JASC 5730
Service difficulty reports · 27,269
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 A6WA200740384Panel · corrodedRT WING PLANK AT PANEL 640BB HAS CORROSION APPROX .004 DEEP X 4 INCH LONG X .2500 INCH WIDE IN NON-CRITICAL AREAS. MAINTENANCE PERFORMED MAJOR REPAIR TO WING PLANK ACCESS HOLE AT WS 54.897 (RT) BY REMOVING CORROSION IN NON-CRITICAL AREAS OF HOLE IAW REO 601R-SDR ARWA20070611Access Door · crackedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505C WT OUT WITH 02 CRACKS. REPAIR ACC DOOR NR 505C OF RT WING UPPER SURFACE MAIN FUEL TANK IN ACCORDANCE WITH DRAWING NR AIPSAC - N661AV-02/07, DATED 01-12SDR ARWA20070610Access Door · crackedDURING "C" CHECK INSPECTIONS, THE FOLLOWING WAS FOUND; RT WING UPPER SURFACE MAIN FUEL TANK ACCESS DOOR NR 505E CUT OUT WITH CRACK. REPAIRED RT WING UPPER SURFACE MAIN FUEL TANK ACC DOOR NR 505E CUT OUT IN ACCORDANCE WITH DRAWING NR AIPSAC-N661AV-02/07 RD, SHSDR 07FDEA02141Doubler · damagedEXISTING SKIN REPAIR RIGHT WING L/E SKIN AT STA XOS 800 REPAIRED IAW SRM 57-10-00 FIG 20 VOL 1.SDR KCSA071191Rivet · pulledRIVETS PULLING THROUGH SKIN AFT OF AFT SPAR TOPSIDE OF WING AT WS-411.SDR QXEA200701109Panel · chafedC3 OKC - LEFT WING PANEL 584ET CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01, 51-21-11.SDR QXEA200701107Panel · chafedC3 OKC - LEFT WING PANEL 584JB CHAFED. REPAIRED IAW SRM 51-12-00, 57-52-01, 51-21-11.SDR QXEA200701108Panel · chafedC3 OKC - LEFT WING PANEL 584GB CHAFED. REPAIRED IAW SRM 51-12-00, 51-25-06, 57-52-01.SDR DHL2007803537Skin · delaminatedRT WING T/E UPPER PANEL SKIN DELAMINATED (STA XW 0.000 - 47.000). REMOVED DELAMINATED PANEL IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0, SRM 51-3-1 PG 2A (TORQUE).SDR AMWA7020DSkin · crackedRT WING SKIN CRACKED BETWEEN FS303.25 AND FS310.75 AT WS25. LENGTH OF CRACK APPROX 5.5 INCHES. REPAIRED IAW REPORT 6702-2 REV 1R.SDR 07FDEA02105Skin Panel · damagedOLD REPAIR (BLEND OUT ) ON LT WING BOTTOM SKIN LOWER SURFACE AROUND HOLE 389 IAW DRW R571-40141 SH 17 REPAIR ACCEPTACLE BY AI RAS/BAE/1004818/2007 ISS. A, APPROVED BY EA 6-5720-106454.SDR C2XA07SH032Panel · corrodedSHV - DURING C-CHECK MAINTENANCE FOUND OVER THE WING TO FUSELAGE PNL 195 WITH CORRODED BONDING STRAPS. MAINTENANCE REPAIRED PNL 195 IAW EC 5750-01315, AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR 2007UALA01907Skin · damagedL/E OF LEFT WING BEHIND NR 4 SLAT DAMAGED. WING LEADING EDGE REPAIRED AND NEW NR 4 LE SLAT INSTALLED.SDR DHL2007803534Skin · wornRT OUTBD FLAP UPPER SKIN WORN, STA XF 224.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 06-06-07, DWG NR AD42-57-106 REV IR DATED 05-21-07. REMOVED EXISTING REPAIR PLATING AND INNER DOUBLER IAW SRM 51-1-21. FABRICATED NEW PLATING SEGMSDR UPS07849964Doubler · crackedINSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE AT XFS 334. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D AND DWG 5769589.SDR 07FDEA02093Skin · corrodedTOP OF CENTER TANK RIGHT SIDE FOUND CORROSION AT STA 1219. CORROSION IN TOP OF CENTER TANK RIGHT SIDE AT STA 1219 CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5710-111114, TITLE: WINGS, CENTER WING FUEL TANK RIGHT SIDE CORROSION REPAIR. REPAIR CLASSIFIED AS MAJSDR 07FDEA02090Skin Panel · wornELONGATED HOLES ON LT WING-PYLON SUPPORT BRACKET AND BOTTOM SKIN REPAIR PERFOMED BY OVERSIZING THE HOLE AND MANUFACTURE A FREEZE PLUG IAW DWG R571- 50532, APPROVED BY EA 6-5720-103269 AND RAS/BAE/1003287/2006 ISS. ASDR 07FDEA02089Skin Panel · wornELONGATED HOLES ON RT WING-PYLON SUPPORT BRACKET AND BOTTOM SKIN, RIB 8 AREA REPAIR PERFORMED BY OVERSIZING HOLES AND MANUFACTURING FREEZE PLUGS IAW DWG R571-50532 ISS. A. APPROVED BY EA 6-5720-103269 AND RAS/BAE/1003287/2006 ISS. ASDR UPS07849963Doubler · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR INNER DOUBLER POSSIBLE CRACK AT XFS 597 AROUND DRAIN HOLE. REMOVED INNER DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW 57-3-3 FIG 7, 51-1-21.SDR DHL2007803526Doubler · crackedRT WING CTR L/E UPPER ANGLE DOUBLER CRACKED STA XFS 428.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED ANGLE DOUBLER (AL7075"0" 0.080") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW SSDR 07FDEA02061Skin Panel · corrodedRT WING TOP SKIN PANEL NR 2, TRAILING EDGE AREA CORRODED, RIB 26-31 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-101256 AND RAS/BAE/1002866/2006 ISS. ASDR DHL2007803521Panel · crackedLT WING LWR PANEL CRACKED 1" STA XW -3.125. REMOVED PANEL IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EC-00359-001 (WO 1028) FOR PANEL FABRICATION.SDR 2007UALA01747Skin · damagedLEFT AND RIGHT LWR WING SKINS HAD DAMAGED FASTENER HOLES AT MOUNTING FLANGE OF PANELS 540NB, 540PB, AND 640NB, 1EA HOLE AT EACH PANEL.SDR DHL2007803515Skin · delaminatedLT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 339.000 - 409.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).SDR SWAA072771Skin · corrodedDURING SCHEDULED 22Y CHECK, FOUND LEFT WING UPPER SKIN CORRODED AT BETWEEN STA 119 AND STA 126, FWD SPAR. REPAIRED SKIN PER ER.SDR SWAA072772Skin · corrodedDURING SCHEDULED 22Y CHECK, FOUND LEFT WING UPPER SKIN CORRODED AT STA 252, FWD SPAR. REPAIRED SKIN PER ER.SDR 07FDEA02030Skin · corrodedCORROSION WITH CRACK FINDINGS (A= 22MM, B= 25MM) ON HOLE 699 (DRW R571-40141 SHEET 12), LT WING BOTTOM SKIN LOWER SURFACE. REPAIR PERFORMED BY REAM UP TO NEXT OVERSIZE IAW EA 6-5720-106453 AND RAS/BAE/1004815/2007 ISS. ASDR 07FDEA02029Skin · corrodedCRACKS AND CORROSION ON RT WING BOTTOM SKIN LOWER SURFACE ON (HOLE 712 CORRODED, HOLE 311 CRACKED A=12MM, B11MM, DRW R571-40141 SHEET 14). REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106453 AND RAS/BAE/1004815/2007 ISS.ASDR 07FDEA02028Skin Panel · corrodedCORROSION LT WING TOP SKIN PANEL NR 3, RIB 26-27, STRINGER 17A TO REAR SPAR REPAIR PERFORMED BY BLEND OUT AND REMOVAL OF AFFECTED FASTENER IAW EA 6-5730-106449 AND RAS/BAE/1004794/2007 ISS.ASDR 2007FA0000512Panel · delaminatedDURING COMPLETION OF MFG PROGRAM PHASE 5 INSPECTION, NOTICEABLE DEPRESSION WAS OBSERVED IN UPPER SURFACE OF LT AND RT WING SKINS IN AREA OF MLG UPLOCK HOOK ASSY ATTACHMENT. DURING COMPLETION OF LANDING GEAR OPERATIONAL CHECK, IT WAS NOTED THAT DEPRESSION ARE SDR 2007FA0000511Panel · delaminatedDURING COMPLETION OF MFG PROGRAM PHASE 5 INSPECTION, NOTICEABLE DEPRESSION WAS OBSERVED IN UPPER SURFACE OF LT AND RT WING SKINS IN AREA OF MLG UPLOCK HOOK ASSY ATTACHMENT. DURING COMPLETION OF LANDING GEAR OPERATIONAL CHECK, IT WAS NOTED THAT DEPRESSION AREASDR 07FDEA02017Fairing · delaminatedLEFT NR 3 FLAP TRACK MOVABLE FAIRING HAS TWO AREAS OF DELAMINATED. REMOVED DAMAGE AND BONDED REPAIR PLIES PER SRM 57-20-35 AND PAINTED PER SRM 51-75-10.SDR HALA0700236Skin · corrodedMODERATE CORROSION ON SURFACE SKIN AROUND FUELING CAP AT APPROX STATION 432, JUST FWD OF STRINGER NR 2 13/8" BY 2" BY .030"DEEP. CLEANED, TREATED CORROSION PER SRM 51-10-9. REPAIRED PER M105 FILE NR 484084. PRIMED AND PAINTED.SDR HALA0700238Fairing · crackedCRACK ON LT WING FLAP INBOARD TRACK FAIRING (ELEPHANT EAR). REPAIRED PER HAL M 105, FILE B10195. FABRICATED AND INSTALLED DOUBLER. INSTALLED WITH PR1440. PRIMED AND PAINTED.SDR HALA0700237Fairing · crackedCRACK ON RT WING INBOARD TRACK FAIRING (ELEPHANT EAR). REPAIRED PER HAL 105, FILE NR B10195. FABRICATED AND INSTALLED DOUBLER WITH PR1440, CORROSION PROTECT. PRIMED AND PAINTED.SDR HALA0700235Skin · corrodedMODERATE CORROSION ON SURFACE SKIN AROUND FUELING CAP AT APPROX STATION 432 BETWEEN STRINGERS NR 2 AND NR 3, 1 3/4" BY 3/4" BY .029" DEEP. CLEANED AND TREATED CORROSION PER SRM 51-10-9. PRIMED AND PAINTED.SDR C1HA200796002Skin · corrodedLT LOWER WING SURFACE APPROX BS 800 IN RAM AIR AREA IS CORRODED (PLENUM). BLENDED OUT DAMAGED AREA AND REPAIRED IAW EO-727-5710-04 REV IR.SDR 07FDEA02142Skin · wornLT WING, AILERON ACTUATORS ACCESS PANEL AREA LOWER SKIN WITH BURROWS WITHOUT MARGINAL DISTANCE. IT WAS REPAIRED IN ACCORDANCE WITH FEDEX EA 6-570-106714.SDR DLM88070626Skin · crackedCRACK ON LT WING FIXED TRAILING EDGE UPPER SKIN. PERM REPAIR INSTALLED PER SRM 57-03D FIG 802D ON N/R T0056674, HMV/GDL.SDR ASAA0741707Skin · crackedRIGHT WING FIXED L/E SKIN AT NR 5 SLAT ACTUATOR CURTAIN CUTOUT CRACKED. RIGHT WING FIXED L/E SKIN AT NR 5 SLAT ACTUATOR CURTAIN CUTOUT REPAIRED SERVICEABLE IAW SRM 51-70-17.SDR UPS07M50365Skin Panel · crackedINSPECTION TYPE:C RIGHT FIXED L/E LWR COMPT THRU ACCESS 619CB (REFUEL PANEL) UPPER SKIN DOUBLER SUSPECTED CRACK AT STA XORS 537. RIGHT WING REFUELING/DEFUELING ADAPTOR O/B REMOVED PER AMM28-21-08R.55. DAMAGE AREA TRIM OFF & REPAIR ANGLES FAB PER ADV EN1375-0SDR UPS07M50284Skin · crackedINSPECTION TYPE:C LT FIXED LE LWR COMPT UPPER SKIN DOUBLER SUSPECTED CRACK AT STA XORS 535. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 PART 06-10-01-001 FOUND CRACK AS MARKED. REPAIR ANGLES FAB AND CRACK AREA TRIM OFF PER EN1375-07. REPAIR ANGLES HEAT TREATESDR DHL2007803506Doubler · crackedRT WING CTR L/E LWR SKIN INTERNAL DOUBLER CRACKED 0.500" STA XFS 428.000. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090") IAW SRM 57-2-0 PG 1 AND CLEANED, TREATED AND PRIMED AREA AND INTERNAL SDR ODR2007F00000Skin · cracked7-8 INCH CRACK IN SKIN OF WING LOCATED BETWEEN LT NACELLE AND FUSELAGE; AFT OF LEADING EDGE; ON TOP OF WING. APPARENT CAUSE IS FATIGUE DUE TO PREVIOUS OWNER WALKING ON WING. CRACK BECAME APPARENT DURING PRE-FLIGHT INSPECTION ON 5/22/2007. (K)SDR 07FDEA01933Skin · crackedRT WING, UPPER WING SKIN CRACKS AT NR 12 I/B HINGE CUT OUT. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATION, FABRICATED AND INSTALLED REPAIR DOUBLER REF SRM 57-30-4.SDR 07FDEA01901Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 3 WS 737-813 RIB 12-13. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TSDR 07FDEA01893Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, OUTB OF SPOILER 3 WS935 RIB 15. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A SRM SDR 07FDEA01892Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, INBD OF SPOILER 3 WS 737 RIB 12. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRMSDR 07FDEA01866Panel · crackedLEFT WING LEADING EDGE LOWER SURFACE ACCESS PANEL 524 EB LAND AREA HAS CRACK LENGTH 1.300 IN WS 1403. FABRICATED DOUBLERS FROM 6061-T6 .063 AND 6061-T6 .071C IAW SRM 57-41-12, SRM 51-71-30, SRM 51-71-40. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED DOUBLSDR 07FDEA01861Skin · crackedRIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT-OUT STA XOS 464 AND STA 469 FOUND CRACKED. [SUP 06-08-07] REPAIRED AS PER SRM 57-10-00 VOLUME I, FIGURE 43. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.
Back to JASC 5730