# N714AX: Boeing 767-223, registration cancelled 2025-03-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 12, 2025
- Exported to: Uzbekistan
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-223](https://openairdocs.org/model/boeing-767-223) (registry code 1385123)
- 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: 22314
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 13, 2008
- Certificate issued: April 12, 2016
- Last registry action: July 28, 2023
- Mode S code: A98AFF
- 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/N714AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=714AX
- Page: https://openairdocs.org/deregistered/N714AX-2025-03-12

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 767-223: https://openairdocs.org/model/boeing-767-223.md

## Service difficulty reports (61, newest 50)

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

- [SDR IXXA20230313022](https://openairdocs.org/sdr/IXXA20230313022), Mar 13, 2023: UNKNOWN. UNKNOWN. PRE-FLIGHT CREW REPORTED L1 ENTRY DOOR CAME OFF TRACKS. ADJUSTED L1 ENTRY DOOR INTO CORRECT POSITION OF TRACK IAW B767 AMM 52-11-00.
- [SDR IXXA20230221017](https://openairdocs.org/sdr/IXXA20230221017), Feb 18, 2023: NONE. NONE. CENTER HYDRAULIC PRESSURE EICAS ON APPROACH. QUANTITY IN CENTER REACHED 0.08. ALTERNATE FLAP AND GEAR EXTENSION ENGAGED. HYDRAULIC QTY WAS FULL AT TOP OF DESCEN
- [SDR IXXA20230211016](https://openairdocs.org/sdr/IXXA20230211016), Feb 11, 2023: FLASHLIGHT. INOPERATIVE. FOUND COCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW B767 AMM 25-05-03. OPERATIONAL CHECK GOOD.
- [SDR IXXA20221101143](https://openairdocs.org/sdr/IXXA20221101143), Oct 28, 2022: PUMP. DAMAGED. DESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGE
- [SDR IXXA2022050501](https://openairdocs.org/sdr/IXXA2022050501), May 5, 2022: VENT. CRACKED. CORE COWL VENT CRACKED
- [SDR IXXA2022050408](https://openairdocs.org/sdr/IXXA2022050408), May 4, 2022: THRUST REVERSER. CHAFED. #2 ENGINE OUTBD THRUST REVERSER HAS A GOUGE AT THE 12 O'CLOCK POSITION
- [SDR IXXA202205040008](https://openairdocs.org/sdr/IXXA202205040008), May 4, 2022: SUPPORT ANGLE. CRACKED. #6 SLAT LOWER EDGE HAS A CRACKED SUPPORT ANGLE. LOCATED BETWEEN THE CENTER AND THE OUTBD AUX TRACK
- [SDR IXXA2022050407](https://openairdocs.org/sdr/IXXA2022050407), May 4, 2022: THRUST REVERSER. GOUGED. THRUST REVERSER HAS GOUGE ON INTERNAL FAIRING
- [SDR IXXA2022050406](https://openairdocs.org/sdr/IXXA2022050406), May 4, 2022: COWL LATCH. WORN. CORE COWL AFT LATCH HAS WEAR
- [SDR IXXA2022050405](https://openairdocs.org/sdr/IXXA2022050405), May 4, 2022: THRUST REVERSER. BENT. THRUST REVERSER TRAILING EDGE BENT
- [SDR IXXA2022050403](https://openairdocs.org/sdr/IXXA2022050403), May 4, 2022: BRACKET. CRACKED. BRACKET CRACKED ON SKIRT FAIRING
- [SDR IXXA2022050402](https://openairdocs.org/sdr/IXXA2022050402), May 4, 2022: THRUST REVERSER. CRACKED. THRUST REVERSER TRAILING EDGE CRACKED
- [SDR IXXA2022050304](https://openairdocs.org/sdr/IXXA2022050304), May 3, 2022: SLEEVE. DETERIORATED. #1 ENGINE EXHAUST SLEEVE LEADING EDGE WEAR COATING CHIPPED AND DETERIORATED.
- [SDR IXXA2022050303](https://openairdocs.org/sdr/IXXA2022050303), May 3, 2022: SLEEVE. WORN. #1 ENGINE EXHAUST SLEEVE HAS A HOLE WORN ON THE LEADING EDGE AT 7 O'CLOCK POSITION
- [SDR IXXA2022050302](https://openairdocs.org/sdr/IXXA2022050302), May 3, 2022: COWLING. CHAFED. LOWER CLOSE OUT CHANNEL CHAFED IN MULTI AREAS WHERE STOP PADS MATE UP ON #1 ENGINE O/B CORE COWL LOWER END
- [SDR IXXA2022050301](https://openairdocs.org/sdr/IXXA2022050301), May 3, 2022: NONE. CRACKED. #1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKED
- [SDR IXXA2022043001](https://openairdocs.org/sdr/IXXA2022043001), Apr 30, 2022: TORQUE TUBE. CORRODED. RH FLAP IB TORQUE TUBE PITTED
- [SDR IXXA20220427002](https://openairdocs.org/sdr/IXXA20220427002), Apr 27, 2022: PANEL. CORRODED. ALC PANEL SUPPORT ON BILGE PANEL RBL16 AT STATION 1281 CORRODED
- [SDR IXXA2022042201](https://openairdocs.org/sdr/IXXA2022042201), Apr 22, 2022: FLOOR PANEL. CRACKED. FLOOR PANEL 122C CRACKED
- [SDR IXXA2022041502](https://openairdocs.org/sdr/IXXA2022041502), Apr 15, 2022: SEAL BRACKET. CRACKED. FAN COWL SEAL RETAINER BRACKET CRACKED
- [SDR IXXA202204290002](https://openairdocs.org/sdr/IXXA202204290002), Apr 14, 2022: BEAM. CORRODED. R/W TRAILING EDGE FLAP #8 SUPPORT 1-2-3 BEAM HAS TWO FASTENERS COMMON TO THE SIDE BRACE ATTACH FITTING WITH DEFECT INDICATION WITH HFEC HOLE SCAN
- [SDR IXXA2022050502](https://openairdocs.org/sdr/IXXA2022050502), Apr 12, 2022: SUPPORT BRACKET. CORRODED. L/H BILGE PANEL SUPPORT BRACKET (L-2) AT STA 1270 CORRODED
- [SDR IXXA2022050305](https://openairdocs.org/sdr/IXXA2022050305), Apr 11, 2022: TORQUE TUBE. WORN. L/H I/B FLAP #4 TORQUE TUBE FOUND PITTED AND WORN BEYOND LIMITS
- [SDR IXXA2022042801](https://openairdocs.org/sdr/IXXA2022042801), Apr 11, 2022: TORQUE TUBE. WORN. RH I/B FLAP TORQUE TUBE REQUIRES REMOVAL FOR INSPECTION IAW J/C ATI-57-793-12-02 #5 TORQUE TUBE FOUND TO BE PITTED AND WORN
- [SDR IXXA2022050201](https://openairdocs.org/sdr/IXXA2022050201), Apr 8, 2022: RETAINER SEAL. CRACKED. I/B FLAP FAIRING 671FB INSIDE O/B SEAL RETAINER CRACKED
- [SDR IXXA20210522038](https://openairdocs.org/sdr/IXXA20210522038), May 17, 2021: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGANCY EXIT SIGN LIGHTS INOPERATIVE. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED BATTERY PACK IAW BOEING 767 AMM 33-51-07. O
- [SDR IXXA20210405014](https://openairdocs.org/sdr/IXXA20210405014), Apr 2, 2021: CONNECTOR. DAMAGED. DURING SERVICE CHECK, FOUND LEFT ENTRY DOOR EXIT SIGN LIGHT NOT ON WITH FLIGHT DECK EMERGENCY LIGHT SWITCH IN THE ON POSITION. TROUBLESHOT IAW B767 IAI WDM 33-5
- [SDR IXXA20201202444](https://openairdocs.org/sdr/IXXA20201202444), Nov 29, 2020: WARNING MESSAGE. ILLUMINATED. PRE-DEPARTURE: CREW REPORTS L1 DOOR INDICATION AFTER ENGINE START. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE, WORK IN PROGRESS.
- [SDR IXXA20200519010](https://openairdocs.org/sdr/IXXA20200519010), May 5, 2020: MOUNT BRACKET. GOUGED. AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-54-408-00-02 " GVI - EXTERNAL - NO. 2 NACELLE STRUT" LEFT AFT PRECOOLER MOUNT BRACKET CRACKED V
- [SDR ABXR2020050600026](https://openairdocs.org/sdr/ABXR2020050600026), May 5, 2020: BRACKET. CRACKED. L/H AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 L/H CORE COWL. REMOVED AND REPLACED L/H AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02 PARA 9 AND I
- [SDR ABXR2020050600027](https://openairdocs.org/sdr/ABXR2020050600027), Apr 27, 2020: TEE FITTING. CORRODED. CORROSION ON INTERIOR "T" SECTION OF ALC DOOR 10" FROM AFT EDGE, 24" FROM TOP EDGE.REMOVED AND REPLACED INTERIOR "T" SECTION OF ALC 3RD FROM TOP USING 140T2604-
- [SDR IXXA20200519015](https://openairdocs.org/sdr/IXXA20200519015), Apr 24, 2020: FLOOR SUPPORT. CORRODED. AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-572-00-01 "GVI - INTERNAL - BULK CARGO COMPARTMENT BULK FLOOR SUPPORT" F.S. 1417 HAS CORROSIO
- [SDR IXXA20200519012](https://openairdocs.org/sdr/IXXA20200519012), Apr 24, 2020: SKIN. CORRODED. AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-073-00-01, ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS. REPLACED
- [SDR ABXR2020050600028](https://openairdocs.org/sdr/ABXR2020050600028), Apr 24, 2020: WEB. CORRODED. ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS.REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02
- [SDR IXXA20200519014](https://openairdocs.org/sdr/IXXA20200519014), Apr 22, 2020: SKIN. CRACKED. AIRCRAGT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-53-730-00-02 "GVI - EXTERNAL - EXTERIOR SECTION 48 - RIGHT SIDE", THE FOLLOWING FINDINGS WERE N
- [SDR IXXA20200519013](https://openairdocs.org/sdr/IXXA20200519013), Apr 22, 2020: WEB. BROKEN. AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-105-00-01 "DET - FORWARD NACELLE STRUT FAIRING - NACELLE 2 (EZAP)" THE FOLLOWING FINDINGS WE
- [SDR ABXR2020050600030](https://openairdocs.org/sdr/ABXR2020050600030), Apr 22, 2020: STRINGER SPLICE. CORRODED. STRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.
- [SDR ABXR2020050600029](https://openairdocs.org/sdr/ABXR2020050600029), Apr 22, 2020: WEB. CRACKED. NUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM
- [SDR ABXR2020050600031](https://openairdocs.org/sdr/ABXR2020050600031), Apr 17, 2020: SKIN. CRACKED. AFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S
- [SDR IXXA20200519017](https://openairdocs.org/sdr/IXXA20200519017), Apr 15, 2020: STRINGER. CORRODED. AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-454-00-01, "GVI - INTERNAL - BULK CARGO COMPARTMENT" THE FOLLOWING FINDINGS WERE NOTED: FLC -
- [SDR IXXA20200519016](https://openairdocs.org/sdr/IXXA20200519016), Apr 15, 2020: STRINGER. CORRODED. AIRCRAFT GROUNDED FOR CHECK-C-24.IN COMPLIANCE OF TASK CARD ATI-53-454-00-01,"GVI - INTERNAL - BULK CARGO COMPARTMENT" FLC - CORROSION ON STRINGER 31R AT STA.41
- [SDR IXXA20200519009](https://openairdocs.org/sdr/IXXA20200519009), Apr 14, 2020: SLAT. BULGED. AIRCRAFT GROUNDED FOR C-CHECK 24. IN COMPLIANCE OF TASK CARD ATI-57-806-00-02, "GVI - ZONAL - INBOARD SLAT NO. 7" THE FOLLOWING FINDINGS WERE NOTED: 7 SLAT - LO
- [SDR ABXR2020050600025](https://openairdocs.org/sdr/ABXR2020050600025), Apr 14, 2020: SLAT. CORRODED. NUMBER 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.REPAIRED #7 SLAT LOWER LEADING EDGE IAW REA# 47404REA02
- [SDR IXXA20180515023](https://openairdocs.org/sdr/IXXA20180515023), Apr 11, 2018: FAILSAFE. CRACKED. RIGHT WING FAILSAFE STRAP AT WS 955, REAMED HOLES IAW SRM 51-40-02. LOWER HOLE DAMAGE EXTENDED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED IAW 47317REA01.
- [SDR IXXA20180515022](https://openairdocs.org/sdr/IXXA20180515022), Apr 6, 2018: BULKHEAD. DENTED. AFT PRESSURE BULKHEAD WAS FOUND DENTED. REPAIRED THE BULKHEAD IAW REA 47317, REA 05, REV IR.
- [SDR IXXA20180515021](https://openairdocs.org/sdr/IXXA20180515021), Apr 6, 2018: SKIN. BULGED. BULGING FUSELAGE SKIN BS 462, STRINGER 23R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01, REPAIR 1.
- [SDR IXXA20180515020](https://openairdocs.org/sdr/IXXA20180515020), Apr 2, 2018: SEAT TRACK. CRACKED. FIRST OFFICER'S RIGHT FORWARD SEAT TRACK WAS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW IAW AMM 25-11-01-822-095-001
- [SDR IXXA20180515019](https://openairdocs.org/sdr/IXXA20180515019), Mar 30, 2018: FAILSAFE. CRACKED. LT FAILSAFE STRAP LOWER HOLE COMMON TO THE TEE FITTING CRACKED. THE FAILSAFE WAS REPAIRED.
- [SDR IXXA20170726253](https://openairdocs.org/sdr/IXXA20170726253), Jul 13, 2017: ESCAPE REEL. FAILED. EMERGENCY DESCENT DEVICE NUMBER 5 PARTIALLY EXTENDED. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW MMS 25-61-03. AIRCRAFT RELEASED TO SERVICE.
- [SDR IXXA20170726252](https://openairdocs.org/sdr/IXXA20170726252), Jul 13, 2017: ESCAPE REEL. INOPERATIVE. EMERGENCY DESCENT DEVICE NUMBER 7 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW 25-61-03. ACFT RELEASED TO SE

All 61: https://openairdocs.org/deregistered/N714AX-2025-03-12/reports.md

---
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.