# Service difficulty reports: N743AX, cancelled Apr 3, 2025 A list on [N743AX, cancelled Apr 3, 2025](https://openairdocs.org/deregistered/N743AX-2025-04-03.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 10 · 458 reports - [SDR 6VAR202503131001](https://openairdocs.org/sdr/6VAR202503131001.md): Skin · corroded · Mar 13, 2025 · N743AX · Boeing 767232 · Fuselage Main, Plate/Skin > CARRIED OUT MAJOR REPAIR OF LH FUSELAGE SKIN FOR CORROSION BEHIND MAIN CARGO DECK SCUFF PLATE AT STA 588-654, STR 19-22LH - [SDR 6VAR202503071001](https://openairdocs.org/sdr/6VAR202503071001.md): Stringer · cracked · Mar 7, 2025 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > DURING AIRCRAFT MAINTENANCE, WAS ACCOMPLISHING HFEC INSPECTIONS AND FOUND CRACK DAMAGE ON THE STRINGERS S-2R & S-8R AT STA 676. THE STRINGERS ARE REPAIRABLE PER BOEING SRM 53-00-03, REPAIR 1; HOWEVER, THE DAMAGE LOCATION IS AFFECTED BY THE IAI FRIEGHTER CONVER - [SDR ABXR2020081100076](https://openairdocs.org/sdr/ABXR2020081100076.md): Spar · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Wing Spar > LT WING UPPER AFT REAR SPAR CORRODED. REPAIRED ON REA 47417REA17 AND NR 0834. - [SDR ABXR2020081100073](https://openairdocs.org/sdr/ABXR2020081100073.md): Skin · damaged · Aug 11, 2020 · N743AX · Boeing 767232 · Wing, Plate/Skin > LT WING LOWER SKIN HAS 34 HOLES THAT ARE OUT OF LIMITS IAW REA 47417REA18. REPAIRED ON REA 47417REA18. REF NR 0927 AND 0472 - [SDR ABXR2020081100075](https://openairdocs.org/sdr/ABXR2020081100075.md): Failsafe · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Main, Structure > STA 539.5, STRINGER 31R FOUND CORROSION ON FAIL SAFE STRAP ON FLC CUT OUT. REPAIRED CORROSION AT STA 539.5 STR 31R ON REA 47417REA09 AND NR 0785. - [SDR ABXR2020081100074](https://openairdocs.org/sdr/ABXR2020081100074.md): Wedge · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Leading Edge Devices > #9 SLAT UPPER TE WEDGE AFT SURFACE IS CORRODED IN NUMEROUS AREAS. REPAIRED DAMAGE ON 39 SLAT TE WEDGE IAW SRM 57-43-02 REPAIR 1,51-70-10 PARA 7, 8, 14, 15, 18, 20, 21, 22. - [SDR ABXR2020081100072](https://openairdocs.org/sdr/ABXR2020081100072.md): Shear Tie · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > SHEAR TIE BETWEEN S33L-S34L AT STA 390 IS CORRODED. REMOVED CORROSION OUT OF LIMITS PER B767 SRM 53-00-07 DETAIL 2. FABRICATED AND INSTALLED NEW PER B767 DWG 114T1223 AND SRM 51-40-02 PARA 4 AND 7. REF NR 0693. - [SDR ABXR2020081100071](https://openairdocs.org/sdr/ABXR2020081100071.md): Support Bracket · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > MAIN DECK CARGO DOOR VIEW PORT CORRODED ON THE MOUNTING FLANGE. REPAIRES MAIN DECK CARGO DOOR VIEW PORT MOUNTING FLANGE I/A/W REA 47417REA20 AND NR 0669. - [SDR ABXR2020081100070](https://openairdocs.org/sdr/ABXR2020081100070.md): Support Beam · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Main, Structure > CORROSION ON FWD SUPPORT BEAM FOR THE FLC DOOR FWD HINGE. CORRODED ON THE UPPER FLANGE JUSTFWD AND ABOVE THE FWD HINGE, JUST INSIDE THE FLC DOOR CUTOUT. REPAIRED THE FWD ACTUATOR SUPPORT BEAM JUST INSIDE FLC DOOR CUTOUT IAW REA 47417REA16 AND NR 0632. - [SDR ABXR2020081000069](https://openairdocs.org/sdr/ABXR2020081000069.md): Stringer · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > CORRODED STR33L AT STA 390. REMOVED AND REPLACED STR 33L AT STA 390 I/A/W REA 47417REA19, B767 SRM 53-00-03 REPAIR 2,51-40-02. - [SDR ABXR2020081100068](https://openairdocs.org/sdr/ABXR2020081100068.md): Shear Tie · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE JUST AFT OF FRAME 742, BETWEEN STR 33L AND STR 34L. REMOVED AND REPLACED SHEAR TIE I/A/W B767 SRM 51-40-02. - [SDR ABXR2020081100067](https://openairdocs.org/sdr/ABXR2020081100067.md): Floor Support · corroded · Aug 11, 2020 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > CORRODED INTERCOSTAL, LOCATED AT BOTTOM OF UPPER CARGO FLOOR BEAM AT STA 764, RBL 12. REMOVED AND REPLACED INTERCOSTAL IAW SRM 53-30-50. - [SDR ABXR2020081000066](https://openairdocs.org/sdr/ABXR2020081000066.md): Window Frame · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Structure > CORROSION ON THE FRAME, OF THE MDCD VIEWING WINDOWS, WINDOWS NR 3, 5, AND 11, ON THE INTERIOR LOWER EDGE OF THE MDCD. MDCD CORROSION OUT OF LIMITS. REPAIRED IAW 47417REA20. - [SDR ABXR2020081000065](https://openairdocs.org/sdr/ABXR2020081000065.md): Stringer · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER 36L AT STRINGER CLIP STA 720. REMOVED CORROSION 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW 15767 SRM 53-00-03 REPAIR 2. REMOVED DAMAGED STRINGER AND INSTALLED REPAIRED SECTION IAW B767 SRM 53-00-07 AND B767 SRM 51-40-02, AND REA 474 - [SDR ABXR2020081000064](https://openairdocs.org/sdr/ABXR2020081000064.md): Stringer · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > CORROSION ON FAILSAFE CHORD, STR 32L AT STA390. REMOVED AND REPLACED DAMAGED S-32L IAW B767 SRM 53-00-03 REPAIR 2. S-32L OUT OF LIMITS IAW B767 SRM 53-00-03 DETAIL II. - [SDR ABXR2020081000063](https://openairdocs.org/sdr/ABXR2020081000063.md): Strut · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Wing Miscellaneous Structure > AIR LOAD STRUT CORRODED AT NR 8 SLAT O/B AUX. TRK. AREA. AIR LOAD STRUT CORRODED OUT OF LIMITS IAW B767 57-41-09 REPLACED STRUT IAW B767 SRM 51-40-02 PARA 4 AND 7. - [SDR ABXR2020081000062](https://openairdocs.org/sdr/ABXR2020081000062.md): Strut · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Wing Miscellaneous Structure > R/W L/E AIR LOAD STRUT AND UPPER L/E FORMER ARE CORRODED NEAR #11 SLAT O/B AUX.TRK. AREA. AIR LOAD STRUT AND UPPER L/E FORMER CORRODED OUT OF LIMITS IAW B767 SRM 57-41-09. REPLACED IAW B767 SRM 51-40-02 PARA 4 AND 7 SEE REVERSE AND PARTIAL WORK SHEET 100 FOR P - [SDR ABXR2020081000061](https://openairdocs.org/sdr/ABXR2020081000061.md): Strut · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Wing Miscellaneous Structure > L/W L/E AIR LOAD STRUT CORRODED UNDER ALL N/P'S AT WS. 785 NR 3 SLAT O/B AUX. TRK. AREA. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B767 SRM 51-41-09 MAX 10% OF OT OF.071 REMAINING.059 REMOVED AND REPLACED AIR LOAD STRUT AT LW WS 785 IAW B767 SRM 51-40- - [SDR ABXR2020081000060](https://openairdocs.org/sdr/ABXR2020081000060.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > SHEAR TIE CORRODED AT BS 1197, STRINGERS 32 - 33R. THE SHEAR TIE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL II. REPLACED THE SHEAR TIE IAW SRM 51-40-02, PARA 4 &7. - [SDR ABXR2020081000059](https://openairdocs.org/sdr/ABXR2020081000059.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > SHEAR TIE CORRODED AT BS 1197, STRINGERS 32-33 LT. REMOVED CORROSION, LOST.011, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. - [SDR ABXR2020081000058](https://openairdocs.org/sdr/ABXR2020081000058.md): Stringer · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > STRINGER 37 LT, BS 1197 WAS CORRODED. THE STRINGER AT BS 1197 WAS ALSO CRACKED, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE STRINGER WITH REPAIR SECTION IAW SRM 53-00-03, REPAIR 2. - [SDR ABXR2020081000057](https://openairdocs.org/sdr/ABXR2020081000057.md): Stringer · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > STRINGER 32 LT, BS 1087 WAS CORRODED ON UPPER SIDE. REPLACED THE SECTION OF THE STRINGER IAW SRM 53-00-03, REPAIR 2, DETAIL IV, AND SRM 51-40-02. - [SDR ABXR2020081000056](https://openairdocs.org/sdr/ABXR2020081000056.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > BS 720 SHEAR TIE CORRODED BETWEEN STRINGERS 36L - 37L. REMOVED CORROSION, ORIGINAL THICKNESS.060, REMOVED.015, REMAINING.045. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. - [SDR ABXR2020081000055](https://openairdocs.org/sdr/ABXR2020081000055.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > BS 720 SHEAR TIE CORRODED BETWEEN STRINGERS 35L-36L. REMOVED THE CORROSION, ORIGINAL THICKNESS.060, REMOVED.015, REMAINING THICKNESS.045, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. - [SDR ABXR2020081000054](https://openairdocs.org/sdr/ABXR2020081000054.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > BS 698 HAD A CORRODED SHEAR TIE BETWEEN STRINGERS 36L AND 37L. THE SHEAR TIE WAS BLENDED IAW 53-00-07, ALLOWABLE 2.0G. THICKNESS.050", REMAINING.040", FOUND OUT OF LIMITS. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02, PARA 4 AND 7. - [SDR ABXR2020081000053](https://openairdocs.org/sdr/ABXR2020081000053.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > STA 698 HAS CORR SHEAR TIE BETWEEN STR 35L AND 36L. REMOVED CORROSION ORIGINAL THICKNESS.050, REMOVED.010, REMAINING.040 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. - [SDR ABXR2020081000052](https://openairdocs.org/sdr/ABXR2020081000052.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > STA 698 HAS CORR SHEAR TIE BETWEEN STR 34L AND 35L. REMOVED CORROSION ORIGINAL THICKNESS.050 REMOVED.010 REMAINING THICKNESS.040 FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-07. REMOVED OLD SHEAR TIE AND REPLACED WITH NEW SHEAR TIE B767 SRM 51-40-02. - [SDR ABXR2020081000051](https://openairdocs.org/sdr/ABXR2020081000051.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > BS 632 HAD A CORRODED SHEAR TIE BETWEEN STRINGERS 39L AND 39R FWD OF LAV SERVICE BOX. REMOVED CORROSION ORIGINAL THICKNESS.052 REMOVED.008 REMAINING.044. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL II. LOCATED AND DRILLED IAW DWG 143T1209 AND INST - [SDR ABXR2020081000050](https://openairdocs.org/sdr/ABXR2020081000050.md): Web · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > CORROSION ON WEB AT BS 390, STRINGERS 29L-28L. REMOVED AND REPLACED WEB AT STA390 STR 29L-28L IAW BOENING DWG 14IT1223, AND SRM 51-40-02. REF CWO 123512-0020 AND AMES REA 47417 FAB 06. - [SDR ABXR2020081000049](https://openairdocs.org/sdr/ABXR2020081000049.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT STA566 STR39L-38L. BLENDED SHEAR TIE. FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-07 FLAG NOTE D AND INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 PARA 7-4. - [SDR ABXR2020081000048](https://openairdocs.org/sdr/ABXR2020081000048.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT STA566 STR38L-37L. REMOVED CORROSION ORIGINAL THICKNESS.050 REMOVED.008 REMAINING.042 TAG # 14483 FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-07 DETAIL II. LOCATED AND DRILLED IAW DWG 143T1209 AND INSTALLED IAW B767 SRM 51-40-02 P - [SDR ABXR2020081000047](https://openairdocs.org/sdr/ABXR2020081000047.md): Floor Support · cracked · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > FLOOR STRINGER SUPPORT IS CRACKED AT THE UPPER RIVET, ON THE FWD SIDE OF FRAME 1417, ABOVE STR.38L, AT FRAME 1417 UPPER CHORD. REMOVED AND REPLACED FLOOR STRINGER SUPPORT ON THE FWD SIDE OF 1417 AT STR 38L IAW B767 SRM 51-40-02 PAR. 7 - [SDR ABXR2020081000046](https://openairdocs.org/sdr/ABXR2020081000046.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT FRAME 1395, BTW STR.37L AND STR.38L. REMOVED DAMAGED SHEAR TIE AND INSTALLED NEW SHEAR TIE FABRICATED FROM 7075T6.063 FROM PO-0145891 TAG#2583486 IAW BOEING DRAWING # 146T1215 AND B767-200 SRM 51-40-02 PARA 4. - [SDR ABXR2020081000045](https://openairdocs.org/sdr/ABXR2020081000045.md): Stringer Splice · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Longeron/Stringer > STRINGER SPLICE 23R IS CORRODED AND CRACKED, BELOW FRAME 1461. REMOVED DAMAGED STRINGER SPLICE ANGLE AND INSTALLED NEW ANGLE FABRICATED ON CWO 123512-0001, IAW DOCUMENT 47417FAB01 AND SRM 51-40-02 PARA 4 AND 7. - [SDR ABXR2020081000044](https://openairdocs.org/sdr/ABXR2020081000044.md): Shear Tie · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE ON THE AFT SIDE OF FRAME 1540, BTW STR.37R AND 38R. CORROSION ON SHEAR TIE ON THE AFT SIDE OF FRAME 1540 BLENDED FOUND TO BE OUT OF LIMITS FABRICATED NEW SHEAR TIE INSTALLED IAW B767 SRM 51-40-02 PAR 4 AND PAR 7. - [SDR ABXR2020081000043](https://openairdocs.org/sdr/ABXR2020081000043.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE LEFT HOR. STAB. AT THE T/E, BTW RIB 3 AND RIB 4. REMOVED CORR. FOUND TO BE OUT OF LIMITS IAW B767 SRM 55-10-01 TABLE I WITH LOWEST POINT AT.120. REPAIRED AREA IAW REA 47417REA04. - [SDR ABXR2020081000042](https://openairdocs.org/sdr/ABXR2020081000042.md): Failsafe · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Fuselage Main, Structure > CORROSION ON FRAME FAIL SAFE CHORD AT STA 390 S33L - S34L. REPAIRED FAIL SAFE CHORD AT STA 390 S37L-S33L I/A/W AMES DOCUMENT 47417REA06. - [SDR ABXR2020081000041](https://openairdocs.org/sdr/ABXR2020081000041.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE RIGHT HOR. STAB., AT STR.3, BTW RIB 4 AND RIB 5.BLENDED AREA IN QUESTION. LOWEST AREA FOUND WAS.130" FOUND TO BE OUT OF LIMITS IAW B767 SRM 55-10-01 FIG 101 DETAIL V. COMPLETED REPAIR INSTRUCTIONS AS - [SDR ABXR2020081000040](https://openairdocs.org/sdr/ABXR2020081000040.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE RIGHT HOR. STAB., AT STR.3, BTW RIB 3 AND RIB 4. BLENDED AREA IN QUESTION. LOWEST AREA FOUND.166" FOUND TO BE OUT OF LIMITS IAW B767 SRM 55-10-01 FIG 101 DETAIL V. COMPLETED REPAIR INSTRUCTIONS AS OU - [SDR ABXR2020081000038](https://openairdocs.org/sdr/ABXR2020081000038.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN ON RIGHT HORIZ STAB AT RIB8 LEADING EDGE. REPAIRED ON 47417REA12. - [SDR ABXR2020081000037](https://openairdocs.org/sdr/ABXR2020081000037.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF SKIN ON RIGHT HORIZONTAL STAB AT RIB 8 TE. REPAIRED ON 47417REA 13. - [SDR ABXR2020081000036](https://openairdocs.org/sdr/ABXR2020081000036.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > RIGHT HORIZONTAL STAB UPPER EXTERIOR SKIN CORRODED AT RIB9 TE. REPAIRED ON 47417REA14. - [SDR ABXR2020081000035](https://openairdocs.org/sdr/ABXR2020081000035.md): Skin · corroded · Aug 10, 2020 · N743AX · Boeing 767223 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERNAL SURFACE OF THE SKIN, ON THE RT HORIZONTAL STAB AT LEADING EADGE AT RIB 13. REPAIRED PER 47417REA15 AND NR 0201. - [SDR ABXR2020081000039](https://openairdocs.org/sdr/ABXR2020081000039.md): Skin · corroded · Aug 4, 2020 · N743AX · Boeing 767232 · Horizontal Stabilizer, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE RIGHT HOR. STAB., AT THE L/E, AT RIB 7. CORROSION OUT OF LIMIT ON UPPER HORZ STAB SKIN 4E AT RIB 7, REPAIRED UPPER SKIN I/A/W AMES DOCUMENT 47417REA11. - [SDR PCSA20205110901](https://openairdocs.org/sdr/PCSA20205110901.md): Hydraulic System · low pressure · May 9, 2020 · N743AX · Boeing 767232 · Hydraulic System, Main > AFTER GEAR DOWN AND FLAPS AT 2" C HYDRAULIC PRESSURE AT 2990 - [SDR ABXR2019020800291](https://openairdocs.org/sdr/ABXR2019020800291.md): Stiffener · corroded · Feb 8, 2019 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > STIFFENER CORRODED. - [SDR ABXR2019020800290](https://openairdocs.org/sdr/ABXR2019020800290.md): Frame · corroded · Feb 8, 2019 · N743AX · Boeing 767232 · Fuselage Main, Frame > RT MAIN FRAME CORRODED (PICKLE FORK). - [SDR ABXR2019020800289](https://openairdocs.org/sdr/ABXR2019020800289.md): Web · corroded · Feb 8, 2019 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > WEB CORRODED. - [SDR ABXR2019020800287](https://openairdocs.org/sdr/ABXR2019020800287.md): Tear Strap · corroded · Feb 8, 2019 · N743AX · Boeing 767232 · Fuselage Miscellaneous Structure > TEAR STRAP CORRODED. - [SDR ABXR2019020500286](https://openairdocs.org/sdr/ABXR2019020500286.md): Skin · corroded · Feb 8, 2019 · N743AX · Boeing 767232 · Fuselage Main, Plate/Skin > SKIN CORRODED. Next page: https://openairdocs.org/deregistered/N743AX-2025-04-03/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 = 'N743AX' AND deregistration_id = 'N743AX-2025-04-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N743AX-2025-04-03/reports --- 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.