IS CRACKED AT APPROXIMATELY BS 1654, STRINGER 3 - 5R. DAMAGED AREA WAS R & R IAW SRM 53-80-01 FIG 201.
- [SDR IXXA2014071418](https://openairdocs.org/sdr/IXXA2014071418), Jul 14, 2014: SEAT TRACK. CRACKED. CAPTAIN'S FWD & OTBD SEAT TRACK IS CRACKED. R & R CAPTAIN'S SEAT TRACK IAW AMM 20-11-00.
- [SDR IXXA20140703016](https://openairdocs.org/sdr/IXXA20140703016), Jul 14, 2014: SKIN. CRACKED. NUMBER 1 PYLON SKIN CRACKED AT ACCESS PANEL 436AL AT THE 7 O'CLOCK POSITION. REPAIRED ACCESS PANEL SKIN IAW REA47107REA05.
- [SDR IXXA20140711011](https://openairdocs.org/sdr/IXXA20140711011), Jul 11, 2014: STRUT. CORRODED. NUMBER 9 SLAT OTBD AUX TRACK ATTACH FITTING LOWER INBD STRUT CORRODED AROUND NUTPLATES. IAW SRM 51-40-05 & 51-40-02 LOWER INBD STRUT R & R.

All 87: https://openairdocs.org/deregistered/N791AX-2024-07-03/reports.md

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