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.

SDR DHL2003604602Skin · damagedLT WING EXTENDED L/E OTBD. VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA. XOLDI 67.000 PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED EXISTING INTERIM REPAIR AND FILLER. TRIMMED OUT DAMAGED SKIN AREA IAW EODHL-030545, ED-3302. PMay 24, 2003 · N604AL · Doug DC873FSDR CA030529003Stitching · broken(CAN) RIB STICHING BROKEN MOST RIBS RT WING RECORDS. ONLY GO BACK TO 1978 NO RECORD OF REPLACEMENT AT THAT TIME. FABRIC TESTED GOOD. (WING RESTITCHED.)May 23, 2003 · Piper PA18150SDR DHL2003604718Skin · crackedLT OUTER WING INBD L/E LOWER PLATING CRACKED 1.000, AROUND STA XFS 597.500. PERFORMED MAJOR REPAIR IAW EODHL-030527, ED-3290. REMOVED FASTENERS, PERFORMED STOP HOLE ON CRACK END USING 0.250 DIA DRILL IAW EODHL-030527, ED-3290. PERFORMED NDT INSPECTION IAW DMay 22, 2003 · N604AL · Doug DC873FSDR DHL2003604601Skin · corrodedRT. WING OB L/E UPPER SKIN CORRODED STA. XFS.710.000 PERFORMED MAJOR REPAIR IAW EODHL-030517, ED-3306. REMOVED FASTENERS AND EXISTING DOUBLER AND FILLER IAW SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM. FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. May 22, 2003 · N604AL · Doug DC873FSDR DHL2003604629Vane · elongatedLT WING CTR L/E VANE SLOT HOLES ELONGATED AT XOLDI 6.224. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT THE ELONGATED HOLES SKIN AREA. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR EXTERNAL DOUBLER (7075-T6 AL0.071), A FILMay 22, 2003 · N604AL · Doug DC873FSDR DHL2003604656Plate · corrodedRT OUTER WING OUTBD L/E UPPER PLATING CORRODED AT STA XW 761.000. PERFORMED MAJOR REPAIR IAW EODHL-030529, ED-3305. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED ANDMay 21, 2003 · N604AL · Doug DC873FSDR DHL2003604749Skin · damagedLT OUTER WING CTR. EXTENDED L/E SLOT HAS ELONGATED HOLES AT STA. XFS.526.000. (MAJOR REPAIR) PERFORMED MAJOR REPAIR IAW EODHL-030550, ED-3353. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. BLENDED OUT THE ELONGATED HOLES SKIN AREA IAW EODHL-030550, ED-3353. PEFORMEDMay 21, 2003 · N604AL · Doug DC873FSDR DHL2003604752Doubler · crackedRT OUTER WING CTR EXTENDED L/E SLOT INNER DOUBLER CRACKED (0.063) AT STA. XFS. 526.000. PERFORMED MAJOR REPAIR IAW EODHL-030532, ED-3350. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED ON CRACK END (0.250 DIA) IAW EODHL-030532, ED-3350. PERFORMED EDDY May 20, 2003 · N604AL · Doug DC873FSDR DHL2003604689Skin · crackedRT OUTER WING INBD EXTENDED L/E LOWER PLATING CRACKED 1.650 AROUND STA XFS 597.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 21. PERFORMED STOP HOLE ON CRACK END USING 0.250 DIA DRILL IAW EODHL-030520, ED-3352. PERFORMED EDDY CURRENT INSPECTION IAW NDT SPM PARTMay 20, 2003 · N604AL · Doug DC873FSDR DHL2003604553Skin · damagedINTERIM REPAIR ON TOP SURFACE OF LT WING L/E (STA XS 246.518-250.089) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38, TR NR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1May 20, 2003 · N604AL · Doug DC873FSDR ABXA030151Panel · crackedWHILE PERFORMING ROUTINE LINE MAINTENANCE, A FUEL LEAK WAS DISCOVERED AT THE LT WING FUEL PANEL 1307. FURTHER INSPECTION REVEALED A CRACK ON THE FUEL PANEL FLANGE. REPAIRED CRACK IAW DC-9 SRM 57-03, FIG 23.May 20, 2003 · N982AX · Doug DC932SDR DHL2003604554Skin · crackedLT WING OUTBOARD L/E UPPER SKIN CRACKED 1.500 AT XFS.207.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38, TR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38, TR 57-May 19, 2003 · N604AL · Doug DC873FSDR AALA20030604Skin · corrodedFOUND CORROSION ON WING CTR SECTION, UPPER SKIN STATION 955 BETWEEN BL0 AND LBL 10 MINIMUM THICKNESS AFTER BLEND ON AFT EDGE O.144 INCHES. REMOVED FASTENERS IN AFFECTED AREA AND REMOVED CORROSION, PERFORMED EDDY CURRENT INSPECTION. REWORKED AREA WITH FLAP PEMay 19, 2003 · N368AA · Boeing 767323SDR ASAA0310446Skin · wornOKC - DURING C-CHECK, FOUND LEFT WING LEADING EDGE AT WING STATION 360 WORN. REMOVED DAMAGE AND REPAIRED PER SRM. (M)May 15, 2003 · N742AS · Boeing 737290CSDR 2003F00502Access Panel · delaminatedAT C-CHECK,F OUND LEADING EDGE ROOT WING 192DT ACCESS PANEL DELAMINATED. REPAIR PANEL IAW SRM 51-73-00, PAGES 1 AND 2. (M)May 15, 2003 · N951LF · Airbus A320233SDR AWXA200300687Skin · corrodedDURING C-15 CHECK CORROSION WAS FOUND ON LT WING LOWER SURFACE SKIN AT NR 2 FLAP TRACK ATTACH POINT. MAINTENANCE REMOVED CORROSION ON LT WING LOWER SURFACE SKIN BY MACHINING A FLAT STEP; PERFORMED A HFEC INSPECTION TO VERIFY MACHINED AREA WAS NOT CRACKED; FABMay 15, 2003 · N178AW · Boeing 737277SDR QXEA200300653Skin · gougedCKB - RIGHT WING LEADING EDGE HAS A GOUGE ON THE TOP SIDE AT WS 163. REPAIRED IAW QX4 SUPPLEMENT 51-12-00.May 14, 2003 · N601QX · Cndair CL6002C10SDR QXEA200300652Skin · gougedCKB - LEFT WING, LOWER WING SKIN AT WS 128.00 HAS A GOUGE. REPAIRED IAW AMM 51-25-01.May 13, 2003 · N601QX · Cndair CL6002C10SDR DHL2003801070Panel · delaminatedLT LWR PANEL NR 723 AT STA 750.000 SHOWS DELAMINATED INTERNAL/EXTERNAL SKIN. REMOVED AND REPLACED LT LWR PANEL 723 AT STA 750.000 IAW SRM 51-3-0 PG 1.May 12, 2003 · N801DH · Doug DC873FSDR DHL2003604615Skin · corrodedLT OUTER WING IB L/E CORRODED AT STA. XFS.710.000. PERFORMED MAJOR REPAIR IAW EODHL-030509, ED-3314. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.11-12. TRIMMED OUT CORRODED SKIN AREA IAW EODHL-030509, EDMay 10, 2003 · N604AL · Doug DC873FSDR DHL2003604605Skin · corrodedLT WING CTR L/E UPPER SKIN SHOWS INTERIM REPAIR & CORROSION BETWEEN STA XFS 360.250 AND XFS 379.000. REMOVED FASTENERS AND INTERIM REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATEMay 9, 2003 · N604AL · Doug DC873FSDR GTIA030447Panel · delaminatedRIGHT WING INNER WING UPPER FORWARD TRAP PANEL DELAMINATING. FITTED AND DRILLED NEW RT WING INNER UPPER FORWARD TRAP PANEL. INSTALLED NEW RT WING INNER UPPER PANEL. (M)May 6, 2003 · N800NK · Doug DC982SDR DHL2003604539Doubler · crackedLT OUTER WING IB L/E LWR DOUBLER CRACKED 2.000, XFS.597.500. REMOVED DAMAGED DOUBLER IAW SRM 51-1-21 PG.1. FABRICATED NEW DOUBLER (7075-T6 AL 0.080) IAW SRM 57-1-0 PG.1, SRM 57-3-3 PG.16. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED May 5, 2003 · N604AL · Doug DC873FSDR GTIA030372Panel · delaminatedFOUND LT WING LOWER TRAP PANEL DELAMINATING. REPAIRED LEFT WING LOWER TRAP PANEL AT DELAMINATED. (M)May 5, 2003 · N800NK · Doug DC982SDR GTIA030363Panel · crackedFTW - FOUND LEFT WING INNER WING UPPER AFT TRAILING EDGE TRAP PANEL CRACKED/DAMAGE TO COMPOSITE MATERIAL. REPAIRED CRACK/DAMAGED AREA. (M)May 5, 2003 · N800NK · Doug DC982SDR DHL2003604501Panel · delaminatedLT WING LWR SURFACE- LT NR 540 LWR ACCESS DOOR OUTER SKIN DELAMINATED FROM XS 475.000 - XS 507.000. REMOVED AND REPLACED LT LWR ACCESS DOOR NR 540 (STA 475.000 - 507.000) IAW SRM 51-3-0 PG 1.May 5, 2003 · N604AL · Doug DC873FSDR GTIA030465Panel · corrodedFOUND RIGHT WING LEADING EDGE PANEL 1248C CORROSION AT FASTENER HOLES AND NUMEROUS GOUGES. MATERIAL OUT OF LIMITS. RECEIVED NEW R/W L/E PANEL. (M)May 4, 2003 · N800NK · Doug DC982SDR 04FDEA01659Doubler · corrodedBASIC WING STRUCTURE LEFT AND RIGHT LOWER DOUBLERS P/N ARB0983-1 AND -2 CORROSION. CORROSION REMOVAL AND DOUBLER INSTALLATION IAW FEDEX EA 8-5710- 70160.May 3, 2003 · N570FE · Doug DC1010SDR GTIA030331Skin · corrodedLT WING LE PANEL 1117C CORROSION AT FASTENER HOLES. FABRICATED DOUBLER. INSTALLED DOUBLER.May 3, 2003 · N800NK · Doug DC982SDR DHL2003801016Panel · delaminatedLT WING LOWER SURFACE- T/E LWR PANEL OUTER SKIN DELAMINATED STA XW 5.000- XW 47.000. REMOVED AND REPLACED LT WING T/E LWR PANEL BETWEEN STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1.May 3, 2003 · N801DH · Doug DC873FSDR DHL2003604547Doubler · crackedRT OUTER WING INBD L/E INNER LOWER DOUBLER CRACKED 2.500 AT XFS 598.500. REMOVED CRACKED INNER LOWER DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW INNER LOWER DOUBLER IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 26. CLEANED, TREATED AND PRIMED AREA AND NEW INNER LOWERMay 2, 2003 · N604AL · Doug DC873FSDR DHL2003604543Skin · damagedLT WING OUTBD L/E UPPER PLATING SHOWS ELONGATED HOLE AT XFS.710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG.38. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CUT OUT DAMAGED AREA IAW SRM 57-2-1 FIG.38. FABRICATED FILLER (7075-T6May 2, 2003 · N604AL · Doug DC873FSDR DHL2003604528Doubler · crackedRT OUTER WING INDB L/E INTERNAL DOUBLER CRACKED .500, STA XFS.572.500. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 & SRM 57-3-3 FIG 6. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED INTERNAL DOUBLER IAW SRM 57-3-3 FIG 6. FABRICATED NEW INTERNAL DOUBLERMay 2, 2003 · N604AL · Doug DC873FSDR 2003FA0000487Skin · crackedDURING ANNUAL INSPECTION, TWO CRACKS WERE FOUND ON THE LOWER LEFT WING SKIN, NEAR THE LOWER SPAR CAP, OUTBOARD OF THE MAIN LANDING GEAR DOOR HINGE. BOTH CRACKS WERE LOCATED NEAR THE DOUBLER, KIT NR 766-210, PREVIOUSLY INSTALLED IAW MFG SB. THIS AIRCRAFT HAS May 1, 2003 · N9173Z · Piper PA46350PSDR DHL2003604533Doubler · crackedRT WING- CTR L/E INNER PART DOUBLER CRACKED, XFS 322.750. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, IAW SRM 51-1-20D PG 21. FABRICATED NEW DOUBLER IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 14. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. INSTALLED DOUApr 30, 2003 · N604AL · Doug DC873FSDR 03FDEA00650Panel · gougedDEEP GOUGE IN RT WING L/E PNL 612B, FOUND TO BE OUT OF LIMITS PER IAW SRM 57-41-11. REPLACED PNL, TREATED, PRIMED AND PAINTED PER IAW SRM 51-40-44, SRM 51-75-10 AND SRM 51-21-10.Apr 29, 2003 · N682FE · Airbus A300B4605RSDR DHL2003604540Skin · damagedLT OUTER WING OUTBOARD L/E UPPER SKIN SHOWS INTERIM REPAIR, XFS 766.250 - XFS 778.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND Apr 28, 2003 · N604AL · Doug DC873FSDR A6WA200360018Skin · damagedLEFT WING INBOARD LEADING EDGE HAS 1 HOLE ENLARGED IN TOP SKIN ABOVE NR 2 PYLON. REPAIRED IAW RIL HC572H9066 AND FAX BARA/AVR/6362/03-DC. (M)Apr 23, 2003 · N610AW · Bac 146200ASDR A6WA200360017Panel · damagedLT WING LEADING EDGE PANEL 464AT HAS SEVERAL ELONGATED HOLES. REPAIRED IAW RIL HC5459009 AND FAX BARA/AVR/6365/03-DC.Apr 23, 2003 · N610AW · Bac 146200ASDR DHL2003741554Skin · damagedDURING C-CHECK DISCREPANCY AS FOLLOWS, LEFT WING I/B LEADING EDGE SKIN IS CREASED WBL 92.8. CUT OUT DAMAGED AREA 6 X 2.25 INCH AND FABBED FILLER FROM 2024-T3 .063 PO 9912380 AND DOUBLER FROM 2024-T3 .080 PO 9912495 DIM 10 X 7.5 INCH IAW B-727 SRM 57-30-4 FIG Apr 23, 2003 · N741DH · Boeing 727200SDR S03457018Skin · corrodedDURING C-CHECK, CORROSION FOUND ON THE RT WING LOWER SKIN FRONT SPAR CAVITY UPPER SURFACE, FSSO 1188 - 1197. AFTER REMOVING ATTACHED FITTING, PERFORM AN HFEC SURFACE AND OPEN HOLE INSPECTION. TO VERIFY NO DAMAGE EXISTS. THE BLENDED OUT DIMENSIONS ARE 2.5IN (WApr 22, 2003 · Boeing 747400SDR DHL2003801024Skin · corrodedLT OUTER WING INBOARD L/E OUTER PLATING CORRODED AT STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030402, ED3253. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16.Apr 21, 2003 · N801DH · Doug DC873FSDR DHL2003801008Skin · damagedLT WING CTR L/E SKIN SHOW ELONGATED HOLES AND INTERIM REPAIR AT XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030409, ED 3257. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW EO DHL 030409, ED 3257. CLEANED, TREATED ANDApr 21, 2003 · N801DH · Doug DC873FSDR DHL2003801025Skin · corrodedRT OUTER WING INBOARD L/E OUTER PLATING SHOWS CORROSION AT XFS 710.000. PERFORMED MAJOR REPAIR IAW EODHL-030403, ED3261. REMOVED FASTENERS, REMOVED CORROSION FROM RT OUTER WING INBOARD L/E OUTER PLATING. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT COApr 19, 2003 · N801DH · Doug DC873FSDR DHL2003801022Skin · corrodedLT OUTER WING OUTBOARD L/E UPPER PLATING CORRODED AROUND STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030414, ED 3267. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 Apr 18, 2003 · N801DH · Doug DC873FSDR DHL2003801023Skin · corrodedLT OUTER WING OUTBOARD L/E OUTER PLATING CORRODED AT STA XFS 710.000. PERFORMED MAJOR REPAIR IAW EODHL 030401, ED3255. REMOVED CORROSION ON LT WING OUTBOARD L/E STA XFS 710.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT CORRApr 18, 2003 · N801DH · Doug DC873FSDR DHL2003801018Skin · damagedLT WING CTR L/E LWR PLATING SHOW ELONGATED HOLES AT STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030411, ED3266. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (7075-T6 AL0.0Apr 18, 2003 · N801DH · Doug DC873FSDR DHL2003801012Skin · corrodedLT OUTER WING OUTBOARD L/E OUTER PLATING CORRODED AT STA XW 761.000. PERFORMED MAJOR REPAIR IAW EO DHL 030404, ED 3254. REMOVED CORROSION FROM LT WING OUTBOARD L/E OUTER PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMApr 18, 2003 · N801DH · Doug DC873FSDR EIA2003065Skin · corrodedRIGHT UPPER WING UPPER SURFACE OF LOWER SKIN HAS HEAVY CORROSION AT FWD SPAR LOWER CHORD AT WS 1323. REMOVED DAMAGE, INSPECTED AND NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 471-57-217-2 REV-A.Apr 17, 2003 · N471EV · Boeing 747273CSDR DHL2003801048Skin · elongatedLT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 410.250 AND XOLDI 6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED DOUBLER INNEApr 14, 2003 · N801DH · Doug DC873F
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