# Service difficulty reports: Boeing 747-428 A list on [Boeing 747-428](https://openairdocs.org/model/boeing-747-428.md). Newest first. General aviation reporting is voluntary. Page 1 of 10 · 495 reports - [SDR U2RA2026091100059](https://openairdocs.org/sdr/U2RA2026091100059.md): Bottle · low pressure · Sep 11, 2026 · N952CA · Boeing 747428 · Escape Slide > UPPER DECK DOOR SLIDE INFLATION CYLINDER PRESSURE LOW. REMOVED AND REPLACED DOOR SLIDE ASSEMBLY. - [SDR U2RA2026090700056](https://openairdocs.org/sdr/U2RA2026090700056.md): Wire · not reported · Sep 7, 2026 · N756CA · Boeing 747428 · Light System Wiring > DEVIATIATED FROM SERVICE BULLETIN FOR FRAME NOT BEING INSTALLED ON AIRCRAFT. REPAIRED AND FOLLOWED INSTRUCTIONS FORM BOEING MUA-MUA-26-13C - [SDR U2RA2026081700049](https://openairdocs.org/sdr/U2RA2026081700049.md): Circuit Card · faulted · Aug 12, 2026 · N952CA · Boeing 747428 · Fire Detection > ON GROUND - ERRONEOUS FIRE WARNINGS - CLEANED AND RESEATED AFOLTS INTERFACE CARD. SYSTEM OPERATION NORMAL PER AIRCRAFT MAINTENANCE MANUAL 26-10-01. - [SDR U2RA2026090700055](https://openairdocs.org/sdr/U2RA2026090700055.md): Structure · cracked · Aug 6, 2026 · N756CA · Boeing 747428 · Fuselage Main, Structure > DURING FCD 744-53-0021 OPEN-HOLE HFEC INSPECTION. CRACK SIGNAL INDICATION AT STA 2590, RT UPPER 1EA HOLE. (CHORD) PER NDTM PART 6, 51-00-00 PROCEDURE 16 AND SB 747-53A2427 REV 7. INSTALLED REPAIR STRAPS ON THE BS 2598 FORWARD INNER CHORD FRAME SUPPORT PER SR - [SDR U2RA2026090700051](https://openairdocs.org/sdr/U2RA2026090700051.md): Tension Tie · cracked · Aug 6, 2026 · N756CA · Boeing 747428 · Fuselage Main, Structure > DURING FCD 744-53-0025 OPEN HOLE HFEC INSPECTION 1EA HOLE CRACK INDICATION FOUND AT STA 1180 LT TENSION TIE AFT DOUBLER AND FWD CHANNEL. INSTALLED FRAME DOUBLER AND FWD CHANNEL REPAIR PART ON BS 1180 LT TENSION TIE IAW SRM 51-40-02, DWG 65B 01752, MUA-26-0 - [SDR U2RA(20260907)000](https://openairdocs.org/sdr/U2RA(20260907)000.md): Tension Tie · cracked · Aug 6, 2026 · N756CA · Boeing 747428 · Fuselage Main, Structure > 2 CRACK INDICATION FOUND (FWD CHANNEL 1EA HOLE AND FRAME AREA 1EA HOLE) DURING OPEN-HOLE HFEC INSPECTION OF THE TENSION TIE AT STA 1120, LEFT HAND SIDE. PER FCD 744-53-0025 R3. REPAIR: REAMED CRACK SIGNAL INDICATION HOLE ON BS 1120 LT FRAME WEB ONLY. UP TO 0. - [SDR U2RA2026072100045](https://openairdocs.org/sdr/U2RA2026072100045.md): Frame · cracked · Jun 29, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > DURING SCHEDULED INSPECTION FOUND 2 CRACK HOLES AT R5 DOOR INNER CHORD STA 2231 S-19. PERFORMED CLASS B REPAIR IAW SRM 53-60-15, REPAIR 2. - [SDR U2RA2026070800032](https://openairdocs.org/sdr/U2RA2026070800032.md): Skin · dented · Jun 25, 2026 · N919CA · Boeing 747428 · Trailing Edge Flaps > DURING AIRCRAFT C-CHECK IN ICN (INCHEON, SOUTH KOREA) SHARP TECHNICS K MAINTENANCE DISCOVERED CHAFE DAMAGE ON THE UPPER SURFACE OF THE INBOARD TRAILING EDGE AFT FLAP OUTER SKIN PANEL P/N 65B02077-508. PERFORMED PERMANENT REPAIR IAW FLIGHT VEHICLES CONSULTING, - [SDR U2RA2026072100046](https://openairdocs.org/sdr/U2RA2026072100046.md): Frame · cracked · Jun 24, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > CRACK FOUND AT RH STA 1140 LH TENSION TIE FRAME. REPAIRS COMPLETED PER BCS CASE 06373559. - [SDR U2R2026F00000](https://openairdocs.org/sdr/U2R2026F00000.md): Frame · cracked · Jun 19, 2026 · N919CA · Boeing 747428 · Fuselage Miscellaneous Structure > DURING OPEN HOLE INSPECTION, DETECTED DEFECT SIGNAL AT FRAME WEB BS 1265. PERFORMED REPAIR IAW NAL FCD 744-53-0014 AND DWG 624U0060. - [SDR U2RA2026071100033](https://openairdocs.org/sdr/U2RA2026071100033.md): Skin · damaged · Jun 19, 2026 · N919CA · Boeing 747428 · Fuselage Main, Plate/Skin > .LIGHTNING-STRIKE DAMAGE FOUND ON THE FUSELAGE SKIN AT STA 225, STRINGER S-23R. PERFORMED REPAIR IAW BOEING BCS CASE MUA-MUA-26-0085. DATA APPROVED BY FAA FORM 8100-9 DATED 06/28/2026. - [SDR U2RA2026072100044](https://openairdocs.org/sdr/U2RA2026072100044.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > CRACK FOUND IN OPEN HOLE INSPECTION AT RT STA 1120 TENSION TIE FRAME WEB 65B01749-22. REPAIRS COMPLETED PER BOEING BCS CASE 06372730 - [SDR U2RA2026072000041](https://openairdocs.org/sdr/U2RA2026072000041.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > A CRACK DAMAGED WAS FOUND ON THE FRAME WEB AT STA 1160 AND BETWEEN S-9R- 10R WHILE PERFORMING SERVICE BULLETIN 747-53A2702 REV 02. PERFORMED CLASS B REPAIR PER CASE 06372691 - [SDR U2RA2026072000040](https://openairdocs.org/sdr/U2RA2026072000040.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > DURING OPEN HOLE INSPECTION, CRACK FOUND AT BS 800 BETWEEN S-16R & S-17R. PERFORMED PERMANENT REPAIR AIW BOEING BCS MUA-MUA-26-0081-09B AND DWG 65B26468. - [SDR U2RA2026072000039](https://openairdocs.org/sdr/U2RA2026072000039.md): Frame · cracked · Jun 17, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > DURING OPEN HOLE INSPECTION, 2 CRACKS FOUND AT BS800 BETWEEN S-15L TO S-17L. PERFORMED CLASS B REPAIR IAW BCS CASE # 06372411 - [SDR U2RA2026072100047](https://openairdocs.org/sdr/U2RA2026072100047.md): Tension Tie · cracked · Jun 14, 2026 · N919CA · Boeing 747428 · Fuselage Main, Attach Fittings > CRACK FOUND DURING OPEN HOLE INSPECTION AT L/H STA1180 TENSION TIE FWD CHANNEL. PERFORMED CLASS B REPAIR IAW SRM 53-40-30-2R-2. - [SDR U2RA2026071900038](https://openairdocs.org/sdr/U2RA2026071900038.md): Tension Tie · cracked · Jun 11, 2026 · N919CA · Boeing 747428 · Fuselage Main, Attach Fittings > OPEN HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING STA 1140 R/H TENSION TIE. REPAIR COMPLETED PER BCS MESSAGE 06370241 INSPECTION THRESHOLD 20,811 TOTAL FLIGHT CYCLES. - [SDR U2RA2026051200028](https://openairdocs.org/sdr/U2RA2026051200028.md): Longeron · cracked · Apr 19, 2026 · N952CA · Boeing 747428 · Fuselage Main, Structure > 2EA CRACK INDICATON FOUND AT BS2598 BULKHEAD R/H S-11R LONGERON P/N 65B02522-4 PER BOEING SR MUA-MUA-26-0026-22B REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12-2026 AND PER BCS 202603210023-0016 - [SDR U2RA2026051200026](https://openairdocs.org/sdr/U2RA2026051200026.md): Frame · cracked · Apr 10, 2026 · N919CA · Boeing 747428 · Fuselage Main, Frame > 1EA CRACK FOUND AT BS2598 BULK HEAD RHS FRAME SUPPORT HOLE D AS PER BOEING SR MUA-MUA-26-0022-07B REPAIRED CARRIED OUT PER BOEING 8100-9 DATED MAY 12 2026 AND PER BOEING BCS 202603210023-0016 - [SDR U2RA2026051200027](https://openairdocs.org/sdr/U2RA2026051200027.md): Frame · cracked · Apr 1, 2026 · N952CA · Boeing 747428 · Fuselage Main, Frame > 1EA CRACK FOUND AT BS2598 BULKHEAD RHS OUTER CHORD HOLE C PER BOEING SR MUA-MUA-26-0022-07B REPAIR CARRIED OUT PER BOEING 8100-9 DATEED MAY, 12,2026.REFF BOEING BCS 202603210023-0016 - [SDR U2RA2026051200019](https://openairdocs.org/sdr/U2RA2026051200019.md): Stringer · cracked · Mar 26, 2026 · N952CA · Boeing 747428 · Fuselage Main, Longeron/Stringer > FCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA R/H 1160 AND STRINGER 10R REPAIR CARRIED OUT PER 8100-9 DATED 04/28/2026 REF BOEING COMMUNICATION SYSTEM MESSAGE NUMBERS FOR CASE # 06320986 - [SDR U2RA2026051200024](https://openairdocs.org/sdr/U2RA2026051200024.md): Frame · cracked · Mar 21, 2026 · N952CA · Boeing 747428 · Fuselage Main, Frame > ONE CRACK FOUND AT FRAME SUPPORT OF 747 SSID REV. H ITEMS F­49G ON THE RHS AREA OF THE HINGE FITTING. PER BOEING SR MUA­MUA­26­0026­03B. REPAIR CARRIED OUT PER BOEING 8100­9 DATED MAY 13 2026 AND REF BCS 202603130057­009 - [SDR U2RA2026051200025](https://openairdocs.org/sdr/U2RA2026051200025.md): Stringer · cracked · Mar 18, 2026 · N952CA · Boeing 747428 · Fuselage Main, Longeron/Stringer > FCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA L/H 1160 AND STRINGER 10L REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12, 2026 REF BCS 0632095 - [SDR U2RA2026032500002](https://openairdocs.org/sdr/U2RA2026032500002.md): Lamp · inoperative · Mar 18, 2026 · N919CA · Boeing 747428 · Emergency Lighting > U/D EMEGENCY LIGHT NO ON QTY 3 EA. REPLACED THE LAMP AND OPERATION CHECK PER AMM 33-51-07 FOUND NORMAL - [SDR U2RA2026051200018](https://openairdocs.org/sdr/U2RA2026051200018.md): Tension Tie · cracked · Mar 16, 2026 · N952CA · Boeing 747428 · Fuselage Main, Structure > OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS AT 1120 R/H TENSION TIE. REPAIR CARRIED OUT PER 8100=9 DATED 05/08/2026 REFF BOEING COMMUNICATION CASE 063200880 - [SDR U2RA202605000011](https://openairdocs.org/sdr/U2RA202605000011.md): Fastener · broken · Mar 10, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure > LOCK FASTENER HEAD BROKEN AT TENSION TIE ATTACH FRAME LOCATED AT BS 1220 RT AND STRINGER 10R - [SDR U2RA2026051200017](https://openairdocs.org/sdr/U2RA2026051200017.md): Doubler · cracked · Mar 9, 2026 · N952CA · Boeing 747428 · Empennage Structure > FINDING 002002 DOCUMENT FCD 744-53-0057-DURING C-CHECK 0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR WAS COMPLTED PER FAA 8100-9 DATED 0/21/2006 ON BOEING SERVICE REQUEST 202603060065-0011. - [SDR U2RA202604110007](https://openairdocs.org/sdr/U2RA202604110007.md): Doubler · cracked · Mar 9, 2026 · N952CA · Boeing 747428 · Horizontal Stabilizer, Plate/Skin > 0.7" CRACK HAS EXTENDED FROM THE STOP HOLE OF THE PREVIOUS CRACK AT R/H STABILIZER UPPER LOBE DOUBLER. REPAIR COMPLETED PER:CASTLE ID: 202603060065: BOEING 8100-9 ISSUED DATED 04/21/2026. REF ID 202603060065-0011 - [SDR U2RA202604110006](https://openairdocs.org/sdr/U2RA202604110006.md): Web · cracked · Mar 3, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure > CRACK FOUND ON FORWARD FUSELAGE WEB OF THE NOSE GEAR WELL AT STRINGER 26, BS 160-180 CORRECTIVE ACTION: CAT B. REPAIR PER SRM. REINSPECT DUE AT 33,018 CYCLES - [SDR U2RA2026033100003](https://openairdocs.org/sdr/U2RA2026033100003.md): Floor Support · cracked · Mar 3, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure > AFT CARGO INTERCOSTAL CRACK AT STA 1940 TO STA 1960, LBL77 PERFORMED REPAIR IAW SRM 51-70-13 R1 - [SDR U2RA202604280010](https://openairdocs.org/sdr/U2RA202604280010.md): Tension Tie · cracked · Mar 2, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure > OPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING BS 1180LT - 1140 RT. - [SDR U2RA2020405000005](https://openairdocs.org/sdr/U2RA2020405000005.md): Web · cracked · Mar 2, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure > CRACK FOUND ON FORWARD FUSELAGE WEB OF NOSE GEAR WELL AT STRINGER S-26 STA 140-160 WL 205 R&R WEB PART NUMBER 65B01870U243 IAW SRM 51-40-02 - [SDR U2RA2026051100015](https://openairdocs.org/sdr/U2RA2026051100015.md): Tension Tie · cracked · Feb 26, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous Structure > OPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING STA 1180 L/H STA 1140 R/H. REPAIR COMPLETED PER BCS MESSAGE NUMBER 06316150 INSPECTION THRESHOLD 21,108 TOTAL FLIGHT CYCLES - [SDR U2RA2026051100014](https://openairdocs.org/sdr/U2RA2026051100014.md): Frame · cracked · Feb 25, 2026 · N952CA · Boeing 747428 · Fuselage Main, Frame > WHILE IN C CHECK - PERFORMED SURFACE HFEC INSPECTION OF FCD 744-53-0017 R2 A 1 INCH CRACK WAS FOUND ON CHORD BETWEEN S-37R AND S-38R. REPAIR PERFORMED PER BOEING BCS MUA N952CA / 25238 FRAME CRACK BS 1140 RH, RBL 80 / WL 330. - [SDR 2026FA0000189](https://openairdocs.org/sdr/2026FA0000189.md): Skin · punctured · Feb 18, 2026 · N903AR · Boeing 747428 · Cargo/Baggage Doors > DURING INSPECTION OF AFT CARGO DOOR, FRAME FOUND PUNCTURED HOLE AND CRACK ON AFT SECTION OF CARGO DOOR SKIN. - [SDR U2RA2025082100020](https://openairdocs.org/sdr/U2RA2025082100020.md): Skin · cracked · Aug 22, 2025 · N919CA · Boeing 747428 · Fuselage Main, Plate/Skin > DURING A CHECK AT RKSI, WHILE PERFORMING FCD 744-53-0076 R2, 250 FLIGHT CYCLE (FC) REPETITIVE INSPECTIONS FOR SCRIBE LINE FINDINGS ON SB 747-53A2563 LIMITED RETURN TO SERVICE (LRTS) PROGRAM, IT WAS DISCOVERED THAT SKIN PANEL 33L WITH P/N: 65B04135-343 HAVE 02 - [SDR U2RA2025013100011](https://openairdocs.org/sdr/U2RA2025013100011.md): Skin · deformed · Jan 31, 2025 · N729CA · Boeing 747428 · Fuselage Main, Plate/Skin > DURNING C CHECK IN HAECO SECTION 41 FUSELAGE SKIN, BETWEEN STA 488 AND STA 520 AND BETWEEN 22L AND STR -257 WAS FOUND WITH BLENDOUT DENT DAMAGE - [SDR U2RA2025010100013](https://openairdocs.org/sdr/U2RA2025010100013.md): Skin · dented · Jan 1, 2025 · N729CA · Boeing 747428 · Fuselage Main, Plate/Skin > DURING AIRCRAFT HEAVY CHECK IN XMV (XIAMEN, CHINA), HAECO MAINTENANCE DISCOVERED (2 EA.) DENTS ON THE SECTION 46 FUSELAGE SKIN. SEE FIGURE 1 FOR DETAILS. THE DAMAGE WAS EVALUATED PER REF /A/ AND FOUND TO BE BEYOND PUBLISHED LIMITS (A/Y <30). THE SKIN IS MADE F - [SDR U2RA2024090600054](https://openairdocs.org/sdr/U2RA2024090600054.md): Engine · faulted · Aug 30, 2024 · N919CA · Boeing 747428 · Engine (Turbine/Turboprop) > DURING TAKE-OFF ROLL, SHORTLY AFTER SELECTING "TOGA", ENGINE NUMBER 4 SHOWED RED EGT INDICATION AS AIRCRAFT VEERED SIGNIFICANTLY TO THE LEFT. LOW SPEED (APPROXIMATELY 40 KTS.) RTO CARRIED OUT. ENGINE NUMBER 4 WAS DETERMINED UNSERVICEABLE AND REPLACED PRIOR T - [SDR U2RA2024081500022](https://openairdocs.org/sdr/U2RA2024081500022.md): Power Supply · no test · Aug 15, 2024 · N919CA · Boeing 747428 · Emergency Lighting > WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTS, POWER PACK AND ATTENDANT SWITCH BY USING THE EMERGENCY LIGHT PILOT CONTROL, EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER POSITION M5056 STA LBL 6 - [SDR U2RA2024081500021](https://openairdocs.org/sdr/U2RA2024081500021.md): Power Supply · failed · Aug 15, 2024 · N919CA · Boeing 747428 · Emergency Lighting > WHILE PERFORMINNG OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, POWER PACKS, AND ATTENDANT PANEL SWITCH BY USING THE EMERGENCY LIGHT PIPLOT CONTROL, EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER TO POSITON M5055 STA 610 LBL 88. - [SDR U2RA2024081520](https://openairdocs.org/sdr/U2RA2024081520.md): Power Supply · no test · Aug 15, 2024 · N919CA · Boeing 747428 · Exterior Lighting > WHILE PERFORMING OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, POWER PACKS, AND ATTENDANT PANEL SWITCH BY USING THE EMERGENCY LIGHT PILOT CONTROL. EMERGENCY LIGHT POWER SUPPLY CAN'T SUPPLY POWER POSITION - M5057 STA 717 LBL 8 - [SDR U2RA2024081519](https://openairdocs.org/sdr/U2RA2024081519.md): Seat Track · cracked · Aug 15, 2024 · N919CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings > FOUND CRACK ON SEAT TRACK BETWEEN STA 980 AND STA 1000 LBL 75 (MAIN DECK) - [SDR U2RA2004081518](https://openairdocs.org/sdr/U2RA2004081518.md): Seat Track · cracked · Aug 15, 2024 · N919CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK BETWEEN STA 980 AND STA 1000 RBL 75 FOUND CRACK ON SEAT TRACK. - [SDR U2RA2004081517](https://openairdocs.org/sdr/U2RA2004081517.md): Seat Track · cracked · Aug 15, 2024 · N919CA · Boeing 747428 · Fuselage, Seat/Cargo Attach Fittings > FOUND CRACKON SEAT TRACK FWD CARGO STA 580, RBL 24 - [SDR U2RA2024081500023](https://openairdocs.org/sdr/U2RA2024081500023.md): Pressure Deck · cracked · Aug 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Bulkhead > DURING C CHECK IN GMF, FOUND CRACK ON SKIN AT LH WLG W/W CANTED PRESSURE DECK STA 1241LBL 11.33 CATEGORY B REPAIR WAS ACCOMPLISED IN ACCORDANCE WITH BOEING MESSAGE BOE MUA-MUA 24-0122 - [SDR U2RA202406040146](https://openairdocs.org/sdr/U2RA202406040146.md): Skin · cracked · Jun 4, 2024 · N952CA · Boeing 747428 · Fuselage Main, Structure > DURING C CHECK IN GMF FOUND CRACK ON SKIN AT LH WLG CANTED PRESSURE DECT STA 1241 LBL 11.33. CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH BOEING MESSAGE NUMBER- BOE-MUA-24-0122 - [SDR U2RA2024081500040](https://openairdocs.org/sdr/U2RA2024081500040.md): Skin · damaged · Jun 1, 2024 · N952CA · Boeing 747428 · Fuselage Main, Plate/Skin > FOUND RIVET HOLES ELOGATED ON SKIN 2700 LH SIDE AFTER MEASURMENT RIVET HOLES DIAMETER BETWEEN.280 INCH UP TO.320 INCH - [SDR U2RA2024081500039](https://openairdocs.org/sdr/U2RA2024081500039.md): Support Frame · corroded · Jun 1, 2024 · N952CA · Boeing 747428 · Aerodynamic Fairings > DURING MAINTENANCE C CHECK AT GMF FOUND LOWER FUSALAGE STA 1000 CENTER TO RH SIDE SUPPORT FRAME FOR BODY FAIRING CORRISON. REAPIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-70-12 (REV59/20FEB2024) AND WAS A CAT A REPAIR. - [SDR U2RA2024081500038](https://openairdocs.org/sdr/U2RA2024081500038.md): Fairing · cracked · Jun 1, 2024 · N952CA · Boeing 747428 · Ailerons > WHILE PERFORMING C CHECK RH WING O/B AILERON UPPERSURFACE L/E FAIRING CRACK POS O/B SIDE REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH SRM 57-60-01 REPAIR 1 (REV59 20FEB2024) Next page: https://openairdocs.org/model/boeing-747-428/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 aircraft_model_key = '747428' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-747-428/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.