# N788AX: 1984 Boeing 767-281, registration cancelled 2018-11-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 15, 2018
- Exported to: Poland
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-281](https://openairdocs.org/model/boeing-767-281) (registry code 1385129)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 23021
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 19, 2011
- Certificate issued: October 18, 2010
- Last registry action: May 17, 2016
- Mode S code: AAAE54
- 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/N788AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=788AX
- Page: https://openairdocs.org/deregistered/N788AX-2018-11-15

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 (76, newest 50)

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

- [SDR ABXA201811263126](https://openairdocs.org/sdr/ABXA201811263126), Oct 23, 2018: SKIN. DENTED. DENT ON #12 SLAT (RIGHT WING) UPPER SKIN AT OUTBOARD SLAT STATION 992. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2018112623123](https://openairdocs.org/sdr/ABXA2018112623123), Oct 23, 2018: FAILSAFE. CORRODED. CORROSION ON FORWARD LOWER CARGO DOOR INNER SILL FAIL SAFE STRAP. REPLACED FAIL SAFE STRAP. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811263122](https://openairdocs.org/sdr/ABXA201811263122), Oct 23, 2018: DOOR FRAME. CRACKED. CRACK IN THE FRAME OF THE LOWER AFT CORNER OF THE L1 DOOR. THE FRAME WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811263121](https://openairdocs.org/sdr/ABXA201811263121), Oct 23, 2018: BEAM. CORRODED. CORROSION ON THE RIGHT HORIZONTAL STABILIZER FIXED TRAILING EDGE BEAM UPPER CHORD BETWEEN ELEVATOR STATIONS 237 AND 261. THE CHORD WAS REPAIRED. THE AIRPLANE WA
- [SDR ABXA201811263120](https://openairdocs.org/sdr/ABXA201811263120), Oct 23, 2018: SPAR. CORRODED. CORROSION ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD BETWEEN REAR SPAR STATIONS 200 AND 226.6. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213119](https://openairdocs.org/sdr/ABXA201811213119), Oct 23, 2018: FITTING. CHAFED. CHAFE ON #1 PYLON INBOARD SIDE LOAD FITTING AT NACELLE STATION 302. THE WEAR AREA MEASURED 3.60” LONG X 0.150” WIDE X 0.043” DEEP (ENTIRE LENGTH). THE FITTING W
- [SDR ABXA201811213118](https://openairdocs.org/sdr/ABXA201811213118), Oct 23, 2018: ANGLE. CRACKED. CHAFE AND CRACK ON #1 PYLON INBOARD HYDRAULIC BAY LOWER BEAM ZEE ANGLE. THE ZEE ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2018112103117](https://openairdocs.org/sdr/ABXA2018112103117), Oct 23, 2018: SKIN. DENTED. DENT ON #12 SLAT ON TOP SKIN. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213116](https://openairdocs.org/sdr/ABXA201811213116), Oct 23, 2018: ATTACH FITTING. CORRODED. CORROSION ON LEFT WING TRAILING EDGE LOWER PANEL ATTACH CHORD. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213115](https://openairdocs.org/sdr/ABXA201811213115), Oct 23, 2018: ATTACH FITTING. CORRODED. CORROSION ON RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH CHORD AT WING STATION 433. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213114](https://openairdocs.org/sdr/ABXA201811213114), Oct 23, 2018: ATTACH FITTING. CORRODED. CORROSION ON LEFT WING LEADING EDGE LOWER PANEL ATTACH STRUCTURE. REPLACED WEB. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213113](https://openairdocs.org/sdr/ABXA201811213113), Oct 23, 2018: RIB. CORRODED. CORROSION ON THE #4 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. THE AIRLOAD RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213112](https://openairdocs.org/sdr/ABXA201811213112), Oct 23, 2018: SPAR. CORRODED. CORROSION ON THE LEFT WING LEADING EDGE FRONT SPAR AT LEADING EDGE STATION 867. THE FRONT SPAR'S WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213111](https://openairdocs.org/sdr/ABXA201811213111), Oct 23, 2018: RIB. CORRODED. CORROSION ON #2 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213110](https://openairdocs.org/sdr/ABXA201811213110), Oct 23, 2018: RIB. CORRODED. CORROSION ON #1 SLAT INBOARD AUX TRACK INBOARD LOWER STRUT. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213108](https://openairdocs.org/sdr/ABXA201811213108), Oct 23, 2018: CIRCUIT BREAKER. FAILED. EXCESSIVE HEAT AT C10 CIRCUIT BREAKER "C BUS PWR" INSIDE P6-2 PANEL. REPLACED CIRCUIT BREAKER C884 AND WIRE W1032-004-6. THE AIRPLANE WAS GROUNDED. THE CAUSE OF
- [SDR ABXA201811213107](https://openairdocs.org/sdr/ABXA201811213107), Oct 23, 2018: STRUCTURE. CORRODED. CORROSION ON LOWER FLANGE ON RIGHT HORIZONTAL STABILIZER CHORD 17. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213106](https://openairdocs.org/sdr/ABXA201811213106), Oct 23, 2018: STRUT. CORRODED. CORROSION ON LOWER STRUT ON AIRLOAD RIB ON RIGHT WING. THE STRUT WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213104](https://openairdocs.org/sdr/ABXA201811213104), Oct 23, 2018: DOUBLER. CORRODED. CORROSION ON DOUBLER FORWARD OF THE OUTBOARD AILERON ON THE LEFT WING. THE DOUBLER WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201811213105](https://openairdocs.org/sdr/ABXA201811213105), Oct 23, 2018: STIFFENER. CRACKED. CRACK IN THE MAIN DECK CARGO FLOOR BEAM VERTICAL STIFFENER AT FUSELAGE STATION 266.5. THE STIFFENER WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA2018072713078](https://openairdocs.org/sdr/ABXA2018072713078), Jul 13, 2018: SKIN PANEL. CHAFED. CHAFE DAMAGE TO THE LOWER WING SKIN PANEL # 1 (P/N: 111T4015-4) AND LOWER CENTER WING BEAM (LBL 62.05) WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWE
- [SDR ABXA201807132076](https://openairdocs.org/sdr/ABXA201807132076), Jul 12, 2018: BEAM. CHAFED. CHAFING AT BODY STATION 900, LBL 57 ON THE LOWER WING SKIN PANEL (P/N: 111T4015-4) AND LOWER CENTER WING BEAM WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21),
- [SDR ABXA20171205145](https://openairdocs.org/sdr/ABXA20171205145), Dec 5, 2017: ESCAPE REEL. MISSING. ONE EMERGENCY DESCENT SAFETY HARNESS WAS MISSING FROM ITS STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), A NEW SAFETY HARNESS WAS INSTAL
- [SDR ABXA20170624071](https://openairdocs.org/sdr/ABXA20170624071), Jun 24, 2017: UNKNOWN. ODOR. WHILE THE LEFT ENGINE WAS IN OPERATION, THE LEFT PRESSURE REGULATING SHUTOFF VALVE WAS CLOSED. A STRONG ODOR WAS ASSOCIATED WITH IT. THE AIRPLANE WAS REMOVED FR
- [SDR ABXA2016216004](https://openairdocs.org/sdr/ABXA2016216004), Feb 16, 2016: COUPLING. FAILED. WITH THE EQUIPMENT COOLING SWITCH IN OVRD POSITION & BOTH PACKS OPERATING AT 39,000 FEET, THE CABIN ALTITUDE CLIMBED TO 11,000 FEET. THE FLIGHT CREW DESCENDED T
- [SDR ABXA20150502068](https://openairdocs.org/sdr/ABXA20150502068), May 1, 2015: MEC. FAULTY. ADVANCED THRUST LEVER APPROX HALF WAY FOR TAKEOFF ON LT ENG & ENG WOULD NOT ACCELERATE. REPLACED LT ENG MAIN ENG CONTROL.
- [SDR ABXA20150227017](https://openairdocs.org/sdr/ABXA20150227017), Feb 27, 2015: SMOKE DETECTOR. FALSE ACTIVATION. LAVATORY SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. REPLACED LAVATORY SMOKE DETECTOR.
- [SDR ABXA20150224031](https://openairdocs.org/sdr/ABXA20150224031), Feb 24, 2015: BEAM. CORRODED. DURING OK TO CLOSE OF LE PANELS FOUND CORROSION ON NUT STRIP ON FIXED LE AT APPROX LES 590. FOUND CORROSION TO BE ON NOSE BEAM WEB COMMON TO NUTPLATES. REMOVED 
- [SDR ABXA20150224029](https://openairdocs.org/sdr/ABXA20150224029), Feb 24, 2015: BEAM. CORRODED. LEFT HORIZONTAL STABILIZER UPPER REAR BEAM HAS AREAS OF CORROSION FROM ELEVATOR STATION 49 - 302. OUT OF LIMITS AREA ELEVATOR STATION 146 - 150.5. REPAIRED IAW 
- [SDR ABXA20150224020](https://openairdocs.org/sdr/ABXA20150224020), Feb 24, 2015: ANGLE. CRACKED. VERTICAL STABILIZER TO SKIN ANGLE LT OTBD END CRACKED, ACCESS THROUGH PANEL 324AL. REMOVED ANGLE, FABRICATED NEW ANGLE IAW DWG 173T1302 FROM 2024-T3 .040. PERFO
- [SDR ABXA20150222028](https://openairdocs.org/sdr/ABXA20150222028), Feb 22, 2015: RIB. CORRODED. RIGHT WING TE LOWER CHORD OF SUPPORT RIB AT WS 1080 IS CORRODED & SPLIT. R & R RT WING TE LOWER CHORD OF SUPPORT RIB WS 1080 IAW SRM 51-40-02 & DOC 113T1521 REV
- [SDR ABXA20150221026](https://openairdocs.org/sdr/ABXA20150221026), Feb 21, 2015: SPAR. CORRODED. LEFT HORIZONTAL STABILIZER REAR SPAR & TE BEAM ARE CORRODED AT ELEVATOR STATION 325. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR SPAR UPPER CHO
- [SDR ABXA20150221025](https://openairdocs.org/sdr/ABXA20150221025), Feb 21, 2015: SPAR. CORRODED. LEFT HORIZONTAL STABILIZER REAR SPAR IS CORRODED AT ELEVATOR STATION 139 - 143. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR UPPER CHORD ELEVATO
- [SDR ABXA20150221022](https://openairdocs.org/sdr/ABXA20150221022), Feb 21, 2015: RIB. CORRODED. LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 91 UPPER CHORD OF THE TE RIB IS CORRODED. R & R CHORD PN 183T1400-5 IAW SRM 51-40-02. SDR INFO, PN 183T1400-5, PART
- [SDR ABXA20150220027](https://openairdocs.org/sdr/ABXA20150220027), Feb 20, 2015: STRUCTURE. CRACKED. EA 53500009-001 NEEDS ACCOMPLISHED. REPAIRED DAMAGED CHORD RT STATION 883.5 STRINGER 18R IAW SRM 53-50-07 REPAIR 1. SDR INFO CRACKED 0.250", PN 145T8000-1, SN N
- [SDR ABXA20150220023](https://openairdocs.org/sdr/ABXA20150220023), Feb 20, 2015: RIB. CORRODED. LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IS CORRODED. INSTALLED NEW LT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD
- [SDR ABXA20150220021](https://openairdocs.org/sdr/ABXA20150220021), Feb 20, 2015: KEELBEAM. CORRODED. RIGHT KEEL BEAM LOWER INBD FLANGE LOWER SURFACE CORROSION FS 998 - 1007. REPAIRED RT KEEL BEAM IAW REA B653-61424-MR. SDR INFO, CRACKED, CORRODED L2, PN 145T861
- [SDR ABXA20150219030](https://openairdocs.org/sdr/ABXA20150219030), Feb 19, 2015: BEAM. CORRODED. CORROSION FOUND ON FIXED LE STRUCTURE AT APPROX LE STATION 894 AT SCREW HOLE. REMOVED NOSE BEAM WEB ASSEMBLY, FABRICATED NEW WEB & REINSTALLED ASSEMBLY WITH NEW
- [SDR ABXA20150219024](https://openairdocs.org/sdr/ABXA20150219024), Feb 19, 2015: RIB. CORRODED. LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 325 UPPER CHORD OF THE TE RIB IS CORRODED. REPLACED UPPER T CHORD FITTING ON LT HORIZONTAL STATION 325. PN 183T1530
- [SDR ABXA20150217019](https://openairdocs.org/sdr/ABXA20150217019), Feb 17, 2015: BEAM. CORRODED. HYDRAULIC LINE SUPPORT CLIP OTBD & AFT OF TOP OF LG CORRODED ON TE SUPPORT. REMOVED CLIP, FOUND BEAM TO BE CORRODED. REPLACED BEAM, REINSTALLED CLIP IAW SRM 51-
- [SDR ABXA20150217018](https://openairdocs.org/sdr/ABXA20150217018), Feb 17, 2015: ANGLE. CORRODED. LEFT FWD KEEL BEAM FWD STATION 977, LBL 2 CORROSION FOUND, MARKED WITH NR. FOUND ANGLE AT STATION 977, LBL 2 TO BE CORRODED BEYOND LIMITS IAW SRM 53-50-12 FIG 1
- [SDR ABXA20150209005](https://openairdocs.org/sdr/ABXA20150209005), Feb 9, 2015: BEAM. CORRODED. CORROSION AROUND NUTPLATE AT APPROX LES 620. R & R WEB IAW SRM 51-40-02. SDR INFO, CORRODED, PN 114T2300-225, SN N/A, PART NAME NOSE BEAM. ACFT WAS GNDED.
- [SDR ABXA20150206006](https://openairdocs.org/sdr/ABXA20150206006), Feb 6, 2015: SPAR. CORRODED. CORROSION AROUND NUTPLATES ON REAR SPAR TO TE BEAM UPPER CHORD AT WS 433 NEAR TE. R & R UPPER CHORD WS 433 REAR SPAR TO TE IAW SRM 51-40-02. SDR INFO, CORRODED 
- [SDR ABXA2014041046](https://openairdocs.org/sdr/ABXA2014041046), Apr 8, 2014: UNKNOWN. FUMES. ON TOP OF DESCENT, THE FLIGHT CREW COULD SMELL ELEC FUMES. COMPLIED WITH SMOKE, FIRE, & FUMES CHECKLIST & FUMES CEASED. INSPECTED THE MAIN EQUIPMENT CTR, FWD EQ
- [SDR ABXA20130516434](https://openairdocs.org/sdr/ABXA20130516434), May 16, 2013: ANGLE. DAMAGED. FUSELAGE SKIN AT LT HORIZONTAL ANGLE, BS 1809, S12L HAS DEFECT INDICATION IN LOWER FWD FASTENER OF INSPECTED AREA 1 IAW NDTM PART 6, FIG 1. FASTENER OBLONG, REA
- [SDR ABXA20130514436](https://openairdocs.org/sdr/ABXA20130514436), May 14, 2013: SKIN. CORRODED. RIGHT SIDE EMERGENCY EXIT DOOR CUTOUT FOUND WITH CORROSION IN THE FORWARD LOWER CORNER AREA APPROX. 2" LONG. REMOVED CORROSION IN RT SIDE EMERENCY EXIT CUTOUT F
- [SDR ABXA20130506432](https://openairdocs.org/sdr/ABXA20130506432), May 6, 2013: MOUNT. CORRODED. NR 2 ENGINE AFT MOUNT HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED ENGINE MOUNT IAW B767 MM CH 71-21-02-4, ACFT WAS GROUNDED.
- [SDR ABXA20130503435](https://openairdocs.org/sdr/ABXA20130503435), May 3, 2013: STIFFENER. CORRODED. STIFFENER BETWEEN KEELBEAM PANELS CORRODED ON BOTH ENDS, STIFFENER CORRODED BEYOND LIMITS, R & R IAW SRM 51-40-02, PARA 4B AND 51-40-0, ACFT WAS GROUNDED.
- [SDR ABXA20130501433](https://openairdocs.org/sdr/ABXA20130501433), May 1, 2013: MOUNT. CORRODED. NR 1 ENGINE AFT ENGINE MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED AFT ENGINE MOUNT IAW B767 AMM 71-21-02-4, ACFT WAS GROUNDED.
- [SDR ABXA20121129311](https://openairdocs.org/sdr/ABXA20121129311), Nov 29, 2012: INERTIA REEL. UNSECURE. EMERGENCY ESCAPE DEVICE (INTERTIAL REEL) FELL OUT OF HOLDER DURING FLIGHT. REPLACED DESCENT DEVICES IN SUPERNUMERARY COMPARTMENT CONTAINER AT POS 7 IAW AMM 25-6

All 76: https://openairdocs.org/deregistered/N788AX-2018-11-15/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.