# Service difficulty reports: N787AX, cancelled Apr 9, 2024

A list on [N787AX, cancelled Apr 9, 2024](https://openairdocs.org/deregistered/N787AX-2024-04-09.md).

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

Page 1 of 3 · 104 reports

- [SDR ABXA201806214072](https://openairdocs.org/sdr/ABXA201806214072.md): Panel · delaminated · Jun 14, 2018 · N787AX · Boeing 767281 · Aerodynamic Fairings
  > 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.md): Door · open · Apr 20, 2018 · N787AX · Boeing 767281 · Emergency Equipment
  > 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 WAS REPLACED WITH A SERVICEABLE DESCENT DEVICE AND THE CONTAINER DOOR WAS CLOSED.
- [SDR ABXA20171208146](https://openairdocs.org/sdr/ABXA20171208146.md): Door · unsecure · Dec 8, 2017 · N787AX · Boeing 767281 · Emergency Equipment
  > THE FIRST OFFICER'S EMERGENCY ESCAPE ROPE CONTAINER DOOR OPENED DURING LANDING. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THE FIRST OFFICER'S ESCAPE ROPE WAS RE-STOWED INTO THE ROPE'S CONTAINER IN ACCORDANCE WITH THE 767 AMM SO THAT THE ROPE DID
- [SDR ABXA20170825093](https://openairdocs.org/sdr/ABXA20170825093.md): Carabiner · missing · Aug 25, 2017 · N787AX · Boeing 767281 · Emergency Equipment
  > THREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS U
- [SDR ABXA20170310021](https://openairdocs.org/sdr/ABXA20170310021.md): Escape Reel · detached · Mar 10, 2017 · N787AX · Boeing 767281 · Emergency Equipment
  > 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.md): Rheostat · failed · Jan 29, 2017 · N787AX · Boeing 767281 · Flight Compartment Lighting
  > 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 OBSERVED IN THE FORWARD-RIGHT SIDE OF THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED)
- [SDR ABXA20160706109](https://openairdocs.org/sdr/ABXA20160706109.md): Stringer · cracked · Jul 6, 2016 · N787AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > 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.md): Seat Track · cracked · Jul 5, 2016 · N787AX · Boeing 767281 · Fuselage, Seat/Cargo Attach Fittings
  > 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 UNTIL CLEAN AND ROUND. REPAIRED NR 8 HOLE IN CONJUNCTION WITH IAW REA B653-62098, B653-62101-MR AND
- [SDR ABXA20160701113](https://openairdocs.org/sdr/ABXA20160701113.md): Frame · cracked · Jul 1, 2016 · N787AX · Boeing 767281 · Fuselage Main, Frame
  > 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 COMPLIED WITH JOB CARD 53D00049-101 AND REA B653-62101-MR. TRACK TO BE INSTALLED ON NR 0338. SDR: CRACKED
- [SDR ABXA20160629110](https://openairdocs.org/sdr/ABXA20160629110.md): Stringer · cracked · Jun 29, 2016 · N787AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > 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.md): Keelbeam · corroded · Jun 28, 2016 · N787AX · Boeing 767281 · Fuselage Main, Keel
  > 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 ENGINEERING REPAIR IAW SRM 51-40-02 AND REA NR B653-62113-MR. CORRODED: LEVEL 2, PN 145T8611-1, KEEL, FS/
- [SDR ABXA20160617112](https://openairdocs.org/sdr/ABXA20160617112.md): Angle · cracked · Jun 17, 2016 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > BRACKET FOR OUTBOARD ARROWHEAD PANEL SEAL BETWEEN PYLON AND EXHAUST CRACKED. REMOVED AND FABRICATED BRACKET FOR OUTBOARD ARROWHEAD PANEL SEAL BETWEEN PYLON EXHAUST IAW SRM 54-51-71 AND 51-30-01. BRACKET WILL BE INSTALLED ON NON ROUTINE 0232.
- [SDR ABXA20160617108](https://openairdocs.org/sdr/ABXA20160617108.md): Stringer · cracked · Jun 17, 2016 · N787AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
  > 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.md): Bracket · cracked · Jun 15, 2016 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > 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 1580875 AND HEAT TREATED IAW BAC 5602, REV AF 20, AVG 2001. CRACKED LENGTH: 1.5", PN 313T3380-236,
- [SDR ABXA20160614092](https://openairdocs.org/sdr/ABXA20160614092.md): Support Beam · cracked · Jun 14, 2016 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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 NEW BEAM IAW AIR REA 62094. INSTALLED NEW SUPPORT BEAM IAW SRM 51-40-02, PAR 7D. CRACKED LENGTH:
- [SDR ABXA20160610094](https://openairdocs.org/sdr/ABXA20160610094.md): Bushing · galled · Jun 10, 2016 · N787AX · Boeing 767281 · Main Landing Gear Attach Section
  > 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: GAUGE 1.0", PN: 113T1110-2, SWIVEL SUPPORT BUSHING, SIDE STRUT RT MLG, SN:ABXV050. ACFT WAS GROUND
- [SDR ABXA20160606091](https://openairdocs.org/sdr/ABXA20160606091.md): Frame · cracked · Jun 6, 2016 · N787AX · Boeing 767281 · Fuselage Main, Frame
  > 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. REMOVED FASTENERS WERE REPLACED WITH NEW IAW EA53000047-101. CRACKED LENGTH.250", PN: 145T1052-
- [SDR ABXA20141022335](https://openairdocs.org/sdr/ABXA20141022335.md): Beam · corroded · Oct 22, 2014 · N787AX · Boeing 767281 · Trailing Edge Flaps
  > 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-MR. REINSTALLED BEAM IAW REA C057-61249-MR. CORRODED L2, PN 113T1266-25, SN NSN, PART NAME LT IN
- [SDR ABXA20141021336](https://openairdocs.org/sdr/ABXA20141021336.md): Support · corroded · Oct 21, 2014 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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 LOCATION WS 1079.95. ACFT WAS GNDED.
- [SDR ABXA20141021334](https://openairdocs.org/sdr/ABXA20141021334.md): Beam · corroded · Oct 21, 2014 · N787AX · Boeing 767281 · Trailing Edge Flaps
  > 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. REINSTALLED 9 - 10 BEAM & NEW FASTENERS IAW REA C057-6150-MR. CORRODED L2, PN 113T1226-26, SN NSN, PART
- [SDR ABXA20141017320](https://openairdocs.org/sdr/ABXA20141017320.md): Support Fitting · cracked · Oct 17, 2014 · N787AX · Boeing 767281 · Spoilers
  > SPOILER ACTUATOR SUPPORT BRACKET CRACKED IN TWO AT RT WING STATION 700. LOCATED JUST FWD OF FLAP TORQUE TUBE SUPPORT. REMOVED & INSTALLED SERVICEABLE FITTING IAW DWG 113T1421. CRACKED 2 INCHES, PN 113T1566-26, SN NSN, PART NAME FITTING, WING SPAR WINGS, ST
- [SDR ABXA20141016331](https://openairdocs.org/sdr/ABXA20141016331.md): Structure · cracked · Oct 16, 2014 · N787AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > 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. REPAIRED CHORD IAW SB 767-53A0078. CRACKED, LENGTH.5, PN 015T1059-4, PART NAME CHORD, SN NSN, FS
- [SDR ABXA20141013332](https://openairdocs.org/sdr/ABXA20141013332.md): Rib · cracked · Oct 13, 2014 · N787AX · Boeing 767281 · Wing, Rib/Bulkhead
  > 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 INDICATION WITH ROTARY SCAN. REAMED & RE-BUSHINGED HOLE LAW SRM 51-70-16 NDT HOLE NO DAMAGE FOUND.
- [SDR ABXA20141013330](https://openairdocs.org/sdr/ABXA20141013330.md): Splice Plate · corroded · Oct 13, 2014 · N787AX · Boeing 767281 · Wing, Plate/Skin
  > 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, PART NAME SKIN SPLICE, SN NSN, LOCATION WS 450 TO 464. ACFT WAS GNDED.
- [SDR ABXA20141008333](https://openairdocs.org/sdr/ABXA20141008333.md): Splice Plate · cracked · Oct 8, 2014 · N787AX · Boeing 767281 · Nacelle/Pylon, Plate/Skin
  > 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, PN 313T3380-59, PART NAME SPLICE PLATE, SN NSN, STRINGER & WS LOCATION 318.50 TO 318.50. ACFT WAS
- [SDR ABXA20141007321](https://openairdocs.org/sdr/ABXA20141007321.md): Splice Plate · corroded · Oct 7, 2014 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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, PART NAME UPPER SPLICE PLATE, STRINGER & WS LOCATION LES 464. ACFT WAS GNDED.
- [SDR ABXA20141006329](https://openairdocs.org/sdr/ABXA20141006329.md): Rib · cracked · Oct 6, 2014 · N787AX · Boeing 767281 · Wing, Rib/Bulkhead
  > 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, PN 113T1345-22, PART NAME FLAP SUPPORT RIB NR 8, SN NSN, STRINGER & WS LOCATION WS 798.2. ACFT
- [SDR ABXA20141006323](https://openairdocs.org/sdr/ABXA20141006323.md): Fitting · corroded · Oct 6, 2014 · N787AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > 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, 148T904441, 015T1059-3148T2512-7, PART NAME CHORD SPLICE FITTING, TENSION FITTING. CHORD SPLICE, LO
- [SDR ABXA20141003327](https://openairdocs.org/sdr/ABXA20141003327.md): Rib · cracked · Oct 3, 2014 · N787AX · Boeing 767281 · Wing, Rib/Bulkhead
  > 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 HOLES AT 12:00 ARE REPAIRED ON REA B657-61257. CRACKED.01562 INCHES, PN 113T1345-25, PART NAME LT
- [SDR ABXA20141002326](https://openairdocs.org/sdr/ABXA20141002326.md): Rib · cracked · Oct 2, 2014 · N787AX · Boeing 767281 · Wing, Rib/Bulkhead
  > 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 113T1345-19, PART NAME LT WING OTBD FLAP SUPPORT RIB NR 1, SN NSN, STRINGER & WS LOCATION WS 798.2. ACFT
- [SDR ABXA20140930324](https://openairdocs.org/sdr/ABXA20140930324.md): Strap · cracked · Sep 30, 2014 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > 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 INCHES, PN 313T3380-245, PART NAME STRAP, SN N/A, EXACT NACELLE STATION 400, EXACT STRINGER & WS FRO
- [SDR ABXA20140929328](https://openairdocs.org/sdr/ABXA20140929328.md): Fitting · cracked · Sep 29, 2014 · N787AX · Boeing 767281 · Engine Cowling System
  > 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 51-40-5 & SRM 51-40-0. INSTALLED NEW FITTING IAW SRM 51-40-02. CRACKED.500, PN 314T1223, PART NAME
- [SDR ABXA20140928322](https://openairdocs.org/sdr/ABXA20140928322.md): Keelbeam · corroded · Sep 28, 2014 · N787AX · Boeing 767281 · Fuselage Main, Keel
  > 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 B653-61253-MR & SRM 51-40-02. CORRODED L2, PN 145T8612-1, PART NAME WEB, KEEL BEAM, SN NSN, EXACT FS &
- [SDR ABXA20140925325](https://openairdocs.org/sdr/ABXA20140925325.md): Beam · cracked · Sep 25, 2014 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > 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 313T1380-242, PART NAME OTBD BEAM, CRACKED 1.75 INCHES, SN N/A, EXACT STRINGER & WS LOCATION ON MC 310 TO 3
- [SDR ABXA20140925319](https://openairdocs.org/sdr/ABXA20140925319.md): Support · corroded · Sep 25, 2014 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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 CHORD, SN NSN, EXACT STRINGER & WS LOCATION ON NC 273WS TO 275WS. ACFT WAS GNDED.
- [SDR ABXA20140624235](https://openairdocs.org/sdr/ABXA20140624235.md): Unknown · odor · Jun 24, 2014 · N787AX · Boeing 767200 · Air Distribution System
  > 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. CAUSE UNKNOWN.
- [SDR ABXA20130806502](https://openairdocs.org/sdr/ABXA20130806502.md): Battery Pack · inoperative · Aug 6, 2013 · N787AX · Boeing 767281 · Emergency Lighting
  > 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 OK, ACFT WAS GROUNDED.
- [SDR ABXA20121221373](https://openairdocs.org/sdr/ABXA20121221373.md): Angle · cracked · Dec 21, 2012 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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 SRM 51-40-02, ACFT WAS GROUNDED.
- [SDR ABXA20121219370](https://openairdocs.org/sdr/ABXA20121219370.md): Tee Fitting · corroded · Dec 19, 2012 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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, FABRICATED NEW BEAM FROM 7075-T6.063 PO 000975, FABRICATED NEW TEE CLIP FROM EXTRUSION BAC 1505-100609-7015
- [SDR ABXA20121219368](https://openairdocs.org/sdr/ABXA20121219368.md): Structure · cracked · Dec 19, 2012 · N787AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > 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.md): Shim · corroded · Dec 17, 2012 · N787AX · Boeing 767281 · Wing Miscellaneous Structure
  > 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, REMOVED TEE CLIP, FABRICATED NEW BEAM FROM 7075-T6.063 PO 000975, FABRICATED NEW TEE CLIP FROM E
- [SDR ABXA20121217367](https://openairdocs.org/sdr/ABXA20121217367.md): Structure · cracked · Dec 17, 2012 · N787AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > 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 51-70-12, ACFT WAS GROUNDED.
- [SDR ABXA20121214369](https://openairdocs.org/sdr/ABXA20121214369.md): Skin · dented · Dec 14, 2012 · N787AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > 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.md): Beam · cracked · Dec 12, 2012 · N787AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > 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.md): Battery · discharged · Aug 27, 2012 · N787AX · Boeing 767281 · Emergency Lighting
  > WHEN EMERGENCY LIGHT, (FLT DECK) TESTED; IT WOULD ILLUMINATE BRIEFLY AND THEN FADE OUT (OVER FLT DECK DOOR). REMOVED & REPLACED BATTERY FOR EMERGENCY LIGHTING AS PER B767 AMM 33- 51-00-2. OPS CHECK OF SYSTEM GOOD, ACFT WAS GROUNDED.
- [SDR ABXA2011081696](https://openairdocs.org/sdr/ABXA2011081696.md): Web · cracked · Sep 16, 2011 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > 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.md): Tee Fitting · corroded · Sep 7, 2011 · N787AX · Boeing 767281 · Fuselage Main, Frame
  > 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.md): Skin Panel · corroded · Sep 5, 2011 · N787AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > 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.md): Skin Panel · cracked · Sep 5, 2011 · N787AX · Boeing 767281 · Fuselage Main, Plate/Skin
  > 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.md): Failsafe · cracked · Sep 3, 2011 · N787AX · Boeing 767281 · Fuselage Main, Frame
  > 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.

Next page: https://openairdocs.org/deregistered/N787AX-2024-04-09/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N787AX' AND deregistration_id = 'N787AX-2024-04-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N787AX-2024-04-09/reports

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