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 IXXA060164SSkin · gougedDURING ROUTINE C CHECK FOUND LT WING NR 1 MAIN-TANK-VENT FLOAT VALVE JUST OB OF XRS-358 HAS GOUGED UPPER SKIN. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, NEW FASTENERS AND SEALED REPAIJun 12, 2004 · N605AL · Doug DC873FSDR IXXA060434SPanel · delaminatedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE FIXED PANEL DELAMINATED AND NICKED AT STATIONS XW10, XW40, AND XW75. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862SDR IXXA060221SFillet · delaminatedDURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 162V DELAMINATED. REPAIRED PANEL PER COOPESA EO COO-CMP-8-53-273-04 DATED 07/15/2004.Jun 11, 2004 · N41CX · Doug DC862FSDR IXXA060159SPanel · dentedDURING ROUTINE C CHECK FOUND LT WING LOWER TRAILING IB FIXED PANEL HAS DENT AFT OF MAIN LANDING GEAR STRUT. REMOVED FASTENERS AS NEEDED TO REMOVE PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, TRIMMED, TREATED, APPLIED ADHESIVE, PERFORMED HOT BOND, INSTALLED Jun 11, 2004 · N605AL · Doug DC873FSDR 04FDEA01657Panel · corrodedLEFT MAIN LANDING GEAR, WING SUPPORT FITTING CORROSION IN THREE TAPER LOCK HOLES. CORROSION REMOVAL AND OVERSIZED TAPER LOKS INSTALLATION IAW FEDEX EA 8-5710-70153.Jun 10, 2004 · N388FE · Doug DC1010SDR IXXA060432SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD SLOT AREA UPPER SURFACE SKIN CORRODED. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862SDR IXXA060431SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS335.25. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862SDR IXXA060430SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED FROM STATION XW257 TO XW260. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862FSDR IXXA060429SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING UPPER IN BOARD PANEL (DIHEDRAL) SKIN, CORRODED. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862FSDR IXXA060428SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATIONS XFS -11.250 THRU XFS63.750. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862FSDR IXXA060220SFillet · delaminatedDURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262K DELAMINATED AND CORRODED. REPLACED PANEL PER COOPESA EO COO-8-53-304-04.Jun 9, 2004 · N41CX · Doug DC862FSDR IXXA060218SFillet · delaminatedDURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262F DELAMINATED AND CORRODED AT AFT FACE. REPLACED PANEL PER COOPESA EO NUMBER COO-8-53-304-04 DATED 08/06/2004.Jun 9, 2004 · N41CX · Doug DC862FSDR C7WA200400019Skin · corrodedFOUND WING CENTER SECTION UPPER SKIN CORRODED RBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232SDR C7WA200400020Skin · corrodedFOUND WING CENTER SECTION UPPER SKIN CORRODED LBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)Jun 9, 2004 · N511PE · Boeing 727232SDR IXXA060426SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATION XW250. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862FSDR IXXA060424SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE LOWER SKIN CORRODED FROM STATION XFS735 TO XFS885. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862SDR IXXA060421SPanel · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE LOWER PANEL CORRODED AROUND SCREWS AT STATION XRS169. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862SDR SWAA041583Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT WING L/E SKIN CUTOUT AT WS 210, CRACKED. REPAIRED SKIN PER EA.Jun 4, 2004 · N634SW · Boeing 7373H4SDR SWAA041568Skin · crackedDURING SCHEDULED C3 CHECK, FOUND LOWER WING SKIN OUTBOARD NR 1 ENGINE, CRACKED. REPAIRED SKIN PER EA.Jun 3, 2004 · N338SW · Boeing 7373H4SDR UPS04242576Panel · crackedINSPECTION TYPE: C, CRACK ON LT WING T/E PANEL UPPER SURFACE FWD OF NR 5 SPOILER. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-02 & 51-10-02.May 31, 2004 · N950UP · Boeing 72725CSDR UPS04242570Skin · crackedINSPECTION TYPE:C SUSPECT CRACK IN SKIN AT LT WING ICE LIGHT CUTOUT (UPPER FWD). REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING 2004-054-004 & SRM 51-30-02 & 51-00-00.May 29, 2004 · N950UP · Boeing 72725CSDR CA040709007Skin · crackedLT WING AT STA 174.50 FOUND TO HAVE HAIR LINE CRACK FROM RIVET FORWARD OF STRINGER AHEAD OF THE MAIN SPAR.May 28, 2004 · Piper PA31350SDR SWIA200413383Panel · crackedLEFT WING LWR WING PLANK IS CRACKED WS 148.019. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21-130 REV. E AND REO 601R-57-21-131 REV. NC.May 28, 2004 · N416SW · Cndair CL6002B19SDR COMA0460337Skin · crackedWORK IN PROGRESS ON DMI 848101, LONG CRACK AT RT WING LOWER PLANK AT WS 148.019. REPAIRED LOWER RT WING PLANK WS 148.019R IAW REO 601R-57-21-130May 28, 2004 · N927CA · Cndair CL6002B19SDR COMA0460336Skin · crackedWORK IN PROGRESS ON DMI 800602, LOWER LT WING PLANK HAS .625 INCH CRACK ALONG WS 148. REPAIRED LOWER LEFT WING PLANK WS 148.019L PER REO 601R-57-21-130.May 28, 2004 · N927CA · Cndair CL6002B19SDR DJFA2004007Skin · corrodedDURING INSPECTION OF THE WING AFTER LEADING EDGES WERE REMOVED CORROSION WAS FOUND ON THE WING SKIN SURFACES WERE THE LEADING EDGES FIT ON. RAYTHEON AIRCRAFT WAS NOTIFIED AND A FIELD REPAIR FOR REMOVING THE CORROSION WAS APPROVED. ALL CORROSION WAS CLEANED AMay 26, 2004 · N867CW · Braero BAE125800ASDR DJFA2004008Skin · corrodedDURING INSPECTION OF THE WING, AFTER LEADING EDGES WERE REMOVED, CORROSION WAS FOUND ON THE WING SKIN SURFACES WHERE THE LEADING EDGES FIT ON. RAYTHEON AIRCRAFT WAS NOTIFIED AND A FIELD REPAIR FOR REMOVING THE CORROSION WAS APPROVED. ALL CORROSION WAS CLEANEMay 26, 2004 · N867CW · Braero BAE125800ASDR QXEA200400372Plate · chafedPDX - LIGHT CHAFING ON LADDER PLATE UNDER STRESS PANEL 622AT AT IB END, ON REAR SIDE FROM YW90 TO YW106 AND ON FORWARD SIDE FROM YW90 TO YW139. REPAIRED IAW DHC-8-200 MM 20-32-02 AND 20-34-08.May 26, 2004 · N357PH · Dhav DHC8202SDR F3LA200400063Panel · crackedDURING C-6 CHECK, INSPECTION REPORTED RT WING UPPER SURFACE AFT PYLON PANEL CRACKED AT AFT I/B CORNER AT FASTENER COMMON TO FUEL CELL. REPLACED PANEL PER SRM 51-40-02 AND 51-40-65.May 23, 2004 · N312FL · Boeing 7373L9SDR ENHA2004P3102Skin · damagedPILOT REPORTED INSPECTION OF AIRCRAFT REQUIRED AFTER LANDING. PILOT REPORTED THAT AIRCRAFT ENCOUNTERED EXTREME SEVERE TURBULANCE UPON DEPATURE FROM GOOD NEWS BAY, ALASKA. VISUAL INSPECTION DETERMINED THAT THE LEFT WING ENCOUNTERED SEVERE STRESS FORMING WRINKMay 22, 2004 · N4105D · Piper PA31350SDR 04FDEA01389Skin · gougedLEFT WING DROOPED LEADING EDGE O/B L/E HAS GOUGE. REPAIRED LEFT WING DROOPED L/E IAW SRM 57-00-01. GOUGE FOUND OUT OF LIMITS BY NTSPM 04-00-03 .070 BEFORE .045 AFTER. REMOVED & REPLACED BROKEN BRACKET ON O/B RIB IAW SRM 57-00-01, REMOVED AND REPLACED WORN May 21, 2004 · N68056 · Doug DC1010SDR SIMA200415414Skin · chafedDURING A MBV INSPECTION OF THE RIGHT WING TO NACELLE FILLET AREA THE INBOARD SIDE WAS FOUND TO BE CHAFED. BLENDED CHAFED AREA. PERFORMED AND EDDY CURRENT INSPECTION OF BLENDED AREA. NO CRACKS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. WORK DONE IAW SAMay 19, 2004 · N388AE · Saab 340BSDR 04FDEA01328Skin · chafedFIXED LEADING EDGE SKIN BEHIND NR 3 SLAT CHAFED. REPAIRED AS PER SRM 57-10-00 FIG 15 VOL I.May 18, 2004 · N609FE · Doug MD11SDR ASAA0480433Panel · corrodedOKC - DURING HV CHECK, FOUND RT WING FUEL PANEL 1462 HAS LIGHT SURFACE CORROSION. REMOVED DAMAGE AND REPLACED WITH NEW FUEL PANEL IAW 51-22-2A. (M)May 17, 2004 · N979AS · Doug MD83SDR ASAA0480429Panel · corrodedDURING HV CHECK, FOUND FUEL PANEL NR 1478C HAS SURFACE CORROSION ON INSIDE FLANGE. REMOVED DAMAGE AND REPLACED FUEL PANEL IAW 51-22-2A. (M)May 17, 2004 · N979AS · Doug MD83SDR IXXA0400085SPlate · wornDURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP L/E UPPER PLATING WEAR AT STA XF 211.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED WORN PLATING IAW DC8 SRM 51-1-21 PG 1 FABRICATMay 15, 2004 · N830BX · Doug DC871FSDR DHL2004803546Panel · delaminatedLT WING T/E LWR HONEYCOMB PANEL INTERIOR AND EXTERIOR SKIN DELAMINATED (STA XF 219.000-339.000). REMOVED AND REPLACED HONEYCOMB PANEL TO LT WING INBD T/E (STA XF 219.000-339.000) IAW DC8 SRM 51-3-0 PG 1.May 12, 2004 · N803DH · Doug DC873SDR DHL2004802005Bracket · crackedINBOARD SLOT, RT WING BRACKET ASSEMBLY CRACKED AT MOUNTING AREA. INSTALLED BRACKET ASSEMBLY P/N: 3770292-1 (I/B AT WING SLOT) IAW DC-8 M/M 22-80-1.May 12, 2004 · N802DH · Doug DC873SDR 2004FA0000381Wing · buckledAIRCRAFT WAS LOOPED, SPUN, AND BARREL ROLLED. PILOT WAS/IS STILL FLYING CLUB PLANES AND ANOTHER VISUAL. A RECENT LOOK AT THE AIRCRAFT INDICATES POSSIBLE STRUCTURAL DAMAGE AT THE WING ROOTS. GETTING INDICATIONS FROM OTHER PILOTS THAT THIS WAS NOT AN ISOLATED May 11, 2004 · Cessna 310HSDR 2004FA0000380Wing Root · buckledAIRCRAFT WAS LOOPED, SPUN, AND BARREL ROLLED. INFORMED, BUT NOTHING WAS DONE. PILOT WAS/IS STILL FLYING CLUB PLANES AND ANOTHER VISUAL. A RECENT LOOK AT THE AIRCRAFT INDICATES POSSIBLE STRUCTURAL DAMAGE AT THE WING ROOTS. GETTING INDICATIONS FROM OTHER PILOTMay 11, 2004 · Cessna 310HSDR COMA0460316Skin · crackedLEFT LOWER WING PLANK CRACKED. REPAIRED IAW REO 601R-57-21-130.May 9, 2004 · N959CA · Cndair CL6002B19SDR 2004F00415Skin · corrodedAFTER REMOVAL OF THE LT WING DEICE BOOT, CORROSION ON THE IB WING SKIN WAS FOUND. THE DAMAGE WAS MEASURED AND FOUND TO EXCEED THE MANUFACTURERS LIMITS REQUIRING WING SKIN REPLACEMENT. THE DAMAGE WAS LIMITED TO CORROSION PITTING, NONE HAD PENETRATED THOUGH THMay 7, 2004 · N962J · Cessna 550SDR AUS20040354Skin · corroded(AUS) RT WING TIP TRAILING EDGE CORRODED. CORROSION ALSO FOUND UNDERSTATIC DISCHARGER BASE.May 6, 2004 · Fokker F28MK0100SDR UPS04442359Panel · delaminatedREF D277226 RT WING FIXED UPPER LEADING EDGE PANEL HAS DELAMINATION. ACCOMPLISH TEMP REPAIR. REMOVED PANEL FROM A/C. REPLACED RT WING UPPER LEADING EDGE PANEL AS PER SRM 51-30-02. THIS CLEARS D277226.May 6, 2004 · N522UP · Boeing 747200SDR CALA0400461Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-40-01, FIGURE 201, PROCEDURE 2.May 4, 2004 · N14337 · Boeing 7373T0SDR IXXA0400071SSkin Panel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CTR LE UPPER SURFACE CORRODED AT STA XFS 341.500. REPAIR WAS ACCOMPLISHED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-8 PG 17-18 AND 57-2-1 PG 11. TOOK OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 38, May 1, 2004 · N830BX · Doug DC871FSDR IXXA0400070SPanel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WIND IB LE SLANT PANEL UPPER CAP CORRODED AT SEVERAL AREAS. STA XW.0 - XFS 164.000. REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITMay 1, 2004 · N830BX · Doug DC871FSDR IXXA0400069SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CENTER LE HAS REPAIR ON UPPER SURFACE, STATION XFS 304.000. THIS REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIG 38 TR NR 57-85, 51-1-21, 51-1-20D. REMOVED DOUBLER AND FABRICATED FILLER AND DOUBLER. CLEANED TREATEMay 1, 2004 · N830BX · Doug DC871FSDR IXXA0400068SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT OB WING LE OB SECTION CORRODED AT STA XFS 710.000. THIS REPAIR WAS ACCOMPLISHED IAW DWG V82-R02 AND N/R 0652. REMOVED FASTENERS IAW SRM 51-1-21 PG1. REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18. FOUND OUT OF LIMITS.May 1, 2004 · N830BX · Doug DC871FSDR IXXA0400067SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING OB LE LOWER SKIN CRACKED .5000 INCH. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 AND 51-1-20D PG1. REMOVED DAMAGED AREA IAW DWG V82-R01. PERFORMED NDT INSPECTION IAW NDT SPM PMay 1, 2004 · N830BX · Doug DC871F
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