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 DHL2003807531Skin · corrodedLEFT WING INBD L/E EXTERIOR SKIN CORRODED AT STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED EXISTING DOUBLER AND TRIPLER. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED AND REMOVED DAMAGED AREAS. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001. SDR 2003FA0001063Skin · corrodedAFTER REMOVAL OF NACELLE AUX FUEL TANK, DISCOVERED A LARGE AREA OF CORROSION ON THE TOP WING SKIN. THE TANK HAD TRAPPED MOISTURE BETWEEN IT AND THE WING TOP OVER A PERIOD OF YEARS. THE CORROSION WAS CLEANED AND THE SKIN HAD LOST LESS THAN 10 PERCENT OF ITS ORISDR DHL2003807522Doubler · crackedLEFT OTBD L/E STUB WING DOUBLER CRACKED AT STA XOLDO 67.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 2. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED DOUBLER (7075-T6AL 0.125) IAW SRM 57-2-1A FIG 2. CLEANED, TRSDR DHL2003807512Skin · corrodedRIGHT OUTER WING OUTBD L/E UPPER SKIN CORRODED STA XFS 716.250 - XFS 735.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 TR 57-85. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT DAMAGED ARSDR QXEA200301320Panel · chafedLT INBOARD WING LEADING EDGE IS CHAFED JUST ABOVE PANEL 522DB. REPAIRED IAW HORIZON AIR EA R-57-48A, EO 601R-57-4253A AND CRJ-700 AMM TASK 27-50-00-710-801.SDR UPS03441500Panel · debondedINSPECTION TYPE: C, RT WING I/B FIXED T/E PANEL UPPER SURFACE ONE LOCATION FOUND DEBONDED AS RED MARKED AT WBL 237 APPROX. RT WING I/B FIXED T/E PANEL UPPER SURFACE REPAIRED AS PER SRM 57-30-04 FIG 7. PERFORM REINSPECT AT EACH A-CHECK AS PER UPS EO B747-572SDR 2003UALA00767Access Panel · damagedLEFT WING INBOARD FLAP LOWER ACCESS PANEL 8407L DAMAGED AT ATTACH HOLE COUNTERSINK. MAJOR REPAIR ACCOMPLISHED. REPLACED PANEL.SDR 0704007Panel · delaminatedL MLG T/E UPPER FIXED PANEL DELAMINATED ON UPPER AND LOWER SKIN.SDR A6WA200360045Skin · delaminatedDENTS ON THE LEFT AND RIGHT WING NOW SHOWING SIGNS OF DELAMINATION. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810001. (M)SDR ABXA030381Skin · cracked11 EACH HOLES HAD CRACK INDICATION ON RIGHT WING 505F PANEL. REMOVED -19 CLIP, FABRICATED NEW CLIP, ALODINED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND DWG NR 5613609. FABRICATED EXTERNAL DOUBLER AND INNER DOUBLER IAW REA D857-48044MR, ALODINED, PRIMED AND INSSDR GTIA030870Panel · delaminatedFOUND RIGHT WING BOTTOM TRAILING EDGE TRAP PANEL JUST FORWARD OF RT MLG DELAMINATED. REMOVED RIGHT WING BOTTOM TRAP PANEL. REPAIRED RT WING BOTTOM TE TRAP PANEL INSTALLED RIGHT BOTTOM TE TRAP PANEL. (M)SDR GTIA030882Panel · delaminatedFOUND LEFT WING LOWER TRAP PANEL MLG DELAMINATED. REMOVED LEFT WING LOWER TRAP PANEL. REPAIRED LEFT TRAP PANEL. INSTALLED PANEL. (M)SDR AMTA200301240Skin · crackedFOUND LEFT UPPER WING SKIN CRACKED PAST STOP DRILL. AT AFT SPAR FORWARD OF INBOARD FLAP PYLON. STOPPED DRILLED/HFEC COMPLETE, COLD WORKED HOLE AND FINAL REAMED TO .250 PER SRM 57-32-00, TREATED PRIMED AREA IAW SRM 51-21-00. (M)SDR DHL2003749515Skin · corrodedDURING C-CHECK, WING CENTER SECTION LOWER SKIN CORRODED ABOVE RT PRIMARY HEAT EXCHANGER. REMOVED CORROSION IAW B-727 SRM 51-10-6 WITH A MAT LOSS OF .057 AREAS FOUND TO BE OUT OF LIMITS IAW B-727 SRM 57-30-1 FIG 4 TABLE I FIG 5, PARA 2 FABBED DOUBLER FROM 2024SDR 2004F00038Skin · corrodedDURING INSPECTION SEVERAL AREAS OF CORROSION FOUND ON LT/RT WING PLANK UPPER LEADING EDGE. REPAIRED BY BLENDING AND REPAIR IAW MFG DRAWINGS SE45632105, SE35803160, SE35803176 AND SE35803002. (M)SDR DHL2003749514Skin · dentedDURING C-CHECK, SKIN DENT LT WING LEADING EDGE AT LEADING EDGE STA 130 (ABOVE I/B EDGE OF NR 3 L/E FLAP). CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .040 PO 90020 DIM 2.5 X 1.5 INCHES AND DOUBLER FROM 2024 T3 .050 PO 90096 DIM 6.5 X 6 INCHES IAW B-72SDR DHL2003749500Skin · dentedDURING C CHECK, SKIN DENT LT WING L/E AT LEADING EDGE STA. 130 ( ABOVE IB EDGE OF NR 3 LE FLAP ). CUT-OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .040 P.O. NR 90024 DIM 2.5 INCH X 1.5 INCH AND DOUBLER FROM 2024 T3 .050 P.O. NR 90096 DIM. 6.5 INCH X 6 INCHSDR DHL2003749506Skin · crackedDURING C-CHECK, WS 464 UPPER LT WING L/E SURF IS CRACKED AT RIVET. REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 2.375 X 1.25 INCH AND FABBED DOUBLERS FROM 2024 T3 .050 INCH PO 90096 DIM 7.25 X 6 X 7.25 X 4.5 INCH AND FILLER FSDR DHL2003749501Skin · crackedDURING C-CHECK, WS 464 UPPER LT WING L/E SURFACE IS CRACKED AT RIVET (SKIN). REMOVED FASTENERS AS REQUIRED IAW B-727 SRM 51-30-2 AND CUT OUT DAMAGED AREA DIM 2.375 X 1.25 INCHES. FABBED DOUBLERS FROM 2024 T3 .050 PO 90096 DIM 7.25 X 6 INCHES AND 7.25 X 4.5 ISDR UPS03841342Skin · crackedINSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 597.5. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.SDR CALA0300537Skin · crackedINSPECTION FOUND AN 8 INCHES CRACK IN LT WING FIXED LEADING EDGE SKIN AT OSS 421-471. THE SKIN WAS REPAIRED IAW ECRA 5721-01010, REV. D.SDR AWXA200301067Skin · crackedDURING C-07 CHECK A .5 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 3 SLAT AFT INBOARD EDGE UP STOP PAD, RIB 15. MAINTENANCE REMOVED UP STOP PAD AND BLENDED OUT CRACK ON LT WING LEADING EDGE SKIN RIB 15; FABRICATED A REPAIR DOUBLER AND NEW REPLACEMSDR QXEA200301128Skin · dentedBOI- DURING WALKAROUND ON LINE CHECK FOUND A DENT IN LEFT HAND WING BOTTOM SKIN, BETWEEN STATIONS 510 AND 494 JUST AFT OF LEADING EDGE PANELS 513DL AND 513CL. REPAIRED IAW HORIZON AIR EA 6-57-176.SDR GTIA030729Skin Panel · corrodedFOUND CORROSION AND TOOL MARKS ON LE PANEL NR 1117C LEFT WING. TWO BLENDED AREAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. (M)SDR AUS20030902Skin · corroded(AUS) RT WING VENT TANK UPPER SKIN LOWER SURFACE CORRODED. LOWER CHORD OF REAR SPAR AND WEBS OF STIFFENERS NR 9 AND NR 10 ALSO CORRODED.SDR IXXA060573SSkin · scratchedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SCRATCHED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-1, 51-1-8, AND 51-1-20D.SDR DHL2003805600Panel · delaminatedRIGHT CTR WING LOWER PART PANEL NR 721 INTERNAL SKIN DELAMINATED AT STA 730.000. REMOVED AND REPLACED NR 721 PANEL ON RIGHT CTR WING, STA 730.000. FOR REMOVAL SEE JC 8-10-30-003, FOR INSTALLATION SEE JC 8-90-30-003.SDR AUS20030895Panel · misinstalled(AUS) LT OUTBOARD SURGE TANK ACCESS DOOR INCORRECTLY FITTED. FUEL LEAKING. DOOR WAS DAMAGED DUE TO BEING FITTED 180 DEGREES OUT.DOOR IS FITTED WITH ONE RAISED NUT WHICH FITS INTO ACORRESPONDING NOTCH TO PREVENT INCORRECT FITMENT. PERSONNEL/MAINTENANCE ERROR.SDR AWXA200301146Panel · chafedLCQ - MAJOR REPAIR - DURING C-16 CHECK THE RT WING TRAILING EDGE CLOSE-OUT PANEL CHAFED AT WBL 200. MAINTENANCE FABRICATED AND INSTALLED A REPAIR PLATE ON CLOSE-OUT PANEL AT WBL 200 IAW B737-300 SRM 51-20-01 PARA G.SDR 03FDEA01447Skin · corrodedMAIN DECK- CTR AUX TANK UPPER SKIN EXTERIOR SURFACE FOUND CORRODED AT STA 1239, LBL 24. MAIN DECK STA 1239 LBL 24 CTR AUX TANK UPPER SKIN CORROSION REPAIRED AS PER SRM 57-00-01 VOL 1 AND EA 1-5720-72606 FUSELAGE. MAINFRAME - UPPER CTR WING SKIN CORROSION REPSDR 03FDEA01523Skin · corrodedLT WING - UPPER SURFACE, STA 118 TO 162, FWD AREA BETWEEN FRONT AND REAR AREA, NUMEROUS PLACES FOUND CORRODED. LT WING UPPER SURFACE, NUMEROUS CORRODED PLACES AT FORWARD AREA BETWEEN FRONT AND REAR AREA STA 118 TO 162 BLENDED OUT AS PER SRM 51-21-01 VOSDR DHL2003805531Skin Panel · delaminatedLEFT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED (STA XW.5.000 - 47.00). REMOVED AND REPLACED LWR WING T/E LWR PANEL (STA XW.5.000 - 47.000) IAW SRM 51-3-0 PG 1.SDR DHL2003805580Skin · damagedRIGHT INNER WING CTR EXTENDED L/E SLOT OUTER PLATING SHOWS ELONGATED HOLES AROUND STA XW.257.000 (MAJOR REPAIR). PERFORMED MAJOR REAPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FASDR DHL2003805588Skin · damagedRT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AT STA XS 247.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER EXTERNAL DSDR SWAA031924Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER SKIN CRACKED AT WBL 181. REPAIRED SKIN PER SWA EA.SDR DHL2003805579Skin · corrodedRIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING CORRODED, AROUND STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND SDR DHL2003805577Skin · damagedLEFT WING OTBD FLAP UPPER PLATING HAS INTERIM REPAIR AROUND STA XF 225.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGSDR DHL2003805576Skin · damagedLEFT WING OTBD FLAP UPPER SKIN SHOWS INTERIM REPAIR AROUND XF 345.000 TO STA XF 354.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8SDR UPS03841202Skin · corrodedINSPECTION TYPE: C2, RT WING LE UPPER SURFACE HAS 6 CRACKED FASTENER HOLES BETWEEN XFS 597.5 TO XFS 628.75. BLENDED OUT CORRODED AREAS, CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLER AND FILLERS I.A.W SRM. 57-2-1 FIG. SDR DHL2003805584Skin · corrodedRIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING HAS CORROSION AROUND STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PSDR DHL2003805586Skin · corrodedRIGHT OUTER WING INBD EXTENDED L/E SHOWS CORROSION AND ELONGATED HOLES AROUND STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. CUT OUT CORRODED AREA. PERFORMED NDT INSPECTION. FABRICATED SDR 2003FA0000862Panel · departedWING BOLT PANEL DEPARTED AIRCRAFT WHILE IN FLIGHT. THIS IS THE THIRD OCCURANCE ON THREE DIFFERENT AC IN APPROXIMATELY ONE MONTH. INSPECTION REVEALED THE THE SPRING TAB HAD FAILED. RECOMMEND CLOSE INSPECTION OF THIS PANEL AT EACH PHASE INSPECTION.SDR DHL2003805585Skin · delaminatedLEFT WING FUSELAGE NR 706 UPPER FAIRING SKIN DELAMINATED, STA 912.000 - STA 980.000. REMOVED AND REPLACED LEFT WING TO FUSELAGE UPPER FAIRING NR 706 (STA 912.000 - 980.000) IAW SRM 51-3-0 PG 1.SDR QXEA200301027Skin · scratchedSEVEN INCH SCRATCH ON TOP SIDE OF LEFT HAND WING 6 INCHES AFT OF FORWARD SPAR STATION YW207. REPAIRED IAW DHC-8 SRM 51-20-11, 51-00-06, 51-00-02 AND 51-00-04.SDR COMA0360377Skin · crackedDURING COMPLIANCE OF SERVICE BULLETIN S/B A601R-57-031, A CRACK WAS FOUND IN THE LEFT WING LOWER PLANK IN THE AREA OF THE REAR SPAR AT WS 148.019. THE PLANK WAS REPAIRED PER BOMBARDIER REO 601R-57-21-351.SDR DHL2003805514Skin · crackedLEFT WING T/E UPPER SKIN SURFACE 0.500 CRACKED, STA XW 31.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-15 PG 1, SDR CALA0300467Panel · delaminatedINSPECTION FOUND RT WING PANEL UPPER SURFACE DELAMINATED O/B OF MLG. THE PANEL WAS REPAIRED IAW BOEING DRAWING 65-50820-188.SDR DHL2003805505Panel · delaminatedLEFT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XA 450.000 - XA 475.000). REMOVED UPPER PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ON LT WING T/E, STA XA 450.000 - XA 475.000 IAW SRM 51-3-0 PG 1SDR 2003FA0000845Skin · crackedDURING ANNUAL INSPECTION, FOUND 20 STRESS CRACKS ON TOP OF BOTH WINGS ALONG BOTH LONGITUDINAL STRINGERS AFT OF MAIN SPAR. CRACKS RANGE FROM .250 INCH TO .750 INCH IN LENGTH, AND PROPOGATE ENTIRE LENGTH OF WINGS. SUSPECT CRACKS CAUSED BY OVER-STRESS OF AIRCRASDR 2003FA0000844Skin · crackedDURING ANNUAL INSPECTION, FOUND LEFT WING INBOARD FORWARD SKIN AT ROOT WITH SPIDER CRACKS IN 2 AREAS. ALSO FOUND WALKWAY SURFACE MUSHY, SUSPECT INTERNAL DAMAGE. SUSPECT CRACKS CAUSED BY OVERSTRESS OF WINGS DURING FLIGHT. REPAIR- IN WORK.
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