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 0500131237Skin · crackedDURING H-CHECK FOUND CRACK ON RT WING LEADING EDGE SKIN AT XOS 693. REPAIRED PER EA 12-202235.SDR UPS05843754Doubler · crackedINSPECTION TYPE:C3, LEFT WING CENTER L/E INTERNAL DOUBLER CRACKED BETWEEN XFS 422.75 & XOLDI 6.225. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6-.080 PER DWG 5769891. REMOVED & REPLACED DOUBLER PER SRM 51-1-8, 51-1-20D, 51-1-21, 51-1-15.SDR UPS05843747Doubler · crackedINSPECTION TYPE:C3, LEFT WING O/B LEADING EDGE LOWER INTERNAL DOUBLER CRACKED NEAR XFS 623. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6-.080 REF DWG 5769545. REMOVED & REPLACED DOUBLER REF SRM 51-1-8, 51-1-21, 51-1-20D.SDR UPS05843744Doubler · crackedINSPECTION TYPE:C3 INNER DOUBLER CRACKED AT DRAIN HOLE NEAR XFS 591, RIGHT WING O/B LEADING EDGE. REMOVED OLD REPAIR DOUBLER, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL FAB REPLACEMENT INTERNAL DOUBLER FROM SHT7075T6-.080. REMOVED AND REPLACED INNER DOUBLERSDR WRLA2005001Panel · corrodedLEFT SIDE UNDER WING TO FUSELAGE PANEL NR 153DB ON BOTTOM SURFACE HAS EXFOLIATE CORROSION BETWEEN STATIONS 1239 AND 1321. REMOVED WING TO FUSELAGE PANEL NR 153DB AND ACCOMPLISHED REPAIR TO LT WING FUSELAGE PER ERA 05-53-001 REV NC DATED 01/07/05 PART 1. ACCOSDR USAA050060Skin · delaminatedPIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 6 INCH AREA, BOTTOM SIDE 14 INCHES FROM INBOARD END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLERS AND FILLRS PER SRM 51-70-10. (M)SDR USAA050061Skin · delaminatedPIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 4.5 INCH AREA, 34 INCHES FROM F/B EDGE. REMOVED DAMAGE, INSTALLED FILLERS, DOUBLERS PER SRM 51-70-10. (M)SDR USAA050155Skin · crackedPIT - Q6 - SKIN, APPROX 1 INCH CRACK; NR 2 ENG OB WING/LEADING EDGE AT SLAT STA3.25, LWR SKIN PANEL. FABRICATED SKIN FILLER/ DOUBLER IAW TYP REP. (K)SDR A6WA200540005Skin · corrodedFOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 163 HAS MINOR FRETTING ON FAYING SURFACE. LESS THAN .008 INCH DEEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M)SDR ASA0440382Skin · corrodedPAE - CORROSION ON LT UPPER WING PANEL 8117 CUTOUT UPPER FLANGE. BLENDED CORROSION AND REPAIRED. (K)SDR COMA0560005Skin · crackedLOWER LEFT HAND WING PLANK CRACK INBOARD OF WS 149.85. REPAIRED IAW REO 601R-57-21-539.SDR A6WA200440230Access Panel · damagedWHILE ACCOMPLISHING SB 601R-57-037, THE NR 18 HOLE AT WS 148 LT WAS FOUND TO BE ELONGATED TO .280 INCH. REPAIRED ELONGATED HOLE AT LT WS 148 BY INSTALLING FREEZE PLUG IAW BRAS REO 601R-57-5757. (M)SDR A6WA200440228Skin Panel · damagedFOUND SCREW HOLE NEAR NACA SCOOP AT LT WS 148 ELONGATED TO .300 INCH. REPAIRED BY INSTALLING COUNTERSUNK FREEZE PLUG IN SKIN PANEL AND INNER STRINGER EO NR 601R-57-5753 REV A. (M)SDR 2004FA0000935Skin · delaminatedSKIN DELAMINATION ON LT WING CENTER SECTION UPPER SURFACE AFT OF THE SPAR NOTICED BY MAINTENANCE CREW, WHILE MAINTENANCE WAS BEING COMPLETED ON A NON-RELATED MATTER.SDR ASAA0480612Access Panel · chafedOKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M)SDR ASAA0480610Access Panel · gougedOKC - HV-CHECK, RIGHT WING STRUCTURE UNDER FUEL PANEL 1436 RUB STRIP IS GOUGED. REPLACED DAMAGED SECTION PR EA 5720-01258. (M)SDR ASAA0480609Skin · gougedOKC - HV-CHECK, RIGHT WING INNER LOWER SKIN GOUGED JUST FORWARD OF DRAIN HOLE. REPLACED DAMAGED SECTION PER EA 5720-01259 AND -10702. (M)SDR QXEA200400886Panel · corrodedPDX - PANEL 522CT HAS CORROSION IN NUMEROUS BOLT HOLES AND ON PANEL MATING SURFACE. REPLACED LEFT HAND WING FUEL PANEL 522 IAW Q400 WC 500ME28 60266.SDR QXEA200400884Panel · chafedPDX - COUNTER SINKS CHAFED AT LEFT WING FUEL PANEL 523AT. HEAVIEST AT INBOARD AND OUTBOARD ENDS. REPLACED IAW Q400 WC 500ME28 60266.SDR QXEA200400883Panel · chafedPDX - COUNTER SINKS CHAFED LEFT WING FUEL PANEL 522CT, HEAVIEST AT INBOARD AND OUTBOARD ENDS. REPLACED IAW Q400 WC 500ME28 60266.SDR A6WA200440208Skin · corrodedLT WING LOWER PANEL FUEL TANK ACCESS DOOR CUT-OUT AT WS 12.245 HAS NUMEROUS AREAS OF PITTING/ FRETTING LOCATED ON FAYING SURFACE AND RADIUS AREAS. DEPTH LESS THAN .015 INCH. REPAIRED ACCESS DOOR CUTOUT AT WS 12/245 IAW BOMBARDIER REO 601R-57-21-030 REV C. (MSDR QXEA200400876Skin · corrodedPDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT HAND WING BETWEEN STATION YW98.6-117.5. REPAIRED IAW RD 8/4-57-399 HORIZON AIR EA 6-57-268 AND SRM 51-21-10.SDR IXXA0500114SPlate · dentedDURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD AILERON UPPER OUTBOARD PLATING DENT DAMAGE AT STA XA 726.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN IAW DC8 SRM 51-1-21 PG1. FABRICATED NEW SKIN + FINGER DOUBLER IAW DC8 SRM 57-8-1 PG 9 FIG 4.SDR USAA041077Skin · delaminatedPIT - WALKAROUND- WING T/E, 8 INCH X 12 INCH AREA, DELAMINATION, UPPER PANEL OB RT FIXED T/E OF WING. REPLACED PANEL IAW SRM AND EA.SDR IXXA0500113SPlate · corrodedDURING A C CHECK INSPECTION, RT OUTER WING OUTBOARD EXTENDED LEADING EDGE OUTER PLAING UPPER SIDE CORROSION DAMAGE AROUND STA XFS 716.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION FROM RT WING OUTBD L/E UPPER SKIN AND IT WAS FOUND OUT OF LIMITS IAW DC8 SDR IXXA0500080SSkin · damagedDURING A C-CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN WITH INTERIM REPAIR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED PLATING PANEL. FABRICACTED NEW PLATING PANEL. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING PANEL INTERNAL PART. APPSDR DXTA200400476Skin · corrodedDURING HEAVY MAINTENANCE FOUND CORROSION AT RIGHT WING TIP AND LEFT WING UPPER SKIN. ITEM IS BEING REPAIRED.SDR IXXA0500108SSkin · damagedDURING A C CHECK INSPECTION, FOUND RT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AROUND STA XILD 7095. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS IAW DC8 SRM 51-1-21 PG 1,DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW SEMAN DWG EO 3792 DC8 NDSDR IXXA0500086SSkin · damagedDURING A ROUTINE C CHECK INSPECTION FOUND LT L/E WING INBOARD EXTENDED L/E OUTER PLATING INTERIM REPAIR AROUND STA XSF 710.000. MAJOR REPAIR ACCOMP IAW FAA FORM 8110-3 NR 04592, DWG SEMON EO 3787. REMOVED FASTENERS IAW DC8 SRM 51-1-21 AND SRM 51-1-20D. REMOVEDSDR 04FDEA03392Skin · bulgedLEFT WING, UPPER SURFACE AT APPROX STA 980 XORS FORWARD OF OUTBOARD AILERON TOP SURFACE FIXED PANEL BULGING. REPAIR CARRIED AT LT WING FORWARD UPPER SURFACE OF OUTBOARD AILERON AT APPROX. STA 980 XORS AS PER SRM 57-20-00 FIG 16 VOL I.SDR ASOA04974Skin · crackedDURING A C-CHECK IN MCN, THE LOWER WING PLANKS AT WS 148.019 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANKS AT WS 148.019 LHS/RHS IAW ASA EO 600-57-0134A. (M)SDR GTIA040865Access Panel · damagedFTW - FOUND LEFT WING INBOARD BUTTE DOOR INBOARD EDGE, BOTTOM SIDE IS DAMAGED. BLENDED OUT DAMAGE MATERIAL LOSS OUT OF LIMITS, FABRICATED NEW DOUBLER, DRILLED AND LOCATED HOLES. OK TO TREAT, PRIME AND INSTALLED DOUBLER. (M)SDR DHL2004873545Skin · crackedLT WING INBOARD L/E CRACKED 3.000 IN LWR SKIN SURFACE (STA XFS 622.500 - 628.725) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R14, REV: IR DATED 11-22-04, FAA FORM 8110-3 DATE 11-29-2004. REMOVED EXISTING REPAIR DOUBLER IAW DWG W90-R14, SRM 51-1-20D PG SDR DHL2004873553Skin · crackedLT WING INBOARD L/E LWR SKIN CRACKED 0.500 AT XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R01, REV IR DATED 11-08-04 FAA FOMR 8110-3 DATED 11-30-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAGED SECTION IAW DWG WSDR 04FDEA03307Skin · corrodedRIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 1042 FOUND CORRODED. REPAIR CARRIED OUT AT RIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 1042 AS PER EA 1-5710-79795.SDR 04FDEA03306Skin · corrodedRIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 980 FOUND CORRODED. REPAIR CARRIED OUT AT RT WING REAR SPAR UPPER SKIN AT STA XORS 980 AS PER EA 1-5710-79795.SDR 04FDEA03257Panel · delaminatedLEFT WING PANEL OVER AFT TRUNNION HAS MANY AREAS OF DELAMINATION. REPAIRED AFT TRUNNION PANEL ARC0269-503 BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC GWG ARC0269 AND FEDEX EA 8-5710-83945, WINGS- LEFT HAND MAIN LANDING GEASDR 04FDEA03256Panel · dentedLEFT HAND WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF MAIN LANDING GEAR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED PANEL PART NUMBER ARC0263, BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, DOUBLER AND CORE IAW RPS 1001 REV E, DAC PRINT ARC0263 AND SDR 04FDEA03210Skin · damagedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING OUTBD AILERON B/T STA XOA1006/1023 FOUND LOWER SIDE FASTENERS PULLED THROUGH IN THE SKIN AND 1EA WITH HEAD BROKEN. REPLACE SKIN PER SRM 51-35-01 PG 1-12 AND REBALANCE PER SRM 57-50-00.SDR 04FDEA03209Skin · delaminatedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND LT WING INBOARD ISLAND UPPER SKIN WITH FINGER DOUBLER DELAMINATED. REPLACE UPPER SKIN PER SRM 51-35-01 PG 1-12 AND SRM 51-35-01 PG 34-47.SDR UPS04843570Doubler · crackedRT WING L/E INTERNAL DOUBLER (AUX TANK) CRACKED AT STA.182.502. FABRICATED REPAIR DOUBLER FROM SHT7075T6/0.125 AND INSTALLED SAME PER SAA SK744-520, SRM 51-1-8, 51-1-26, 51-1-20D.SDR DL73S041057Skin · wornLT LOWER WING SKIN WORN AT FUEL TANK ACCESS DOOR CUTOUT. REPAIRED IAW ERA 094867-14.SDR MALA040895Skin · dentedDURING C-CHECK INSPECTION IN YYC, A DENT WAS FOUND ON RT WING LEADING EDGE. MAINTENANCE REPAIRED LEADING EDGE IAW EO NR A57080. AIRCRAFT RETURNED TO SERVICE 11/23/2004.SDR UPS04143542Skin Panel · crackedRT WING T/E OUTER SHROUD BOX INNER SKIN PANEL CRACKED. R & R PANEL ASSY IAW EO A300-5720-21353. DMI CLOSED.SDR 04FDEA03173Skin · damagedRIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650KB HAS 1 EA ELONGATED SCREW HOLE AS MARKED AREA RIB 23 TO 24. COMPLIED WITH FED EX ENGINEERING AUTHORIZATION 6-5710-83632 (NOTE: MAJOR REPAIR PER EA ).SDR 04FDEA03172Skin · damagedRIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650 HB HAS 6 EA ELONGATED SCREW HOLES AS MARKED AREA RIB 21 AND 22. COMPLIED WITH FEDEX ENGINEERING AUTHORIZATION 6-5710-83632.SDR 05FDEA00380Doubler · corrodedLEFT WING UPPER GEAR DOUBLER CORRODED. CORROSION WAS BLENDED OUT AND REPAIRED WITH FILLER AND DOUBLER IAW FEDEX EA 8-571-84840.SDR USAA040975Skin · corrodedPIT - Q6 - WING SKIN CUTOUT, .5 INCH X .75 INCH AT (4) LOCATIONS, CORROSION; NO LEVEL OR TASK; LT WING 7403L PANEL FUEL BOOST PUMP ACCESS AREA. REMOVED CORROSION AND REPAIRED IAW DRAFT EA 79514.SDR 04FDEA03132Access Panel · delaminatedLEFT WING ACCESS PANEL NR 541JB HAS 4 EACH DENTS ON LOWER SURFACE. REPAIRED LEFT HAND WING ACCESS PANEL P/N ARC0585, BY FABRICATING AND BONDING NEW INNER AND OUTER SKINS, DOUBLER AND CORE IAW FEDEX EA 8-5710-81522 AND TPS 1001 REV E AND DAC PRINT ARC0585. RESDR QXEA200400774Panel · corrodedPDX - FUEL PANEL 622AT HAS ALL COUNTERSINKS THAT HAVE PITTING CORROSION. REPLACED IAW WORK CARD 600ME2860267.
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