# N794AX: Boeing 767-281, registration cancelled 2024-04-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 8, 2024
- Status when cancelled: Registration pending
- 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: 23144
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 16, 2009
- Last registry action: January 14, 2024
- Mode S code: AAC6F7
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Individual
- Owner's area on the map: 38.1517° N, 85.5172° W: Placed by OpenAirDocs at the center of ZIP code 40299, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N794AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=794AX
- Page: https://openairdocs.org/deregistered/N794AX-2024-04-08

From the FAA registry file of October 29, 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 (93, newest 50)

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

- [SDR ABXA20171127141](https://openairdocs.org/sdr/ABXA20171127141), Nov 27, 2017: SENSOR. MALFUNCTIONED. PASSING THROUGH FLIGHT LEVEL 230, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. THE CREW COULD NOT RESTORE NORMAL ENGINE OPERATION VIA THE QUICK REFERENCE HAN
- [SDR ABXA20171124140](https://openairdocs.org/sdr/ABXA20171124140), Nov 24, 2017: STATOR VANE. OUT OF ADJUST. DURING CLIMB THROUGH FLIGHT LEVEL 200, THREE LOUD BANGS OCCURRED THAT JOLTED THE AIRCRAFT. THE AIRPLANE SEEMED TO YAW EACH TIME. NO ABNORMAL ENGINE INDICATIONS 
- [SDR ABXA20171122139](https://openairdocs.org/sdr/ABXA20171122139), Nov 22, 2017: COMPRESSOR. STALLED. RIGHT ENGINE HAD A COMPRESSOR STALL. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE FAULT ISOLATION MANUAL DIAGRAM 71-05, FAULT TREE 808 WAS ACCOMPLISHED. ALL FI
- [SDR ABXA20171121138](https://openairdocs.org/sdr/ABXA20171121138), Nov 21, 2017: TEE FITTING. CORRODED. CORROSION ON THE ATTACH TEE AT THE REAR SPAR/UPPER RIB INTERSECTION OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE TEE W
- [SDR ABXA20171121137](https://openairdocs.org/sdr/ABXA20171121137), Nov 21, 2017: RIB. CORRODED. CORROSION ON UPPER RIB CHORD OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121135](https://openairdocs.org/sdr/ABXA20171121135), Nov 21, 2017: FLOORBEAM. CORRODED. CORROSION ON THE FORWARD SIDE OF THE FLOOR BEAM CHORD AT FUSELAGE STATION 1109, LBL 46, IN THE AFT LOWER CARGO COMPARTMENT. THE CHORD WAS REPLACED. AIRPLANE WAS
- [SDR ABXA20171121134](https://openairdocs.org/sdr/ABXA20171121134), Nov 21, 2017: TEE FITTING. CORRODED. CORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, RBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS G
- [SDR ABXA20171121133](https://openairdocs.org/sdr/ABXA20171121133), Nov 21, 2017: TEE FITTING. CORRODED. CORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, LBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS G
- [SDR ABXA20171121132](https://openairdocs.org/sdr/ABXA20171121132), Nov 21, 2017: STRINGER. CORRODED. CORROSION ON STRINGER 32L AT FUSELAGE STATION 434. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121131](https://openairdocs.org/sdr/ABXA20171121131), Nov 21, 2017: RIB. CORRODED. CORROSION IN RIGHT LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121130](https://openairdocs.org/sdr/ABXA20171121130), Nov 21, 2017: RIB. CRACKED. CRACK IN RIGHT WING NOSE RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121129](https://openairdocs.org/sdr/ABXA20171121129), Nov 21, 2017: RIB. CORRODED. CORRODED NUT PLATES ON THE RIGHT WING LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121128](https://openairdocs.org/sdr/ABXA20171121128), Nov 21, 2017: STRINGER. CRACKED. CRACK IN STRINGER 5L AT SPLICE. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20171121127](https://openairdocs.org/sdr/ABXA20171121127), Nov 21, 2017: FITTING. CRACKED. CRACK IN FRAME TO STRINGER ATTACH CLIP AT STA 1702. THE ATTACH CLIP WAS REPLACED. AIRPLANE WAS GROUNDED.
- [SDR ABXA20170830095](https://openairdocs.org/sdr/ABXA20170830095), Aug 30, 2017: CARABINER. MISSING. TWO EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), TWO NEW SAFETY HA
- [SDR ABXA20170513063](https://openairdocs.org/sdr/ABXA20170513063), May 13, 2017: WIRE. SHORTED. DURING TAXI, EICAS MESSAGE FOR THE LT REVERSER ISOLATION VALVE DISPLAYED AND THE THRUST REVERSER INDICATION CIRCUIT BREAKER TRIPPED OPEN. THE AIRPLANE WAS REMOV
- [SDR ABXA20160506088](https://openairdocs.org/sdr/ABXA20160506088), May 6, 2016: FAILSAFE. CRACKED. LOWER FASTENER HOLE IN RT FAILSAFE COMMON TO T FITTING IS CRACKED, VERIFIED BY HFEC HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUM
- [SDR ABXA20160505089](https://openairdocs.org/sdr/ABXA20160505089), May 5, 2016: FAILSAFE. CRACKED. LEFT FAILSAFE LOWER HOLE COMMON TO T FITTING HAS CRACK INDICATION, VERIFIED BY HFEC ROTARY HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IA
- [SDR ABXA20151209201](https://openairdocs.org/sdr/ABXA20151209201), Dec 9, 2015: FITTING. CORRODED. NUMBER 9, COUNTED FROM FRONT, MAIN DECK CARGO DOOR LATCH CAM PIN FITTING HAS CORROSION IN THE BORE. REMOVED, REPAIRED & RE-INSTALLED NR 9 LATCH PIN & LATCH PIN 
- [SDR ABXA20151208199](https://openairdocs.org/sdr/ABXA20151208199), Dec 8, 2015: SKIN. CORRODED. SUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 912. REMOVED PANELS, REMOVED CORROSION & NDT INSPECTED. PERFORMED REPAIR ON REA B657-61824-MR. REINSTALLED PANE
- [SDR ABXA20151208198](https://openairdocs.org/sdr/ABXA20151208198), Dec 8, 2015: SKIN. CORRODED. SUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 1025. REPAIRED CORRODED AREA ON RT WING AT REAR SPAR & WS 1030 IAW REA B657-61825-MR. REINSTALLED FIXED PANELS 
- [SDR ABXA20151208196](https://openairdocs.org/sdr/ABXA20151208196), Dec 8, 2015: SKIN. CORRODED. LEFT WING SURFACE CORRODED AFT OF OVERWING EXIT AT WING TO BODY FAIRING AT APPROX STATION 938. REMOVED CORROSION & REPAIRED AREA IAW REA B657-61841-MR. SDR INFO
- [SDR ABXA20151205204](https://openairdocs.org/sdr/ABXA20151205204), Dec 5, 2015: BULKHEAD. CRACKED. MID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER TS4 & TS5, RS23, INBD OF APU SHROUD. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T261
- [SDR ABXA20151205203](https://openairdocs.org/sdr/ABXA20151205203), Dec 5, 2015: BULKHEAD. CRACKED. MID FREQUENT EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148
- [SDR ABXA20151205202](https://openairdocs.org/sdr/ABXA20151205202), Dec 5, 2015: BULKHEAD. CRACKED. MID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 14
- [SDR ABXA20151203213](https://openairdocs.org/sdr/ABXA20151203213), Dec 3, 2015: STRUCTURE. CRACKED. LEFT 1809 FWD OUTER CHORD INBD FLANGE AT OTBD FASTENER BELOW SPLICE FITTING CRACKED APPROX 1.5". HFEC VERIFIED IAW NDTM PART 6 51-00-19. REMOVED & REINSTALLED A
- [SDR ABXA20151203197](https://openairdocs.org/sdr/ABXA20151203197), Dec 3, 2015: SKIN. CORRODED. CORROSION SUSPECTED AT LT WING REAR SPAR WS 854. BLEND OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA 657-61837-MR, WS 810-815. BLEND OUT & TRIM OUT FOR CORR
- [SDR ABXA20151202215](https://openairdocs.org/sdr/ABXA20151202215), Dec 2, 2015: SUPPORT BEAM. CORRODED. RIGHT WING TE UPPER PANEL SUPPORT AT WS 1052 IS CORRODED. REMOVED CORRODED PANEL SUPPORT BEAM & INSTALLED NEW FABRICATED BEAM REV NO 61536-0000-0005 & REA NO B6
- [SDR ABXA20151130214](https://openairdocs.org/sdr/ABXA20151130214), Nov 30, 2015: SKIN PANEL. CORRODED. RIGHT WING SKIN UPPER TE IS CORRODED UNDER PANEL 113T1651 AT WS 512 - 521. CORROSION UNDER UPPER WING TRAILING EDGE PANEL WAS REPAIRED ON REA B657-61823-M. PANE
- [SDR ABXA20151127216](https://openairdocs.org/sdr/ABXA20151127216), Nov 27, 2015: SUPPORT. CORRODED. RIGHT WING TE OTBD AILERON, HINGE SUPPORT RIB AT WS 1079.95 HAS CORROSION ON THE UPPER CHORD OF THE SUPPORT ASSEMBLY. REMOVED CORRODED CHORD & REPLACED WITH NEW
- [SDR ABXA20151125211](https://openairdocs.org/sdr/ABXA20151125211), Nov 25, 2015: STRINGER. CRACKED. UPPER CARGO STRINGER 19L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 19L, STATION 698 - 720 IAW ENGINEERING SKETCH NO ESO2821 REV A & 
- [SDR ABXA20151125194](https://openairdocs.org/sdr/ABXA20151125194), Nov 25, 2015: BRACKET. CRACKED. NUMBER 6 SLAT LOWER TE ATTACH ANGLE, OUTBOARD OF CTR AUX TRACK, IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFO
- [SDR ABXA20151125193](https://openairdocs.org/sdr/ABXA20151125193), Nov 25, 2015: ATTACH ANGLE. CRACKED. NUMBER 6 SLAT LOWER TE ATTACH ANGLE, LOCATED OUTBOARD OF OUTBOARD AUX TRACK IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 
- [SDR ABXA20151118210](https://openairdocs.org/sdr/ABXA20151118210), Nov 18, 2015: STRINGER. CRACKED. UPPER CARGO STRINGER 17L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. CONTACT ENGINEERING FOR REPAIR. REPAIRED CRACKED LONGERON STRINGER 17L, FS 676 - 70
- [SDR ABXA20151118209](https://openairdocs.org/sdr/ABXA20151118209), Nov 18, 2015: STRINGER. CRACKED. UPPER CARGO STRINGER 7L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED CRACKED LONGERON STRINGER 7L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES 028
- [SDR ABXA20151117205](https://openairdocs.org/sdr/ABXA20151117205), Nov 17, 2015: CHANNEL. CORRODED. WING TE PANEL ATTACH LOWER CHANNEL SPLIT ON EDGE AT TE WS 936. REMOVED DAMAGED CHANNEL, NEW CHANNEL FABRICATED REA B657-61805 & INSTALLED NEW CHANNEL IAW SRM 51
- [SDR ABXA20151113212](https://openairdocs.org/sdr/ABXA20151113212), Nov 13, 2015: STRINGER. CRACKED. FORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 21L AT FS. 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & 
- [SDR ABXA20151111208](https://openairdocs.org/sdr/ABXA20151111208), Nov 11, 2015: STRINGER. CRACKED. FORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE, CONTACT ENGINEERING FOR REPAIR. REPAIRED STRINGER 21L AT FS 676 - 707 IAW S
- [SDR ABXA20151111206](https://openairdocs.org/sdr/ABXA20151111206), Nov 11, 2015: SUPPORT. CORRODED. AT OPENING ABOVE LT LG, AFT WING PANEL ATTACH BEAM CORRODED AROUND NUTPLATE. REMOVED CORRODED PANEL ATTACH BEAM, DRILLED FOR LOCATION & INSTALLED IAW SRM 51-40-
- [SDR ABXA20151111195](https://openairdocs.org/sdr/ABXA20151111195), Nov 11, 2015: STRUCTURE. CORRODED. HORIZONTAL STABILIZER S10 UPPER AFT FLANGE AT RIB 2R OUTBOARD CORROSION. BLENDED AREA WITHIN LIMITS TO REMOVE CORROSION IAW SRM 51-10-02. SDR INFO, CORRODED LEV
- [SDR ABXA20151110207](https://openairdocs.org/sdr/ABXA20151110207), Nov 10, 2015: BEAM. CRACKED. NUMBER TWO STRUT INTERIOR STRUCTURE IS CRACKED WHERE PANEL 447ERX ATTACHES AT LOWER EDGE. R & R NR 2 PYLON HYD BAY OTBD BEAM WHERE PANEL 447ERX ATTACHES IAW SRM
- [SDR ABXA20151103200](https://openairdocs.org/sdr/ABXA20151103200), Nov 3, 2015: KEELBEAM. CORRODED. CORROSION FOUND ON LT LOWER KEEL CHORD STATION 952. CLEANED UP CORROSION ON LT LOWER KEEL CORD AT FS 952 IAW SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101. CORROSION 
- [SDR ABXA20150201002](https://openairdocs.org/sdr/ABXA20150201002), Feb 1, 2015: SWITCH. OUT OF TOLERANCE. MAIN CARGO DOOR LIGHT & SIREN ILLUMINATED DURING CLIMB OUT AT APPROXIMATELY 2.0 TO 2.1 PSID. INDICATION SWITCHES GAP ADJUSTED TO TOLERANCE & E1-1 BURNDY BLOCK C
- [SDR ABXA2014021423](https://openairdocs.org/sdr/ABXA2014021423), Feb 14, 2014: SUPPORT. CORRODED. HINGED PANEL 651TB OTBD LOWER PANEL ATTACH CHANNEL SPLIT ON EDGE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED BEAM, REPAIRED IAW REA B657-60865, PN 113
- [SDR ABXA2014021422](https://openairdocs.org/sdr/ABXA2014021422), Feb 14, 2014: STRUCTURE. CORRODED. TRAILING EDGE PANEL 652HB AFT ATTACH BEAM LOWER CHORD SPLIT ON EDGE. REPLACED LOWER CORD AT PANEL 652HB AFT ATTACH IAW SRM 51-40-02 PER 4 & 7. SDR INFO CORRODED
- [SDR ABXA2014021421](https://openairdocs.org/sdr/ABXA2014021421), Feb 14, 2014: BEAM. CORRODED. REAR SPAR TO TE PANEL ATTACH BEAM SPLIT ON INBD SIDE LOWER CHORD AT STATION 257, 20 INCHES FROM REAR SPAR. REPLACED REAR SPAR TO TE PANEL ATTACH BEAM IAW SRM 51
- [SDR ABXA2014021324](https://openairdocs.org/sdr/ABXA2014021324), Feb 13, 2014: SKIN. CORRODED. RIGHT WING TRAILING UPPER WING SKIN IS CORRODED 40 INCHES OTBD OF FUSE AT FWD EDGE OF PANEL 651 FT. BLENDED CORROSION AS DESCRIBED IAW SRM 51-20-01, AREA BLENDE
- [SDR ABXA2014021225](https://openairdocs.org/sdr/ABXA2014021225), Feb 12, 2014: SUPPORT BEAM. CORRODED. LEFT WING UPPER SURFACE, BULGE IN PANEL JUST FWD OF NR 5 SPOILER CTR OTBD FITTING. FOUND SPOILER SUPPORT BEAM TO BE CORRODED BEYOND LIMITS. FABRICATED NEW BEAN 
- [SDR ABXA2014021220](https://openairdocs.org/sdr/ABXA2014021220), Feb 12, 2014: FORMER. CRACKED. RIGHT WING LE NOSE BEAM FORMER IS CRACKED AT THE NR 8 SLAT INBD AUXILIARY TRACK INBD SIDE. REMOVED DAMAGED NOSE FORMER & INSTALLED NON-NOSE FORMER IAW SRM 51-40
- [SDR ABXA2014021216](https://openairdocs.org/sdr/ABXA2014021216), Feb 12, 2014: ANGLE. CORRODED. CORROSION FOUND BETWEEN STATION 999 & STATION 1021 IN LT WW BEHIND MAIN GEAR DOOR ACTUATOR ON CTR BEAM. CLEANED LT WW BEHIND MLG DOOR ACTUATOR FS 999 - 1021, FO

All 93: https://openairdocs.org/deregistered/N794AX-2024-04-08/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20040413004709I](https://openairdocs.org/incident/20040413004709I), Apr 13, 2004: Boeing 767281 (N794AX), Sacramento, CA. (-23) Abx flight 426 departed from international falls, MN, enroute to san jose CA. The right hand main landing gear (MLG) would not extend to the down and…

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