JASC 5730
Service difficulty reports · 27,259
Reports filed under 5730 · Wing, Plate/Skin, newest first.
Query with SQL
duckdb -csv -c "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 jasc_code = '5730' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 jasc_code = '5730' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2025050803569Skin · damagedSHIP 684 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589971-14AD REV D. CORRECTIVE ACTION: REF ERA 589971-14AD.SDR CALA2025050604488Skin · damaged(SUPPORT TASK) R/H WING TRAILING EDGE, LOWER WINT SKIN HAS 4EA ELONGATED HOLES BETWEEN WS 278.50 AND 3025.50(AT THE WIGGLE PLATE). TRANSCRIBED FROM HAECO GSO NR 9285003 REPARIED PER EC/RA NO. 5720-03526SDR AALA202505059058Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT WS 3758 AND RIB 7. REPAIRED SKIN PANEL PER EA 362466.SDR AALA202505055989Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL / DOOR 540QB COUNTERSINK FASTENER HOLES. REPLACED AFUEL TANK ACCESS PANEL / DOOR 540QB PER TASK CARD 26C54057007.SDR IPXA2025060885179Skin · delaminatedLEFT WING OUTBOARD TRAILING EDGE HAS MULTIPLE AREAS OF DELAMINATION AND CORROSION. RECEIVED NEW SECTION PANEL,TRAILING EDGE P/N:A5724701724500 BTCH#:0004400445. INSTALLED NEW SECTION PANEL,TRAILING EDGE FROM L/H WING T/E USED RIVETS (45EA) P/N:CR3212-4-05 BTSDR IXXA20250523001Skin Splice · crackedRH WING FIXED LEADING EDGE SKIN PLATE IS CRACKED AT APPROX OFSS 505SDR CALA2025050504453Panel · crackedFIXED LEADING EDGE PANEL P/N 114T2800-275 DAMAGED DURING SLAT RETRACTION FAILURE. FIXED LEADING EDGE PANEL P/N 114T2800-275 REMOVED FOR REPAIR. SENT TO SHOP IN HOUSTON. DURING REMOVAL FOUND TWO DAMAGED GANG CHANNELS (NUT PLATE STRIPS) IDENTIFIED FROM REF/2/ DRSDR AALA202507156297Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT RIB 10 AND THE REAR SPAR AREA. REPAIRED SKIN PANEL PER EA 365112.SDR AALA202507154771Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT RIB 15 AND THE REAR SPAR AREA. REPAIRED SKIN PANEL PER EA 365112.SDR DALA2025050603486Access Panel · worn(LOG 0945409) FUEL TANK PANEL 632NB HAS WEAR MARKS AROUND CUTOUT I84-036. FOUND TO BE WITH LIMITS USING TOOL #0020240 CAL DUE 07/22/25 IAW B737 SRM 57-20-01-2R-1 FIG 203, TREATED AREA AS REQ AT FUEL TANK ACCESS PANEL 632NB IAW B737 SRM 51-20-01.SDR DALA2025050603485Access Panel · worn(LOG 0945396) FUEL TANK PANEL 632PB HAS WEAR MARKS AROUND CUTOUT I84-035. REMOVED AND EVA DAMAGE AT RT WING LOWER SIDE FUEL TANK PANELS REMAINING MATERIAL PANEL 632PB .169 FOUND TO BE WITH LIMITS USING TOOL #0020240 CAL DUE 07/22/25 IAW B737 SRM 57-20-01-2R-1 SDR DALA2025050603484Access Panel · worn(LOG 0945392) FUEL TANK PANEL 632RB LANDING HAS WEAR MARKS I84-034. REMOVED AND EVA DAMAGE AT RT WING LOWER SIDE FUEL TANK PANELS REMAINING MATERIAL PANEL 632RB .169 FOUND TO BE WITH LIMITS USING TOOL #0020240 CAL DUE 07/22/25 IAW B737 SRM 57-20-01-2R-1 FIG 20SDR 2025FA0000483Stiffener · crackedLEFT WING TOP I/B FWD SKIN, AFT STIFFENER CRACKED.SDR 2025FA0000480Stiffener · crackedRIGHT WING FWD LWR I/B SKIN. AFT STIFFENER CRACKED.SDR 2025FA0000479Stiffener · crackedRIGHT WING FWD LWR I/B SKIN. FWD STIFFENER CRACKED.SDR HNAA2025061600420Skin · corrodedF043518 LH MLG BAY FWD AT SPAR II LOWER SKIN CORRODED. REMOVED AND REPLACED LH MLG BAY LOWER FWD SKIN IAW EMB 145 SRM 51-40-02.SDR SWAA2025052766286Access Panel · crackedCRACK COVER OF ACCESS PANEL 551FB AT LT WING 2025-296072<[01] REMOVED AND REPLACED COVER OF ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02-0G-0 GENERAL AND DWG 115A2200. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] JOB COMPLETED.SDR JR2R20250501485Skin · chafedRIGHT HAND WING LEADING EDGE PANEL, EXISTING REPAIR ABOVE PYLON, IS CHAFED OUT OF LIMITS.SDR JR2R20250501484Skin · chafedLEFT HAND WING LEADING EDGE PANEL, EXISTING REPAIR ABOVE PYLON, IS CHAFED OUT OF LIMITS.SDR FDEA202505010698Skin · crackedOPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. RH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM51-40-02-0G, SRM51-40-04-0G AND EA G-5730-T0383252 P1 TITLE:WING-PLASDR FDEA202505010697Skin · crackedOPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51-40-05-0G, SRM51-40-02-0G, SRM51-40-04-0G AND EA G-5730-T0383251 P1, TITLE:WING - PSDR FDEA202505010696Skin · crackedOPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE 01EA CRACK AS MARKED REPAIRED AS PER B777 SRM 51- 40-05-0G,51-40-02-0G,51-40-04-0G REV47.5 AND EA G-5730-T0383099A P1 TITLESDR DALA2025050503425Access Panel · corroded(LOG 0941529) LT WING LOWER SIDE ALL FUEL TANK ACCESS OPENINGS SHOW SIGNS OF FRETTING. REMOVED DAMAGE AT ALL LT WING LOWER SIDE FUEL TANK PANELS FOUND TO BE WITH LIMITS USING TOOL #0020240 CAL DUE 07/22/25 IAW B737 SRM 57-20-01-2R-1.SDR AALA202505026563Skin · crackedAIRCRAFT WAS NOT GROUNDED: LONG CRACK IN SHEET METAL ON TOP OF RIGHT WING INBOARD OF GROUND SPOILER. DECESION WAS MADE TO INSPECTED THE LONG CRACK IN SHEET METAL ON TOP OF RIGHT WING INBOARD OF GROUNDSPOILER . FOUND TO BE THE PRODUCTION SEAM. OK FOR SERVICE.SDR CALA2025050204409Skin · damagedRII INSPECTION REQUIRED RH NO.2 LOWER WING SKIN REQUIRES REPLACEMENT DUE TO NON-REPAIRABLE DAMAGES AT LOCATION WS667.5-WBL616.75. INITIAL DISCREPANCY L/P 4003188 CREATED 2/27/2025. UPDATE TO INDICATE WING LOWER SKIN AND STRINGER REPLACEMENT IS A MAJOR REPAIR.SDR DALA2025050103358Skin · damagedLEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137 (7 EA) MARKED AS A1 THRU A7. DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD REV 0 PRI REV 7 SECTION IV STEP # 5, #6, AND #7. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941448SDR IXXA20250430004Skin · wornL WING WINGLET L/E PANEL HAS 1 FASTENER HOLE THAT IS OVER SIZEDSDR WRXR20250430001Skin Panel · dentedPANEL 622AR HAS 6 GOUGES COVERED WITH PAINT FROM WS 88 TO WS 126. GOUGE #1- 1"LONG, .05"WIDE, .004" DEEP. GOUGE #2- 1.5"LONG, .05" WIDE, .004" DEEP. GOUGE #3- 4.5" LONG, .05"WIDE, .005"DEEP. GOUGE #4- 14" LONG, .05"WIDE, .005" DEEP. GOUGE #5- 1.2" LONG, .05" WSDR AALA202508269814Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TOP SKIN LOWER SURFACE LEVEL RIB 14 ON RH WING L= 4.214 INCH W= 1.954 INCH D= 0.114 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON TOP SKIN LOWER SURFACE BTW RIB 13 TO RIB 15 ON RH WING IAW EA# 364937 DWG R572-58616 SDR REXA2025052900624Access Panel · crackedCRACK ON SKIN AND STTIFENER ON ACCESS PANEL 172CR IN REF. TO TASK CARD 900-57-510-700. CRACK ON SKIN AND STTIFENER ON ACCESS PANEL 172CR WAS REPAIRED REO 670-53-82-430 REV: - -SDR AALA202507168706Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN SKIN PANEL UPPER SURFACE BETWEEN RIB 5 AND RIB 6 AT STRINGER 17. REPAIRED SKIN PANEL PER EA 365114.SDR SWIA20250715427Skin · chafedCENTER WING, LOWER WING PLANK HAS MINOR CHAFE DAMAGE UNDER PANEL 193AB, L/H AND R/H SIDES AT MLG WHEEL WELL. (C-CHECK RO 07/15/2025)REPAIRED CHAFE DAMAGE AT LH AND RH WING PLANKS UNDER PANEL 193AB IAW REO 601R-57-21-880-REV D DATED 2017/03/06. COMPLETED TASK SDR AALA202507159555Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT RIB 19 AND THE FRONT SPAR AREA. REPAIRED SKIN PANEL PER EA 365114.SDR 2025FA0000325Skin · corrodedFOUND SEVER CORROSION ON L/H WING, MAIN FLAP UPPER SURFACE, REAR SPAR UPPER CHORD, NEAR IFS 125.5.SDR IPXA2025052569682Skin · crackedLH WING, UPPER SKIN, BETWEEN RIB 16 TO RIB 18 AREA HAS A CRACK. VERIFIED STEP #29 ACCOMPLISHED STEP #13 IN PRELIMINARY 2 E.A.# 300-5751-27-A3942.SDR 2025F00105Access Panel · leakingDURING POSTFLIGHT INSP FUEL LEAKAGE WAS FOUND AT RIT TANK TOP SIDESDR AALA202504305072Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT WING UPPER SKIN AT RIGHT WING BL 273.30. REPAIRED SKIN PER EA 364114.SDR VNAA20250529031Access Panel · elongatedELONGATED HOLE ON SETTLEMENT AREA OF ACCESS PANEL 684CB AT RH INB FLAP. ELONGATED HOLE ON SETTLEMENT AREA OF ACCESS PANEL 684CB AT RH INB FLAP WAS REPAIRED PER REO 690-57-52-527 REV.--. (THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTS FROM THE ISSUE DATE OFSDR SWIA20250428004Skin · damagedFASTENER HOLE DAMAGED/ELONGATED (ORIGINAL FASTENER NAS1581F3R9) THROUGH STACK UP AT APPROX. RH WS 75.27 WING SKIN AND INBD T/E EDGE MEMBER 601R10225-14 MEMBER - SECOND SCREW HOLE INBOARD OF FLAP ACTUATOR. (FILED CLOSED)COMPLIED WITH REO 601R-57-51-1067 REV -- SDR CALA2025042804263Panel · gougedL/W L/E SLAT #4 PANEL AFT OF ACTUATOR PANEL DEEP GOUGE I/B END REF AAR A/R 9954724 ESFR ENTRY. L/W L/E SLAT #4 PANEL AFT OF ACTUATOR PANEL DEEP GOUGE I/B END REF AAR A/R9954724 ESFR ENTRY. REF ESFR NO.800SDR AALA202504258163Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540HB COUNTERSUNK FASTENER HOLES. REPLACED ACCESS PANEL PER TASK CARD 26C54057007.SDR JR2R20250424289Panel · chafedLEFT HAND WING PANEL, 516QT, CHAFED IN MULTIPLE PLACES AREAS OUT OF LIMITS.SDR FDEA202504230629Skin · crackedOPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 02EA CRACKS AS MARKED. RH WING UPPER SKIN WBL262 #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-50-02-0G, 51-40-02-0G, 51-10-01-0G, 51-20-06-0G, 51-40-05-0G, 51-40-08-0G, 51-20-SDR IPXA2025050888488Skin · crackedRIGHT WING BEHIND SLAT # 9, FIXED LEADING EDGE HAS A CRACK.REMOVED FIXED LEADING EDGE SKIN AT RIGHT WING BEHIND SLAT # 8 AND #9 FOR REPAIR FROM OSS 562 TO OSS 696 PER SRM 51-40-02. REMOVED DAMAGE AND PREPARED AREA IAW B757-200PF SRM 51-70-17-0G-0 PAR. 4.BONDEDSDR DALA2025042403213Skin · damagedSHIP 6712 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT WINGS / UPPER SURFACE / LH FWD DRAG FITTING, HOLE LOCATION #8 / CRACK REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 625378-14AD. CORRECTIVE ACTION: REF ERA 625378-14AD. (0927025)SDR UIEA2025042100558Skin · crackedL/H WING, INBOARD LEADING EDGE SKIN PANEL, KRAS 206, 1 (E.A.) HOLE WITH CRACK INDICATION. CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS.(<P>PERFORMED LH WING AT KRAS 206 INBD LEADING EDGE SKIN PANEL FASTENERS OVERSIZE HOLE REPAIR IAW COO-EO-2025-2221-R00SDR UIEA2025042100559Skin · crackedR/H WING, INBOARD LEADING EDGE SKIN PANEL, KRAS 206, 1 (E.A.) HOLE WITH CRACK INDICATION. CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS.(<P>PERFORMED RH WING AT KRAS 206 INBD LEADING EDGE SKIN PANEL FASTENERS OVERSIZE HOLE REPAIR IAW COOPESA COO-EO-2025SDR AALA202508269041Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION UPPER SURFACE, TOP SKIN BETWEEN RIB 13 TO RIB 14 ON RH WING, CORROSION MEASURES ARE: L= 3.338 INCH; W= 2.143 INCH; D= 0.003 INCH. MAINTENANCE REPAIRED SKIN PANEL IAW EA 364937.SDR AALA202507222472Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT WX3494.5 BETWEEN RIBS 7 AND 9. REPAIRED SKIN PANEL PER EA 364615.SDR AALA202507186680Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR SPAR TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 364615.
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