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 A6WA200540370Skin · corrodedRT WING LOWER PLANK HOLE NR 16, WS 303.861 HAS CORROSION AT IB SIDE 1 INCH L X .005 INCH D. NOT CRITICAL. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 16 IAW REO. (K)SDR A6WA200540369Skin · corrodedRT WING LWR PLANK HOLE NR 7, WS 116.366 HAS CORROSION AT IB SIDE 2 INCHES L X .005 INCH DEEP AND FWD SIDE .5 INCH L X .005 INCH D, NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT LWR WING PLANK ACCESS HOLE NR 7 IAW REO. (K)SDR A6WA200540368Skin · corrodedRT WING LOWER PLANK HOLE NR 5 WS 76.161 HAS CORROSION AT IB FORWARD SIDE 4 INCHES L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING LOWER WING PLANK ACCESS HOLE NR 5 IAW REO. (K)SDR A6WA200540371Skin · corrodedLT LWR WING PLANK HOLE NR 2, WS 12.245 HAS CORROSION AT OB SIDE AFT 2 INCH L X .005 INCH D AND AT IB SIDE 8 INCHES L X .005 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 IAW REO. (K)SDR A6WA200540372Skin · corrodedLT LOWER WING PLANK HOLE NR 1, WS 54.897 HAS CORROSION AT IB SIDE FORWARD EDGE 2 INCH L .005 INCH D AND AT OB SIDE AFT 4 INCH L X .005 INCH D. NOT IN CRITICAL AREA. MAINT REPAIRED LT LOWER WING PLANK ACCESS HOLE NR 1 IAW REO. (K)SDR A6WA200540373Skin · corrodedLT WING LOWER PLANK HOLE NR4, WS 54.681 HAS CORROSION AT OB SIDE 5 INCH L X .002 INCH D AND AT IB SIDE 5 INCH L X .002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 4 AT WS 54.681 IAW REO. (K)SDR COMA0560757Channel · corrodedFLOOR SEAT RAIL CORRODED. REPAIRED RT FLOOR SEAT RAIL FROM FS 399.5 TO 409+126 BY REMOVING AND REPLACING TRACK IAW BRAS EO 601R-53-7965A.SDR IXXA05SMN305SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, RT WING - T/E LWR SKIN NON STANDARD REPAIR, XW 762.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-0 FIG 2A (SHEET 1), TR 57-84 DATED 08-01-00. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW DC-8SDR IXXA05SMN314SRepair · improperDURING ROUTINE C-CHECK INSPECTION, RT WING L/E HAS NON STANDARD REPAIR, XFS 761.695. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06014 DATED 01-1-06, SEMAN DWG ED-4135 DATED 01-06-06, ED SEMAN 2005 1472 DATED 01-11-06. REMOVED NON STANDARD REPAIR IAW DC8 SRSDR IXXA05SMN313SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RIGHT WING - INBOARD L/E LWR PART HAS NON STANDARD REPAIR, XFS 63.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4133 DATED 02-06-06, ED SEMAN 2005 1470 DATED 01-05-06. REMOVED EXISTING NSDR IXXA05SMN312SRepair · misinstalledDURING ROUTINE C-CHECK, RT WING - CTR L/E LWR PART HAS NON STANDARD REPAIR, XFS 304.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06006 DATED 01-05-06, SEMAN DWG ED-4134 DATED 01-04-06, ED SEMAN 2005 1471 DATED 01-05-06. REMOVED NON STANDARD REPAIR IAW DC8SDR IXXA05SMN299SSkin · corrodedDURING ROUTINE C-CHECK INSP, LT WING OB L/E CORRODED, XFS 566.250 (LWR SURFACE) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATE 12-23-05, DWG NR ED 4126 DATE 12-21-05 EO NR 20051457 DATE 12-23-05 REMOVED FASTENERS IAW SRM 51-1-21, DC8 SRM 51-1-20D . SDR IXXA05SMN297SRepair · misinstalledDURING ROUTINE C CHECK INSPECTION, LT WING.- OB L/E HAS NON STANDARD REPAIR, XW 762.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06006 DATED 01-05-06 REMOVED NON-STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D DC8 SRM 51-3-0 REMOVED DAMAGED SECTION IAW DWSDR IXXA05SMN302SSkin · corrodedDURING INSPECT, LT WING CTR L/E CORRODED, XFS 422.750. PERFORMED REPAIR IAW FAA FORM 8110-3 # 05587 DATE 12-29-05, SEMAN DWG # ED 4127 DATE 12-28-05 AND EO SEMAN # 20051458 DATE 12-29-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED CORROSION IAW DC-8 SRM SDR IXXA05SMN301SSkin · corrodedDURING INSPECT, LT WING OTBD L/E HAS NON STANDARD REPAIR, XW 485.000. PERFORMED REPAIR IAW FAA FORM 8110-3 # 05582 DATE 12-23-05, SEMAN DWG # ED 4125 DATE 12-22-05 AND EO SEMAN # 20051456 DATE 12-23-05. REMOVED NON STANDARD REPAIR IAW DC-8 SRM 51-1-21, DC-8 SSDR IXXA05SMN300SSkin · corrodedDURING INSPECT, LT WING CTR L/E LWR PART SKIN CORRODED, XFS 341.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4124 DATE 12-22-05, EO SEMAN NR 20051455 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. SDR IXXA05SMN298SSkin · corrodedDURING INSPECT, LT WING CTR L/E EXT LWR SKIN CORRODED, XFS 304.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4123 DATE 12-27-05 AND EO SEMAN NR 20051454 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-SDR COMA0560762Skin · corrodedRT LOWER WING PLANK HAS FRETTING CORROSION AT FUEL TANK ACCESS CUTOUTS, (610AB NOT IN CRITICAL AREA), (640DB, 640EB, 640FB, 650AB, 650CB, 650DB, 650FB, 650HB IN CRITICAL AREA). REPAIRED LOWER WING PLANK FUEL TANK ACCESS CUTOUTS IAW BOMBARDIER REO 601R-57-21-0SDR COMA0560761Skin · corrodedLT LOWER WING PLANK HAS FRETTING CORROSION AT FUEL TANK ACCESS CUTOUTS, 540AB, (510AB AND 540BB NOT IN CRITICAL AREA), 540CB, 540EB, 540FB, 550AB, 550CB, 550DB, 550EB, 550FB. REPAIRED LOWER WING PLANK FUEL ACCESS CUTOUTS IAW BOMBARDIER REO 601R-57-21-030. RESDR UPS06M46178Skin · chafedINSPECTION TYPE:C LHW UPP SURFACE FIXED L/E AREA AT STA XRO 1192 APP (ON TOP LT NR 8 SLAT O/B EDGE AREA) FOUND CHAFF MARK. CHAFF MARK PER A/M DISCREPANCY BLENDED AND PROTECTED PER SRM 51-21-01.V2. R38.ORI THK 0.065,MAT REMOVED 0.031" FOUND EXCEEDED LIMIT. DASDR 05FDEA04401Skin · crackedLT WING L/E FOUND 1 CRACK 3.50" LONG ON SKIN AT STA XORS 505 AND 1 CRACK ON INT STRUCTURE LOWER CHORD FIXED PANEL. CLEANED AREA IAW M/M 12-22-01. REMOVED REFUELING DOOR IAW SRM 51-31-01 PAGE 36/41 VOL 2. REMOVED FASTENERS, WEB AND SKIN AS REQUIRED, REMOVED SDR MWEA050139Panel · bentRT WING TRAILING EDGE PANEL FORWARD OF RT IB SPOILER IS BENT UP. REMOVED DAMAGE INSTALLED DOUBLER.SDR A6WA200540365Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR2 UNDER PNL 510AB AT WS 12.245 HAS CORROSION ON IB SIDE APPROX 3 INCH L X .1 INCH W X .004 DEEP IN NON CRITICAL AREA. MAINTENANCE REPAIRED WING PLANK ACCESS HOLE AT WS 12.245 IAW REO. (K)SDR DHL2005803556Skin · crackedPERFORM PREVENTATIVE MODIFICATION IAW SB 57-88 REV. 3 ON LT WING LOWER SKIN CRACK AT STA 69.5 REF. SB AND DRAWING JO 60095-506. PERFORMED PREVENTATIVE MODIFICATION IAW AD80-22-01, SB 57-88 REV. 3 DWG NR JO60095-506. REMOVED FASTENERS AND SKI FITTING IAW DWG JOSDR AU510001884Screw · looseOUTER WING FORWARD UPPER BATHTUB FITTING TO UPPER SKIN PANEL ATTACHMENT SCREWS LOOSE. SUSPECT SCREWS INCORRECTLY TORQUED DURING MANUFACTURE.SDR AU510001738Stitching · loose(AUS) TOP WING FABRIC RIB STITCHING LOOSE AND BROKEN. INSPECTION FOUND UNAPPROVED KNOTS IN THE STITCHING WHICH SLIPPED WHEN PULLED. SEE ATTACHMENT FOR PHOTOGRAPHS. (CASA NR 510001738)SDR 05FDEA04219Skin · crackedSMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPASDR DHL2005803553Skin · crackedITEM REF. NR. 038581: RT WING LWR SKIN OB FASTENER HOLE CRACKED 0.250 INCH S-64 (MAJOR REPAIR). PERFORMED MAJOR REPAIR AND REMOVED FASTENERS IAW SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW SB 57/100 FIG. 5 SHEET 2 OF 5. FABRICATED DOUBLERS (7075T6 AL 0.125 INCHSDR EIA23005257Skin · corrodedDURING "B" CHECK INSPECTION, FOUND CORROSION ON LT WING LOWER SKIN, LOWER FRONT SPAR CHORD, AND FRONT SPAR WEB BETWEEN FSS 1250 AND 1510. REMOVED DAMAGED CHORD AND REPLACED A REPAIR SECTION OF CHORD FROM FSS 1260 TO THE PRODUCTION SPLICE AT FSS 1446.13. REPASDR QXEA200600239Skin · damagedYYC - RT WING UPPER TRAILING EDGE (JUST I/B OF MULTIFUNCTION SPOILERS) HAS LOOSE FASTENER. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-00-001-001-A01 AND 51-42-21-001-001-A01.SDR QXEA200600243Skin · damagedYYC - LT WING, I/B MFS SURROUND AT WS 170.83 LOOSE FASTNERS. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCH-UP IAW CRJ 700 SRM 51-25-16-001-001-A01.SDR QXEA200600242Skin · damagedYYC - LT WING, I/B MFS SURROUND SKIN AT WS 170.83 LOOSE FASTNERS. FASTENERS REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCH-UP IAW CRJ 700 SRM 51-25-16-001-001-A01.SDR QXEA200600241Skin · damagedYYC - LT WING, O/B MFS SKIN (SURROUND) AT WS 231.23 LOOSE FASTENERS. REPLACED FASTENERS (MS20426T) IAW CRJ 700 SRM 51-42-06-001-001-A01. TOUCHED UP IAW CRJ 700 SRM 51-25-16-001-001-A01.SDR QXEA200600261Skin · chafedYYC- RT WING OUTBD LEADING EDGE SKIN HAS CHAFED MARK FRO ADJACENT RIVET HEAD AT WS294. CHAFE DAMAGE BLENDED IAW CRJ 700 SRM 57-41-01-101-001-A01 AND 51-12-00-001-001-A01 REMAINING MATERIAL WITHIN LIMITS. LPI COMPLETED ON BLENDED AREA IAW CRJ 700 PT 01 51-20-SDR SDR2005083Skin · corrodedDURING INSPECTION FOUND LT WING LOWER EXTERNAL SKIN WITH CORROSION AT THE T/E (UNDERWING BOX ANGLE END). REMOVED CORROSION AND TREATED IAW SRM. DEFERRED IAW SRAS. AREA BLENDED AS INSTRUCTED.SDR 05FDEA04139Repair · unknownRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH 236 DIMENIONS 3.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P. RESTORED PAINT ON STRIPPED AREA IASDR 05FDEA04138Repair · unknownRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENIONS 8.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2. RESTORED PAINT ON STRIPPED AREA ISDR 05FDEA04137Repair · unknownRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 155 DIMENIONS 3.25 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IASDR 05FDEA04131Skin · corrodedMAIN CABIN, CENTER WING BOX UPPER SURFACE, SKIN IS CORRODED AT STA BS 820 LBL10. REPAIR CENTER WING BOX UPPER SURFACE OF SKIN IAW FEDEX EA7 5710-92595. "WINGS UPPER SKIN PANEL, CENTER TANK CORRODED, REPAIR ". ALODINED AND PRIMED BARE METAL IAW B727 SRM 51SDR ASAA0570111Skin · tool damageSEA: DURING SCHEDULED MTX FOUND L/E LWR SURFACE DEFORMED AT WBL 658.17. REPAIRED IAW EA. (K)SDR SWAA053842Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT WING UPPER SKIN CRACKED AT WBL 157.00, REAR SPAR UPPER CHORD. REPAIRED SKIN PER SWA EA.SDR 05FDEA04083Skin · corrodedLEFT HAND WING UPPER TRAILING EDGE PANEL FOUND BULGING AT XORS 1036. REMOVED CORROSION AT LEFT HAND WING UPPER TRAILING EDGE PANEL, XORS 1036 AS PER SRM 51-21-011 VOLUME II. ORIGINAL THICKNESS=0.140, MATERIAL REMOVED 0.100, REMAINING THICKNESS=0.040", FOUNSDR AUCR200500005Skin Panel · corrodedRT WING LOWER SKIN PANEL NR 7 AT BUTT LINE 65 INTERNAL INTERGRANULAR CORROSION. THE DEFECTIVE PANEL WAS FIRST DETECTED BY A FUEL LEAK AT BUTT LINE 65. FURTHER INVESTIGATION REVEALED EXFOLIATION FROM INTERGRANULAR CORROSION. THE CORROSION WAS CONCEALED BY LAYERSDR 05FDEA04080Repair · unknownLEFT WING UPPER SURFACE FOUND A DOUBLER 30.50" BY 12.50" ON SKIN AT STA XORS 130. PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 44 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-500, RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VSDR 0601056Skin Panel · delaminatedRIGHT WING TRAILING EDGE LOWER PANEL DELAMINATEDSDR 05FDEA04046Repair · unknownPREVIOUS REPAIR INSTALLED ON LT WING IB L/E IB OF NR 1 SLAT, EXTERNAL DOUBLER WS 139 RIB3, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUS REPAIR WAS NOT AN APPROVED REPAIR. REMOVED SKIN IAW A310-200 SRM 51-72-10. FABBED NSDR 05FDEA04045Repair · unknownPREVIOUS REPAIR INSTALLED ON RT WING TE PANEL EXTERNAL SKIN AFT OF PYLON, EXTERIOR DOUBLER, STA 482-513 RIB 8-9, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. PREVIOUSLY INSTALLED REPAIR ON RT WING T/E PANEL AFT OF PYLON WAS ACCOSDR 05FDEA04044Repair · unknownPREVIOUS REPAIR INSTALLED ON RT IB FLAP UPPER SURFACE RIB 17-19, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. THE REPAIR AS NOTED CONFORMS TO SRM 57-52-12 FIG 204 WITH THE EXCEPTION OF FASTENER PITCH. LOCATED AND DRILLED FASTENERSDR AUCR200500001Panel · crackedLOCATED LOWER WING PLANK RISER FRACTURE 7 INCHES IN LENGTH LT WING STA. 167. FRACTURE EMANATED ALONG BASE OF RISER EXTENDING IB AND OB SPANWISE. FRACTURE WAS VISUALLY DETECTED DURING SCHEDULED INSPECTION. FRACTURE WAS PROPAGATED BY THE MAIN LANDING GEAR TRUSS SDR ABXA050332Skin · crackedFOUND SKIN, FORWARD OF PANEL 1601, HAD A CRACK COMPLETELY ACROSS THE SKIN. MANUFACTURED NEW SKIN AND INSTALLED IAW DC9 51-30-5 AND 51-30-1.
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