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 SWI2025F00255Skin · corrodedRIGHT WING UPPER SURFACE, MATING SURFACE FOR PANEL 640AT HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 2/27/2025) REMOVED CORROSION FROM THE MATING SURFACE FOR PANEL 640AT ON THE R/H UPR WING SURFACE PER CRJ200SRM 51-21-06 AND REPAIRED PER REO 6SDR IPXA2024121990371Skin · damagedL WING PANEL 561GB LEADING EDGE HAS SEPARATION WITH RIVETS PULLED THROUGH. MARKED WITH TAPE. REPLACED DAMAGED WIGGLE PLATES WITH 113T1663Y1013, 113T1663-1037 AND 113T1663Y1009 IAW BOEING SRM 51-40-02.SDR WRXR20241218002Skin · chafedCUSTOMER REPORTS QTY (3) BLENDED AREAS OF CHAFE DAMAGE TO AFT WING PLANK LOWER SKIN (DWG CC670-10046, AL ALY 7475-T7351, 0.250”,0.270”,0.300” AND 0.350” NOM. THK. +/-0.005” AT BLENDED AREAS) BTW STR10L – AUX SPAR DATUM AND WS48.95-WS68.00. BLENDING OF DAMAGE WSDR SWI2025F00226Skin · chafedLH LOWER WING PLANK CHAFFED ON TRAILING EDGE WHERE MLG BAY FORWARD FAIRING (193AB) MOUNTS (C-CHECK RO 2/27/2025) BLENDED AND REMOVED CHAFE FOUND TO BE ACCEPTABLE REF REO NO. 601R-57-21-880 REV -D DATE 2017/03/06. COMPLIED WITH TASK CARD 51-900-1003-SKSDR SWI2025F00225Skin · chafedRH LOWER WING PLANK CHAFFED ON TRAILING EDGE WHERE MLG BAY FORWARD FAIRING (193AB) MOUNTS (C-CHECK RO 2/27/2025) PERFORMED REPAIR OF RH LOWER WING PLANK CHAFFED ON TRAILING EDGE WHERE MLG BAY FORWARD FAIRING (193AB) MOUNTS REF REO NO. 601R-57-21-880 REVSDR CALA2024121803112Skin · corrodedRIGHT WING FRONT SPAR, CENTER FUEL TANK LOWER SKIN HAS CORROSION, 13 INCHES INBOARD OF TERMINAL FITTING AT BS 540 AND RBL 52 UNDER DRAG LINK. AN INTERNAL HFEC INSPECTION OF THE WING CENTER SECTION LOWER OF EC/RA 5711-0207 ON OR BEFORE THE AIRCRAFT REACHING 25SDR DALA2024121711773Skin · damaged-AD- FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS=164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A. #FC5720-01103-01A. REFER TO NRC 0714281 FOR COMPLETION OF ERA 622950-14AD. NO LEAKS NOTED. OK FOR SESDR DALA2024121711772Skin · damaged-AD- REF TO LOG PAGE #6930830. ORIGINAL WRITE UP: FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS+164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A #FC5720-0110-01A. ALL WORK COMPLETED PER ERA 622950AD RESDR WRXR20241216005Panel · gougedFOUND GOUGING ON WING ON FWD SIDE OF FAIRING PANEL 592AB TO WING MATING SURFACE. BLENDED GOUGES ON LOWER LH WING SKIN AT AREAS C/T PANEL 592AB IAW CRJ700 SRM 51-12-00-001-001-A01. ROTO-PEENED REWORKED AREA IAW CRJ700 SRM 51-24-11. ALODINE AND PRIMED AND PAINTESDR SWAA2025012177551Skin · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP IB LOWER CORNER AT LT WING 2024-766038<[01] TOOL USED CALIPER: PN: 500-196-30; SN: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED: BOND TESTING UNIT; P N: BONDMASTER 600M; S N: 230106912; CAL DUE DATE: 09-JASDR JR2R20241215064Skin · chafedRH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIREDSDR JR2R20241215044Skin · chafedLH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIREDSDR SWI2025F00253Skin · chafedS/N 0295CENTER LH WING PLANK APPROX. (WS47.61), CHAFES FOUND FROM OUTBD CORNER PANEL 193AB. FLAGGED (C-CHECK RO 2/27/2025) BLENDED AND REMOVED DAMAGED FOUND TO BE ACCEPTABLE WITHIN THE MAX ALLOWABLE DAMAGE AT NON PAD UP IS 0.040" ( ZONE A ) AND PAD UP SDR DALA2024121811809Skin · corrodedSHIP 3145 CORROSION OUTBOARD FIXED TRAILING EDGE AT LEVEL RIB 13 TO RIB 14 ON LH WING (3EA). CORRECTIVE ACTION: REMOVED CORROSION ON O/B FIXED TRAILING EDGE AT LEVEL RIB13 TO RIB14 ON LH WING (3EA) AS PER A319 SRM 51-74-00-801. (0708883)SDR DALA2024121811808Skin · corrodedSHIP 3145 SECONDARY FINDING CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE LOCATED BETWEEN RIB17 TO RIB18 ON RH WING. CORRECTIVE ACTION: EMOVED CORROSION ON TRAILING EDGE UPPER SKIN LOWER SURFACE LOC BTW RIB17 TO RIB18 ON RH WING AS PER A319 SRM 51-74-00. (0SDR WRXR202412130001Skin · chafedLH FLAP FAIRING 586AB FOUND GOUGING ON WING ON FWD SIDE OF PANEL TO WING MATING SURFACE DUE TO CERAM-KOTE ON SEAL. BLENDED GOUGES ON LOWER LH WING SKIN AT AREAS C/T PANEL 586AB IAW CRJ700 SRM 51-12-00-001-001-A01. ROTO-PEENED REWORKED AREA IAW CRJ700 SRM 51-24SDR WRXR20241213004Skin · chafedLH WS264 HAS CHAFFING ON WING COMMON TO THE FWD. FARING 597AB SEAL. BLENDED DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00. INSTALLED HI-LITES IAW SRM 51-42-21 AND SRM 51-23-00. EDDY CURRENT INSPECTED IAW NDTM 53-00-000-251. ATT # 11. SHOT PENNED IAW SRM 51-24-11SDR 2024FA0000960Skin · crackedRH WING WALK BUCKLES AND IS CRACKED.SDR DALA2024121311705Access Panel · delaminatedSHIP 3136 DELAMINATED ACCESS PANEL 675KB ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 675KB ON RH WING AS PER ER/A 622452-14. (0707172)SDR SWIA2025031901211Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA73255-690-57-41-248 N554CA MXCODEID59074-PR - TEMPORARY DISPOSITION FOR BLENDED WEAR DAMAGE TO LH WING FIXED LEADING EDGE SKIN. COMPLIED WITH TEMPORARY REPAIR TO LH WING FIXED LEADING EDGE SKIN AT SS144.94, REF REO SDR AALA202412144082Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING LOWER SKIN AT WS 746. REPAIRED SKIN PER 360204.SDR WRXR20241211001Skin · gougedRH WS264 LOWER WING SKIN HAS CHAFFING COMMON TO 697AB FAIRING SEAL. REMOVED DAMAGE BLEND PER ENGINEERING NOTE 3 IAW CRJ 700 SRM 51-12-00-001-A01. ULTRASONIC INSPECTED BLENDED AREAS FOR REMAINING MATERIAL THICKNESS IN ACCORDANCE WITH MHIRJ NON-DESTRUCTIVE TESTISDR DALA2024121011572Access Panel · delaminatedSHIP 3134 DELAMINATED TRAILING EDGE ACCESS PANEL 675KB ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 675KB ON RH WING AS PER ER/A 622004-14. (0702281)SDR AALA202503034446Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOCATED ON TRILING EDGE FALSE REAR SPAR TOP SKIN OVERHANG UPPER SURFACE BETWEEN WX3622 AND WX4013 RH WING L=2.232 INC W=0.625 INCH D=0.007 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON TOP SKIN UPPER SURFACE FALSE RESDR WRXR20241209001Skin · chafedRH WS128 HAS CHAFFING ON WING LOWER SKIN COMMON TO THE 686AB FAIRING SEAL. BLENDED RH WS128 WING LOWER SKIN COMMON TO THE 686AB FAIRING SEAL IAW CRJ 700 SRM 51-12-00-001-A01. NDI REPORT F281024.PDF IN ATTACHMENTS, NO CRACKS NOTED. SHOT-PEEN REWORKED AREA IAW CSDR DALA2024121011586Skin · crackedSHIP 6704 INDICATION OF CRACK NOTED ENG DRAG FTG CLAMP UP HOLE # 13 IN THE TOP SKIN AT APPROX. 3 O'CLOCK POSITION FACING AFT. CORRECTIVE ACTION: -SUMMARY OF NR-00252- ACCOMPLISHED REPAIR ON HOLE #13 ON LH OUTER WING UPPER SKIN AT DRAG FITTINGS IAW ER/A 622147-SDR SWAA2024121074776Blade · crackedLEFT WINGLET LOWER BLADE FRAME HAS CRACK<[01] REMOVED LEFT WINGLET LOWER BLADE PER MM 57-31-21;[02] INSTALL LEFT WINGLET LOWER BLADE PER AMM 57-31-21. OPS CHECK GOOD.SDR JR2R20241207508Panel · dentedWING PANEL 551AB IS DENTED AND SCREW HOLE IS ELONGATEDSDR SWIA2020113206Access Panel · damagedLEFT WING LOWER PLANK FUEL ACCESS HOLE FOR PANEL 540DB HAS FRETTING AS MARKED. (C-CHECK RO 1/13/2025) BLENDED OUT PITTING ON THE L/H WING LOWER PLANK FUEL ACCESS HOLE 540DB, OTBD LANDING REF BOMBARDIER REO 601R-57-21-030 REV-L, DATED 2014-02-05, DETAIL SDR DALA2024120911551Skin · damagedREPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 622147-14AD. CORRECTIVE ACTION: REF ERA 622147-14AD. (0696718)SDR WRXR20241206002Skin · chafedRH WS54.55 HAS CHAFFING ON LOWER WING SKIN COMMON TO THE 683AB FAIRING SEAL. BLENDED RH WS54.55 LOWER WING SKIN COMMON TO 683AB FAIRING SEAL IAW CRJ 700 SRM 51-12-00-001-A01. NDI REPORT E281024.PDF IN ATTACHMENTS, NO CRACKS NOTED. ROTO-PEENED REWORKED AREA IAWSDR R61A2024120900584Skin · crackedDURING BI-WEEKLY INSPECTION FOUND RH WING SKIN CRACKED JUST INDB OF RIB 17 AND AFT OF FWD SPAR APROX 1 INCH LONG. REPAIRED IAW ETD2024-170-032412 ALSO REF VP-050678-2024 N/R 1 FOR WORK ACCOMPLISHED.SDR EE4Y2024120521414Skin · damagedPERFORMED PERMANENT REPAIR AT RH WING LOWER SKIN SB 190-57-0056 AFT REINFORCEMENT AREA COMMON TO SPAR II COOPESA´S EO COO-EO-2024-21236-R00 REV 00, DUE TO OVERSIZED HOLES FOUND DURING THE ACCOMPLISHMENT OF THE SB 190-57-0056, THE REPAIR WAS FOLLOWED BY THE EMBSDR EE4Y2024120521413Skin · damagedPERFORMED PERMANENT REPAIR AT RH WING LOWER SKIN SB 190-57-0056 REINFORCEMENT AREA COMMON TO SPAR I COOPESA´S EO COO-EO-2024-21119-R00 REV 00, DUE TO OVERSIZED HOLES FOUND DURING THE ACCOMPLISHMENT OF THE SB 190-57-0056, THE REPAIR WAS FOLLOWED BY THE EMBRAER SDR EE4Y2024120521410Access Panel · corrodedPERFORMED PERMANENT REPAIR AT LH WING TRAILING EDGE SLAT 4 AS PER COOPESA´S EO COO-EO-2024-21029-R00 REV 00, DUE TO CORROSION FOUND AT REAR OUTBOARD AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026436 REV ORIG. THIS REPAIR WAS CATEGORIZSDR EE4Y2024120521409Skin · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT LH WING SKIN TRAILING EDGE AT RIB 11 AREA, AS PER COOPESA´S EO COO-EO-2024-21043-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISDR SCNA20241220400Panel · damagedBIRD STRIKE ON R/H WING L/E FIXED PANEL O/B OF FIXED LANDING LIGHT. DAMAGE L-11", H-9", D 1 3/4" SPEED TAPE APPLIED TO DAMAGED AREA. HISTORICAL WORK: MRO EMP # 3426 - REMOVED AND REPLACED R/H WING FIXED L/E SKIN O/B OF FIXED LANDING LIGHT IAW SRM 51-40-02-OGSDR AALA202412185761Skin · corrodedAIRCRAFT WAS GROUNDED: FOUND DELAMINATION AND EXFOLIATION DUE TO CORROSION WITH THE FOLLOWING DIMENSIONS. 1 INCH WIDE FROM EDGE SKIN TO FORWARD, 5.250 INCHES LONG FROM INBOARD TO OUTBOARD, AND DEPTH 100 % (VERTICAL AXIS) EQUAL TO THE SKIN THICKNESS. 10 INCHES SDR AALA202412055761Skin · delaminatedAIRCRAFT WAS GROUNDED: FOUND DELAMINATION AND EXFOLIATION DUE TO CORROSION WITH THE FOLLOWING DIMENSIONS. 1 INCH WIDE FROM EDGE SKIN TO FORWARD, 5.250 INCHES LONG FROM INBOARD TO OUTBOARD, AND DEPTH 100 % (VERTICAL AXIS) EQUAL TO THE SKIN THICKNESS. 10 INCHES SDR WRXR2024001Skin · chafedRH WS220 HAS CHAFFING ON WING LOWER SKIN COMMON TO 695AB FAIRING SEAL. BLENDED DAMAGE ON RH LOWER SKIN COMMON TO PANEL 695AB L/E SEAL IAW CRJ 700 SRM 51-12-00-001-A01. REF C281024.PDF IN ATTACHMENTS FOR NDI REPORT, NO CRACKS. ROTO-PEENED REWORKED AREA IAW CRJ7SDR AALA202503034686Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE FALSE REAR SPAR STIFFENER 6 DATUM ON RH WING L=3.212 INCH W=1.413 INCH D=0.050 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON TOP SKIN UPPER SURFACE FALSE REAR SPAR BTW RIB WX3622 TO RIB WX4349 ON RH WINGSDR AALA202502287046Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE BETWEEN RIBS 7 AND 8. REPAIRED SKIN PANEL PER EA 360704.SDR AALA202502284253Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE REAR SPAR TOP SKIN PANEL #2 LOWER SURFACE BETWEEN RIBS 14 AND 15. REPAIRED SKIN PANEL PER EA 360704.SDR AALA202502243613Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE REAR SPAR TOP SKIN LOWER SURFACE AT WX6695.749 AND RIB 18. REPAIRED SKIN PANEL PER EA 360549.SDR AALA202502245186Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE REAR SPAR TOP SKIN LOWER SURFACE AT WX2210.93 AND RIB 10. REPAIRED SKIN PANEL PER EA 360549.SDR CALA2024120403018Skin · crackedACCOMPLISH A PERMANENT REPAIR ON THE RH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591 PRIOR TO 02 JULY 2026 SKIN AROUND THE OUTBOARD FASTENER OF STRINGER R-9 BETWEEN WS 564.5 AND WS 591.5 REF NR 002323616 FOUND A CRACK THAT PROPAGATES 0.8" FWD OF THE FASTENER SDR NACA2024120200002Skin · corrodedRIGHT WING LOWER INSPAR SKIN CORROSION REAR SPAR, WS 694~720. ACCOMPLISHED EO 767-57-0038.SDR UIEA2024120301157Skin · corrodedCORROSION - SKIN, L/H WING L/E CAVITY FRONT SPAR LOWER SKIN, ILES 949.(<P>1. REMOVED THE EFFECTED FASTENERS IAW SRM 51-40-02-0G-0, REV.58. 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-2, REV. 58. 3. PFM NDT INSP REFER TO JOB CARD ATTACHING NO. 0428990 & SDR DALA2024120311388Plate · corrodedSHIP 3134 CORROSION WAS FOUND ON PYLON REINFORCING PLATE, ON BOTTOM SKIN AT RIB 8 AND STR 5. CORRECTIVE ACTION: COMPLIED WITH ER/A 621753-14. (0690255)SDR AALA202412303689Panel · brokenAIRCRAFT WAS GROUNDED: RIGHT WING, TOP SIDE AT WS 387.00 FRONT SPAR, PANEL BROKEN. ACCOMPLISHED PERMANENT REPAIR PER SRM 51-70-04-2R.
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