# N787AX: 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: 23020
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: September 14, 2009
- Certificate issued: January 14, 2024
- Last registry action: January 14, 2024
- Mode S code: AAAA9D
- Owner when cancelled: [First Class Air Support LLC](https://openairdocs.org/faa-owner/FIRST%20CLASS%20AIR%20SUPPORT%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- 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/N787AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=787AX
- Page: https://openairdocs.org/deregistered/N787AX-2024-04-09

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 (104, newest 50)

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

- [SDR ABXA201806214072](https://openairdocs.org/sdr/ABXA201806214072), Jun 14, 2018: PANEL. DELAMINATED. DELAMINATION FOUND ON THE TWO LEFT WING TO BODY FAIRING PANELS, 197KL AND 195PL, THE PANELS WERE REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201805240057](https://openairdocs.org/sdr/ABXA201805240057), Apr 20, 2018: DOOR. OPEN. IN THE CEILING BY THE L1 ENTRY DOOR, THE DESCENT DEVICE CONTAINER DOOR OPENED AND ONE DESCENT DEVICE UNWOUND TO THE FLOOR. THE WAS GROUNDED, THE DESCENT DEVICE 
- [SDR ABXA20171208146](https://openairdocs.org/sdr/ABXA20171208146), Dec 8, 2017: DOOR. UNSECURE. THE FIRST OFFICER'S EMERGENCY ESCAPE ROPE CONTAINER DOOR OPENED DURING LANDING. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THE FIRST OFFICER'S ESCA
- [SDR ABXA20170825093](https://openairdocs.org/sdr/ABXA20170825093), Aug 25, 2017: CARABINER. MISSING. THREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFET
- [SDR ABXA20170310021](https://openairdocs.org/sdr/ABXA20170310021), Mar 10, 2017: ESCAPE REEL. DETACHED. THREE DESCENT DEVICES WERE FOUND ON THE FLOOR AFTER TAKEOFF. THE AIRPLANE WAS REMOVED FROM SERVICE. REPLACED WITH SERVICEABLE DESCENT DEVICES.
- [SDR ABXA20170129003](https://openairdocs.org/sdr/ABXA20170129003), Jan 29, 2017: RHEOSTAT. FAILED. AFTER ENGINE START WHEN TURNING OFF THE LEFT OVERRIDE LIGHT SWITCH, THE "MAIN PNL FLOOD LT" CIRCUIT BREAKER TRIPPED OPEN. SMOKE AND AN ELECTRICAL ODOR WERE OBSE
- [SDR ABXA20160706109](https://openairdocs.org/sdr/ABXA20160706109), Jul 6, 2016: STRINGER. CRACKED. STRINGER 22L CRACKED 6 INCHES, REPAIRED THE STRINGER IAW SRM 53-00-03 REPAIR 2. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20160705111](https://openairdocs.org/sdr/ABXA20160705111), Jul 5, 2016: SEAT TRACK. CRACKED. CRACK INDICATION DETECTED AT FASTENER HOLE NR 8 ON THE LEFT HAND STUB BEAM AT BS 883.5, LBL89. REMOVED FASTENERS FROM SEAT TRACK FOR ACCESS REAMED NR 8 HOLE UP 
- [SDR ABXA20160701113](https://openairdocs.org/sdr/ABXA20160701113), Jul 1, 2016: FRAME. CRACKED. UPPER HALF BS 883.5 LBL89 LOWER SIDE FRAME INNER CHORD CRACKED IN RADIUS LOWER END. VERIFIED BY EDDY CURRENT. REMOVED FASTENERS FOR REPAIR AND FOR ACCESS COMPLI
- [SDR ABXA20160629110](https://openairdocs.org/sdr/ABXA20160629110), Jun 29, 2016: STRINGER. CRACKED. STRINGER SPLICE 24L CRACKED BS 676. REMOVED AND REPAIRED THE STRINGER SPLICE BS 676 - 698 IAW SRM 53-00-03 REPAIR 2 DETAIL 3. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20160628107](https://openairdocs.org/sdr/ABXA20160628107), Jun 28, 2016: KEELBEAM. CORRODED. CORROSION ON KEEL PANEL EXTENSION STA 793 TO 808 LBL. REMOVED CORRODED AREA OF KEEL. NDT CHECKED SURFACE AND HOLES FOUND TO BE DEFECTIVE. COMPLIED WITH ENGINEER
- [SDR ABXA20160617112](https://openairdocs.org/sdr/ABXA20160617112), Jun 17, 2016: ANGLE. CRACKED. BRACKET FOR OUTBOARD ARROWHEAD PANEL SEAL BETWEEN PYLON AND EXHAUST CRACKED. REMOVED AND FABRICATED BRACKET FOR OUTBOARD ARROWHEAD PANEL SEAL BETWEEN PYLON EXHA
- [SDR ABXA20160617108](https://openairdocs.org/sdr/ABXA20160617108), Jun 17, 2016: STRINGER. CRACKED. STRINGER 21L CRACKED AFT SIDE OF BS 676. REMOVED AND REPAIRED THE DAMAGE IAW SRM 53-00-03 REPAIR 2 DETAIL 4.
- [SDR ABXA20160615093](https://openairdocs.org/sdr/ABXA20160615093), Jun 15, 2016: BRACKET. CRACKED. UPPER T/E BRACKET FOR INBD ARROWHEAD PANEL SEAL BETWEEN PYLON AND EXHAUST NOZZLE CRACKED. FABRICATED REPAIR ANGLE IAW SRM 51-30-01, FIG 2 ID 1 AND 00838880 TAS 
- [SDR ABXA20160614092](https://openairdocs.org/sdr/ABXA20160614092), Jun 14, 2016: SUPPORT BEAM. CRACKED. LEFT WING T/E UPPER PANEL SUPPORT BEAM FORWARD OF INBD AILERON AT WING STA 431-WING STA 468 IS CRACKED AT THE LNBD END. REMOVED PANEL SUPPORT BEAM. FABRICATED N
- [SDR ABXA20160610094](https://openairdocs.org/sdr/ABXA20160610094), Jun 10, 2016: BUSHING. GALLED. RT MLG SIDE BRACE AFT OTBD BUSHING HAS GALLING MARKS ON THE INSIDE RACE. REMOVED AND INSTALLED A NEW RT MLG SIDE BRACE AFT OTBD BUSHING IAW REA 62096. LENGTH: G
- [SDR ABXA20160606091](https://openairdocs.org/sdr/ABXA20160606091), Jun 6, 2016: FRAME. CRACKED. LEFT STA 859.5, LBL89 LOWER LT SIDE FRAME INNER CHORD CRACKED IN RADIUS ON LOWER END, VERIFIED BY EDDY CURRENT. REMOVED FASTENERS, COMPLIED WITH EA 53000047-101
- [SDR ABXA20141022335](https://openairdocs.org/sdr/ABXA20141022335), Oct 22, 2014: BEAM. CORRODED. LEFT FLAP 9 - 10 BEAM 4 AFT ATTACHMENT & 2 FWD ATTACHMENT HOLES ARE CORRODED. REMOVED & RE-ROUTE 9 - 10 BEAM TO COMPONENT SERVICES FOR REPAIR IAW REA C057-61249
- [SDR ABXA20141021336](https://openairdocs.org/sdr/ABXA20141021336), Oct 21, 2014: SUPPORT. CORRODED. RIGHT WING PANEL 661NB AFT PANEL SUPPORT EXFOLIATED. R & R PANEL SUPPORT IAW B657-61286. CORRODED L2, PN 113T1912-29, PART NAME BEAM, SN NSN, STRINGER & WS LOCA
- [SDR ABXA20141021334](https://openairdocs.org/sdr/ABXA20141021334), Oct 21, 2014: BEAM. CORRODED. RIGHT FLAP 9 - 10 BEAM FWD 4 & AFT 2 ATTACHMENT HOLES ARE CORRODED. REMOVED & RE-ROUTE 9 - 10 BEAM TO COMPONENT SERVICES FOR WORK IAW REA C057-61250-MR. REINSTA
- [SDR ABXA20141017320](https://openairdocs.org/sdr/ABXA20141017320), Oct 17, 2014: SUPPORT FITTING. CRACKED. SPOILER ACTUATOR SUPPORT BRACKET CRACKED IN TWO AT RT WING STATION 700. LOCATED JUST FWD OF FLAP TORQUE TUBE SUPPORT. REMOVED & INSTALLED SERVICEABLE FITTING IA
- [SDR ABXA20141016331](https://openairdocs.org/sdr/ABXA20141016331), Oct 16, 2014: STRUCTURE. CRACKED. RIGHT 1809 CHORD CRACKED AREA 2 FWD LOWER LE. FWD LOWER FASTENER OF AREA 1 NEEDS REMOVED TO VERIFY DEFECT INDICATION IAW STEP 11 OF TASK CARD NEA53800003-001. R
- [SDR ABXA20141013332](https://openairdocs.org/sdr/ABXA20141013332), Oct 13, 2014: RIB. CRACKED. RIGHT OTBD FLAP NR 7 SUPPORT INBD FLANGE ACTUATOR HOLE AT 1:00 LOOKING INBD HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN, ALSO OTBD FLANGE HOLE AT 12:00 HAS AN
- [SDR ABXA20141013330](https://openairdocs.org/sdr/ABXA20141013330), Oct 13, 2014: SPLICE PLATE. CORRODED. FRONT SPAR UPPER CHORD CORRODED ABOVE NR 8 SLAT TAI TELESCOPING DUCT. REPAIRED CORROSION ON UPPER SPLICE PLATE IAW REA B657-61236. L2 CORROSION, PN 114T023-20, 
- [SDR ABXA20141008333](https://openairdocs.org/sdr/ABXA20141008333), Oct 8, 2014: SPLICE PLATE. CRACKED. NUMBER 1 PYLON AT INBD LOWER BEAM HYD BAY DOOR AT AFT END STRUCTURE IS CRACKED ABOVE & BELOW THE BEAM. R & R SPLICE PLATE IAW SRM 51-10-2. CRACKED 2.O INCHES, P
- [SDR ABXA20141007321](https://openairdocs.org/sdr/ABXA20141007321), Oct 7, 2014: SPLICE PLATE. CORRODED. FRONT SPAR UPPER CHORD CORRODED AT LES 464. REMOVED CORROSION FOUND TO BE OUT OF LIMITS WILL BE REPAIRED ON REA B657-61236. CORRODED L2, PN 114T023-20, SN NSN, 
- [SDR ABXA20141006329](https://openairdocs.org/sdr/ABXA20141006329), Oct 6, 2014: RIB. CRACKED. RIGHT WING NR 8 ACTUATOR SUPPORT INBD FLANGE 1 EACH HOLE OVERSIZE, 1 EACH OTBD HOLE. REPAIRED HOLES IAW REA B657-61258-MR, RFTS NR E-46238. CRACKED .0625 INCHES
- [SDR ABXA20141006323](https://openairdocs.org/sdr/ABXA20141006323), Oct 6, 2014: FITTING. CORRODED. LEFT 1809 CHORD TENSION FITTING AREA 1 UPPER AFT HOLE ELONGATED. PERFORMED PERMANENT REPAIR OF THE FWD CHORD IAW SB 767-53A0078. CORRODED L2, PN 0157T1059-7, 14
- [SDR ABXA20141003327](https://openairdocs.org/sdr/ABXA20141003327), Oct 3, 2014: RIB. CRACKED. LEFT OTBD FLAP NR 2 SUPPORT INBD FLANGE 2 ACTUATOR HOLES AT 12:00 HAVE DEFECT INDICATIONS WITH HFEC ROTARY SCAN. OTBD FLAP NR 2 SUPPORT INBD FLANGE 2 ACTUATOR H
- [SDR ABXA20141002326](https://openairdocs.org/sdr/ABXA20141002326), Oct 2, 2014: RIB. CRACKED. FLANGE ACTUATOR HOLE AT 12:00 HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. CLEANED OUT HOLES LAW AMM 20-10-22 SEE REA 657-61238-MR. CRACKED 1/64, PN 113T1345-
- [SDR ABXA20140930324](https://openairdocs.org/sdr/ABXA20140930324), Sep 30, 2014: STRAP. CRACKED. INSIDE ACCESS PANEL 447BR NR 2 STRUT AFT VERTICAL ROW OF FASTENERS FOR ARROWHEAD PANEL STRUCTURE IS CRACKED. R & R DOUBLER LAW SRM 51-40-02 PER 7. CRACKED 3 INC
- [SDR ABXA20140929328](https://openairdocs.org/sdr/ABXA20140929328), Sep 29, 2014: FITTING. CRACKED. NUMBER 2 ENG OTBD CORE COWL NR 4 LATCH FITTING CRACKED INSIDE OF POCKET & LOCK FASTENERS ARE DAMAGED. REMOVED OLD LATCH FITTING & DRILLED NEW FITTING IAW SRM 51
- [SDR ABXA20140928322](https://openairdocs.org/sdr/ABXA20140928322), Sep 28, 2014: KEELBEAM. CORRODED. CENTER BEAM IN LT WW BS 997, LBL 8, WL 115 IS CORRODED. CORRODED AREA WAS BLENDED, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-50-12. REPAIRED IAW REA B653-6
- [SDR ABXA20140925325](https://openairdocs.org/sdr/ABXA20140925325), Sep 25, 2014: BEAM. CRACKED. NUMBER 2 STRUT OTBD LOWER BEAM IS CRACKED AT FWD END. R & R OTBD LOWER STRUT BEAM INSTALLED IAW SRM 51-40-02. INSTALLED BRACKETS IAW SRM-51-40-02. PN 313T1380-2
- [SDR ABXA20140925319](https://openairdocs.org/sdr/ABXA20140925319), Sep 25, 2014: SUPPORT. CORRODED. RIGHT WING UPPER PANEL SUPPORT TEE INBD END OF 651MT EXFOLIATED NEAR AFT END OF TEE. R & R UPPER CLAMP LAW SRM 51-40-2. CORRODED L2, PN 113T1623-158, PART NAME 
- [SDR ABXA20140624235](https://openairdocs.org/sdr/ABXA20140624235), Jun 24, 2014: UNKNOWN. ODOR. NOTICED STRONG ELEC ODOR WITH HOT CUP ON AFTER TWO MINUTES. TURNED OFF & SMELL WENT AWAY. RAN HOT CUP FOR SEVERAL MINUTES, CHECKED GOOD. NO ELEC SMELL NOTICED. 
- [SDR ABXA20130806502](https://openairdocs.org/sdr/ABXA20130806502), Aug 6, 2013: BATTERY PACK. INOPERATIVE. SUPER NUMERARY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW AMM 33-50-00-00, AND FOUND M736 POWER SUPPLY INOPERATIVE. R & R BATTERY ASSY. ALL EMERGENCY LIGHTS O
- [SDR ABXA20121221373](https://openairdocs.org/sdr/ABXA20121221373), Dec 21, 2012: ANGLE. CRACKED. ANGLE PIECE AT TOP OF FRONT SPAR TO LEADING EDGE CRACKED AT BOTTOM LOCATED AFT AND ABOVE SLAT PDU BEHIND NUMBER 6 SLAT. REMOVED & REPLACED ANGLE IAW B767-200 SR
- [SDR ABXA20121219370](https://openairdocs.org/sdr/ABXA20121219370), Dec 19, 2012: TEE FITTING. CORRODED. RIGHT WING LOWER FORWARD STRUCTURE AT WING STATION 735 HAS CORROSION ON PANEL BRACE TEE CLIP STRUCTURE. REMOVED FWD BEAM AT STA 735, REMOVED TEE CLIP, FABRICATE
- [SDR ABXA20121219368](https://openairdocs.org/sdr/ABXA20121219368), Dec 19, 2012: STRUCTURE. CRACKED. RIGHT NOSE LANDING GEAR VERTICAL CHORD HAS DEFECT INDICATION 11.25 INCHES IN FROM TOP. REPAIRED AREA IAW B767-200 SRM 51-70-12 PG 1 FIG 1, ACFT WAS GROUNDED.
- [SDR ABXA20121217371](https://openairdocs.org/sdr/ABXA20121217371), Dec 17, 2012: SHIM. CORRODED. SHIM PACK UNDER DOUBLER AT LEADING EDGE PANEL ATTACH ANGLE 20 INCHES OUTBOARD OF LEFT WING NUMBER 3 SLAT INBOARD AUX TRACK CORRODED. REMOVED FWD BEAM AT STA 735
- [SDR ABXA20121217367](https://openairdocs.org/sdr/ABXA20121217367), Dec 17, 2012: STRUCTURE. CRACKED. LEFT NOSE LANDING GEAR VERTICAL CHORD HAS DEFECT INDICATION 11 INCHES FROM TOP. INSTALLED REPAIR ON LEFT NOSE LANDING GEAR VERTICAL CHORD IAW B767-200 SRM 51-70
- [SDR ABXA20121214369](https://openairdocs.org/sdr/ABXA20121214369), Dec 14, 2012: SKIN. DENTED. FORWARD LEFT FUSELAGE STA 526 S30L-31L HAS UNMARKED DENT. REPAIRED DENT IAW B767-200 SRM 53-00-01 FIG 201 REPAIR 14, ACFT WAS GROUNDED.
- [SDR ABXA20121221374](https://openairdocs.org/sdr/ABXA20121221374), Dec 12, 2012: BEAM. CRACKED. OUTBOARD HYDRAULIC BAY DOOR LATCH PLATE ATTACH BEAM CRACKED AT FORWARD END. REMOVED AND REPLACED BEAM IAW B767-200 SRM 51-40-02, ACFT WAS GROUNDED.
- [SDR ABXA20120827248](https://openairdocs.org/sdr/ABXA20120827248), Aug 27, 2012: BATTERY. DISCHARGED. WHEN EMERGENCY LIGHT, (FLT DECK) TESTED; IT WOULD ILLUMINATE BRIEFLY AND THEN FADE OUT (OVER FLT DECK DOOR). REMOVED & REPLACED BATTERY FOR EMERGENCY LIGHTING A
- [SDR ABXA2011081696](https://openairdocs.org/sdr/ABXA2011081696), Sep 16, 2011: WEB. CRACKED. NR 1 PYLON T/E WEB CRACKED AT LOWER O/B CORNER JUST FWD OF PNL 437DB. REPLACED NR 1 PYLON T/E WEB IAW B767 SRM 51-40-02 AWG.
- [SDR ABXA20110907104](https://openairdocs.org/sdr/ABXA20110907104), Sep 7, 2011: TEE FITTING. CORRODED. LT FAILSAFE STRAP "T" FITTING IS DEEPLY CORRODED AND ONE OF THE FASTENER HOLES HAS INSUFFICIENT. REMOVED AND REPLACED "T" FITTING IAW REA B653-59439-MR, AWG.
- [SDR ABXA20110905106](https://openairdocs.org/sdr/ABXA20110905106), Sep 5, 2011: SKIN PANEL. CORRODED. SKIN PANEL COMMON TO RT FAILSAFE STRAP "T" FITTING CORRODED. REPAIRED SKIN IAW REA B653-59476-MR, AWG. CRACK AREA: 2" X 5".
- [SDR ABXA20110905105](https://openairdocs.org/sdr/ABXA20110905105), Sep 5, 2011: SKIN PANEL. CRACKED. SKIN PANEL COMMON TO LT FAILSAFE STRAP "T" FITTING CORRODED. REPAIRED SKIN IAW REA B653-59477-MR, AWG., CRACK AREA: 2" X 6".
- [SDR ABXA2011090389](https://openairdocs.org/sdr/ABXA2011090389), Sep 3, 2011: FAILSAFE. CRACKED. LEFT FAILSAFE STRAP FS 955 LEFT WHEEL WELL IS CRACKED AT THE 1:00 CLOCK POSITION, CRACK EXTENDS TO .160 FROM RADIUS. DAMAGED REMOVED IAW B767 SB 767-53A0100.

All 104: https://openairdocs.org/deregistered/N787AX-2024-04-09/reports.md

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