# N775AX: Boeing 767-281, registration cancelled 2024-04-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 9, 2024
- 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: 22790
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 4, 2010
- Certificate issued: July 14, 2023
- Last registry action: July 14, 2023
- Mode S code: AA7BB0
- 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/N775AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=775AX
- Page: https://openairdocs.org/deregistered/N775AX-2024-04-09

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 (82, newest 50)

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

- [SDR ABXA20170705082](https://openairdocs.org/sdr/ABXA20170705082), Jul 5, 2017: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AT BS 720 STRINGES 37-38L. THE SHEAR TIE WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170705081](https://openairdocs.org/sdr/ABXA20170705081), Jul 5, 2017: FLOORBEAM. CORRODED. CORROSION AROUND THE NUTPLATES AND NUTCLIP HOLES ON THE UPPER TEE OF THE FORWARD LOWER CARGO COMPARTMENT FLOOR BEAM AT BS 742. THE TEE WAS REPLACED. AIRPLANE WA
- [SDR ABXA20170705080](https://openairdocs.org/sdr/ABXA20170705080), Jul 5, 2017: STRUCTURE. CORRODED. CORROSION ON UPPER STRUCTURE AT BS 1373 IN THE AFT LOWER CARGO COMPARTMENT. THE STRUCTURE WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170705079](https://openairdocs.org/sdr/ABXA20170705079), Jul 5, 2017: BRACKET. CRACKED. CRACKED BRACKET AT THE UPPER AFT SECTION OF THE FORWARD LOWER CARGO DOOR CUTOUT. THE BRACKET WAS REPLACED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170705078](https://openairdocs.org/sdr/ABXA20170705078), Jul 5, 2017: SKIN. CORRODED. CORROSION ON LEFT WING LEADING EDGE UPPER SPLICE PLATE AT LEADING EDGE LWS 456. THE SPLICE PLATE WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705077](https://openairdocs.org/sdr/ABXA20170705077), Jul 5, 2017: RIB. CORRODED. CORROSION ON LOWER AIR LOAD RIB AT LEFT WING LEADING EDGE STATION 938. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705076](https://openairdocs.org/sdr/ABXA20170705076), Jul 5, 2017: SKIN. CORRODED. CORROSION ON LOWER SIDE OF UPPER SKIN AT LT WS 410 TO 424. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170705075](https://openairdocs.org/sdr/ABXA20170705075), Jul 5, 2017: BRACKET. CRACKED. CRACK IN TWO AFT ATTACH ANGLES FOR THE LOWER LONGITUDINAL BEAMS AT THE AFT SPAR IN THE CENTER TANK. ONE BRACKET WAS CRACKED 4.25 INCHES, THE OTHER WAS CRACKED 2
- [SDR ABXA20170705074](https://openairdocs.org/sdr/ABXA20170705074), Jul 5, 2017: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AROUND A FASTENER AT BS 1678. SKIN WAS REPAIRED. ACFT WAS GROUNDED.
- [SDR ABXA20170705073](https://openairdocs.org/sdr/ABXA20170705073), Jul 5, 2017: SKIN. DENTED. DENT IN FUSELAGE SKIN BS 325-347. THE FUSELAGE SKIN WAS REPAIRED. THE ACFT WAS GROUNDED.
- [SDR ABXA20170114002](https://openairdocs.org/sdr/ABXA20170114002), Jan 14, 2017: BOLT. MISSING. LEFT ENGINE FLAME OUT (SHUT DOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 10,000 FEET. THE QUICK REFERENCE HANDBOOK’S ENGINE FAILURE AND ENGINE IN FLIGH
- [SDR ABXA20160916146](https://openairdocs.org/sdr/ABXA20160916146), Sep 16, 2016: ESCAPE REEL. UNWANTED DEPLOY. WHILE PERFORMING INSPECTION OF THE DESCENT DEVICES, TWO DESCENT DEVICES FELL TO THE FLOOR, BREAKING THE SEALS. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) 
- [SDR ABXA20160812141](https://openairdocs.org/sdr/ABXA20160812141), Aug 12, 2016: ESCAPE ROPE. INOPERATIVE. ONE DESCENT DEVICE WAS FOUND NOT PROPERLY STOWED AND INOPERATIVE DURING THE FLIGHT CREW’S PRE-FLIGHT INSPECTION. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED
- [SDR ABXA20160331048](https://openairdocs.org/sdr/ABXA20160331048), Mar 31, 2016: TEE FITTING. CORRODED. LEFT T FITTING IS CORRODED AT THE FWD BOLT HOLES. MATCH DRILLED THE NEW T FITTING IAW SRM 51-40-05. T FITTING TO BE INSTALLED ON JC DOCUMENT 47008ORD03. CORRODE
- [SDR ABXA20160331047](https://openairdocs.org/sdr/ABXA20160331047), Mar 31, 2016: TEE FITTING. CORRODED. RIGHT T FITTING IS CORRODED AT THE FWD BOLT HOLES. NEW T FITTING DRILLED IAW SRM 57-40-05. NEW T FITTING TO BE INSTALLED ON DOCUMENT 47008ORD04. CORRODED LEVEL 
- [SDR ABXA20160324049](https://openairdocs.org/sdr/ABXA20160324049), Mar 24, 2016: FAILSAFE. CRACKED. LEFT WW FAILSAFE STRAP AT STATION 955 IS CRACKED AT LOWER FASTENER HOLE. REFERENCE DOCUMENT 47008ORD01 STEP 21. PERFORMED CUT OUT OF CRACKED FAILSAFE IAW DOCUME
- [SDR ABXA20160323046](https://openairdocs.org/sdr/ABXA20160323046), Mar 23, 2016: FAILSAFE. CRACKED. RIGHT WW FAILSAFE STRAP AT STATION 955, IS CRACKED AT LOWER FASTENER HOLE. REFERENCE DOCUMENT 47008ORD02 STEP 21. PERFORMED CUT OUT OF FAILSAFE IAW DOC 47008ORD
- [SDR ABXA20150527067](https://openairdocs.org/sdr/ABXA20150527067), May 27, 2015: SMOKE DETECTOR. FALSE ACTIVATION. SERVICE AREA SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. CLEANED GRILL & DETECTOR UNIT. OPERATION CHECKED GOOD.
- [SDR ABXA20150526066](https://openairdocs.org/sdr/ABXA20150526066), May 26, 2015: SMOKE DETECTOR. FALSE ACTIVATION. LAVATORY SMOKE ALARM SOUNDED. NO SMOKE OBSERVED. LAVATORY SMOKE DETECTOR OPERATION CHECKED GOOD.
- [SDR ABXA20131113654](https://openairdocs.org/sdr/ABXA20131113654), Nov 13, 2013: BEAM. CRACKED. NUMBER 1 PYLON SKIRT BEAM ON OTBD SIDE IS CRACKED & CHAFED AROUND FASTENER HOLES. R & R NR 1 PYLON SKIRT BEAM OTBD SIDE IAW B767 SRM 51-40-02, PN 313T1380-241, 
- [SDR ABXA20131113653](https://openairdocs.org/sdr/ABXA20131113653), Nov 13, 2013: GUSSET. CORRODED. NUMBER 1 ENG PYLON FWD EDGE UPPER STRUCTURE HAS CHAFED AREA TO BARE METAL, WITH INLET REMOVED. R & R -36 CHAFFED GUSSET ON NR 1 ENG PYLON FWD UPPER EDGE IAW B76
- [SDR ABXA20131107652](https://openairdocs.org/sdr/ABXA20131107652), Nov 7, 2013: STIFFENER. CRACKED. NR 1 PYLON FWD OF PANEL 437DB INSIDE STRUCTURE LOWER CROSS BRACE HILOCK LOOSE. R & R NEW FABRICATED PADS ON ALL AREAS DAMAGED. PN 313T3380-303 WEB & FRAME 1INCH
- [SDR ABXA20131107651](https://openairdocs.org/sdr/ABXA20131107651), Nov 7, 2013: SKIN PANEL. CORRODED. UPPER TRAILING PANELS FWD OF OTBD AILERON RAISED IN TWO SPOTS ON PANEL LE. R & R UPPER TE PANELS IAW B767 SRM 51-40-02 PARA 4 & PARA 7. REPAIRED CORRODED SKIN I
- [SDR ABXA20131107650](https://openairdocs.org/sdr/ABXA20131107650), Nov 7, 2013: CHANNEL. CORRODED. REAR SPAR TO TE PANEL ATTACH CHANNEL AT WING STATION 1046 SPLIT ON EDGE. FABRICATED NEW CHORD ON RFA B657-60757 REMOVED OLD CHORD & INSTALLED NEW CHORD IAW B767
- [SDR ABXA20120225219](https://openairdocs.org/sdr/ABXA20120225219), Feb 25, 2012: SPAR. CORRODED. CORROSION SPOT ON TOP OF REAR SPAR OF LEFT HORIZ STAB STA 318 TO 335. REPAIRED ON REA B655-59696-MR, A/W/G.
- [SDR ABXA20120225214](https://openairdocs.org/sdr/ABXA20120225214), Feb 25, 2012: SPAR. CORRODED. CORROSION SPOT ON REAR SPAR UPPER CAP ON LT HORIZONTAL STAB AT SS 238. REPAIRED ON REA B655-59696-MR.
- [SDR ABXA20120225213](https://openairdocs.org/sdr/ABXA20120225213), Feb 25, 2012: RIB. CORRODED. CORROSION SPOT ON TOP OF RIB AT LEFT HORIZ STAB REAR SPAR TO TRAILING EDGE AT STA 226. REPAIRED ON REA B7655-59696-MR, AWG.
- [SDR ABXA20120225212](https://openairdocs.org/sdr/ABXA20120225212), Feb 25, 2012: SPAR. CORRODED. CORROSION SPOT ON TOP OF REAR SPAR OF LEFT HORIZ STAB REPAIRED ON REA B655-59696-MR, AWG
- [SDR ABXA20120225211](https://openairdocs.org/sdr/ABXA20120225211), Feb 25, 2012: SPAR. CORRODED. SPOT OF CORROSION ON TOP OF REAR SPAR OF LEFT HORIZ STAB REPAIRED ON REA B655-59696-MR, A/W/G.
- [SDR ABXA20120224220](https://openairdocs.org/sdr/ABXA20120224220), Feb 24, 2012: SPAR. CORRODED. CORROSION SPOT ON RIB OF LEFT HORIZ STAB FROM REAR SPAR TO TRAILING EDGE AT STA 335. REPLACED "T" CORD IAW B767 SRM 51-40-02, AWG.
- [SDR ABXA20120224218](https://openairdocs.org/sdr/ABXA20120224218), Feb 24, 2012: RIB. CORRODED. CORROSION SPOT ON RIB AT REAR SPAR TO TRAILING EDGE OF LEFT HORIZ STAB AT STA 323. REPLACED "T" CORD B767 SRM 51-40-02, A/W/G.
- [SDR ABXA20120224217](https://openairdocs.org/sdr/ABXA20120224217), Feb 24, 2012: SPAR. CORRODED. CORROSION SPOT MARKED NR 4 ON TRAILING EDGE UPPER SPAR OF LEFT HORIZ STAB AT STA 287. REPAIRED IAW REA B655-55695-MR, A/W/G.
- [SDR ABXA20120224209](https://openairdocs.org/sdr/ABXA20120224209), Feb 24, 2012: SPLICE PLATE. CRACKED. LEFT WING OUTBD UPPER L/E SPLICE PLATE CRACKED AT APPOX LWS 564. REPAIRED IAW REA B651-59661, AIRCRAFT WAS GROUNDED.
- [SDR ABXA20120220206](https://openairdocs.org/sdr/ABXA20120220206), Feb 20, 2012: SKIN. GOUGED. FUSELAGE SKIN IS GOUGED AT FLC DOOR CUTOUT AREA LOWER FWD. REPAIRED IAW REA B653-59680.
- [SDR ABXA20120216207](https://openairdocs.org/sdr/ABXA20120216207), Feb 16, 2012: SHIM. CORRODED. RT HORZ STAB TRAILING EDGE UPPER SURFACE BONDED PANEL BULGED AROUND FASTENER, LOCATED AFT OF RIB 13. REPLACED CORRODED SHIM AT RIB 13 IAW B767-200 SRM 51-20-11.
- [SDR ABXA20120215208](https://openairdocs.org/sdr/ABXA20120215208), Feb 15, 2012: FITTING. DENTED. LEFT ENGINE BACK UP FITTING OUTBOARD OF RIB 8 HAS 3 SMALL TOOLING MARKS. REMOVED TOOLING MARKS IAW REA B657-59674, AIRCRAFT WAS GROUNDED.
- [SDR ABXA20120206210](https://openairdocs.org/sdr/ABXA20120206210), Feb 6, 2012: WEB. CRACKED. VERT STAB PANEL 324CLX ACCESS, LWR LT FWD ANGLE CRACKED INSIDE AUX BOX. REMOVED WEB AND ANGLE, FABRICATED ANGLE IAW BOEING DWG 173T1215. RE-INSTALLED FABRICATED
- [SDR ABXA20111117132](https://openairdocs.org/sdr/ABXA20111117132), Nov 22, 2011: ESCAPE REEL. DEPLOYED. FOUR ESCAPE REELS DEPLOYED AFTER LANDING. INSTALLED 4 EMERGENCY ESCAPE REELS PER B767 AMM 25-61- 03-4. PART EFFECTIVITY VERIFIED, AIRCRAFT WAS NOT GROUNDED.
- [SDR ABXA2011071669](https://openairdocs.org/sdr/ABXA2011071669), Jul 16, 2011: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AT LOWER AFT CORNER OF MED DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS PLACED TO "ON". RELAMPED, OP CHECK GOOD.
- [SDR ABXA201012070167](https://openairdocs.org/sdr/ABXA201012070167), Dec 5, 2010: SMOKE DETECTOR. FALSE ACTIVATION. DETECTED FIRE/SMOKE IN MAIN CARGO COMPARTMENT. DECLARED EMERGENCY AND RETURNED TO LAND AT CVG. COMPLIED WITH OVERWEIGHT LANDING INSPECTION IAW 05-51-35-2 PHASE 
- [SDR ABXA201008090103](https://openairdocs.org/sdr/ABXA201008090103), Aug 8, 2010: FIRE WARNING. FALSE ACTIVATION. WHEEL WELL FIRE ANNUNCIATOR LIGHT ON FORWARD PANEL COME ON DURING CRUISE. COMPLIED WITH ABNORMAL, FIRE TEST NORMAL. DEFERRED. WHEEL WELL LIGHT WILL NOT STAY ON 
- [SDR ABXA201006010083](https://openairdocs.org/sdr/ABXA201006010083), May 29, 2010: SLAT TRACK. CORRODED. NR 11 SLAT I/B AND O/B MAIN TRACKS HAVE SURFACE CORROSION ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED NR 11 SLAT MAIN TRACKS IAW B767 AMM 27-81-54-4. REMO
- [SDR ABXA201006010086](https://openairdocs.org/sdr/ABXA201006010086), May 26, 2010: SUPPORT. DAMAGED. NR 2 FLAP SUPPORT ACTUATOR FASTENER HOLES 3 EACH, 2 FWD UPPER SMALL DIA AND 1 LARGE AFT UPPER CENTER HOLE HAVE EDDY CURRENT INDICATION USING HOLD SCAN IAW 50-04
- [SDR ABXA201006010085](https://openairdocs.org/sdr/ABXA201006010085), May 25, 2010: CHANNEL. CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL ATTACH HAT CHANNEL HAS VERTICAL ATTACH ANGLE CRACKED AT STA 1417 RBL 8. REMOVED AND REPLACED ATTACH ANGLE IAW B767 SRM 51-40-
- [SDR ABXA201006010084](https://openairdocs.org/sdr/ABXA201006010084), May 25, 2010: SUPPORT. CORRODED. LT WING L/E SUPPORT CORRODED ABOVE WING FUEL PANEL. REMOVED CORROSION. FOUND LT WING L/E SUPPORT TO BE OUT OF LIMITS. REPAIRED LT WING L/E SUPPORT IAW 767-200 S
- [SDR ABXA201005200082](https://openairdocs.org/sdr/ABXA201005200082), May 18, 2010: STRUCTURE. CRACKED. #1 ENG I/B THRUST REVERSER #13 CASCADE HAS 3 CRACKS. REMOVED AND REPLACED #13 CASCADE IAW B767 AMM 78-31-16-4
- [SDR ABXA201005200081](https://openairdocs.org/sdr/ABXA201005200081), May 17, 2010: RIB. CORRODED. LT WING L/E SUPPORT HAS CORROSION JUST INBD OF OUTBD AUX TRACK NR 3 SLAT. REMOVED AND REPLACED RIB IAW SRM 51-40-2
- [SDR ABXA201005200079](https://openairdocs.org/sdr/ABXA201005200079), May 17, 2010: SUPPORT. CORRODED. LT WING LE NR 3 SLAT INBD AUX TRACK HAS CORROSION ON INBD & OUTBD SUPPORTS. REMOVED CORROSION ON I/B SUPPORT IAW SRM51-10-02. REMOVED AND REPLACED SUPPORT IAW S
- [SDR ABXA201005200080](https://openairdocs.org/sdr/ABXA201005200080), May 14, 2010: RIB. DAMAGED. CLOSE OUT NOSE RIB AT LES 568 IS DAMAGED. REMOVED DAMAGED NOSE RIB FABRICATED NEW NOSERIB IAW B767 DWG 114T2512. INSTALLED NOSE RIB IAW B767-200 SRM 51-40-02
- [SDR ABXA201005140076](https://openairdocs.org/sdr/ABXA201005140076), May 13, 2010: STRUCTURE. CRACKED. CRACK EMANATING FROM RIVET AT BS 1702 BETWEEN S7L TO S8L. CRACK IS .1250 INCH IN LENGTH. REPAIRED AREA IAW B767 SRM 53-80-01-FIG 201.

All 82: https://openairdocs.org/deregistered/N775AX-2024-04-09/reports.md

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