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 LR7A08126Skin · damagedDURING CLIMB, ACFT SUSTAINED A BIRD STRIKE TO LT WING L/E AT FS480, WL284, OWS421. REPAIRS IN WORK. WILL UP DATE SDR AS FURTHER INFORMATION BECOMES AVALIABLE. LOG PAGE 26549.Dec 18, 2008 · N401LC · Lkheed 382GSDR I5HA0824013Wing · dentedDURING THE LANDING FLARE, A BIRD STRUCK THE OTBD L/E OF THE LT WING. THE CREW LANDED THE ACFT WITHOUT FURTHER INCIDENT. THE LEADING EDGE WAS REMOVED AND REPLACED AND THE ACFT RETURNED TO SERVICE.Dec 18, 2008 · N150PA · Cvac 240*SDR FDEA200812165182Doubler · chafedRIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT OUT REPAIR DOUBLER FOUND CHAFED. DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME II AND INSTALLED WITH A NEW REPAIR DOUBLER AS PER EA 1-5740-122639 PART 1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-Dec 16, 2008 · N575FE · Doug MD11FSDR DU4R2008275Skin · corrodedDURING SCHEDULED INSPECTION, FOUND LT WING HAD CORROSION IN UPPER SKIN AT ALL VORTEX GENERATORSDec 16, 2008 · N868AN · Boeing 75723APFSDR FDEA200812155144Skin · crackedLT WING SLATS, FOUND CRACK AND NR 10 FASTENERS U/S ON CORNER SKIN INTERNAL SIDE SLAT NR 2. REPAIRED AREA IAW SRM 57-10-00 FIG 31, VOL I.Dec 15, 2008 · N317FE · Doug DC1030FSDR COMA2008121750032Skin · damagedLT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 540 AB, AT WS 67.75 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.Dec 12, 2008 · N785CA · Cndair CL6002B19SDR COMA2008121750031Skin · damagedLT WING LOWER DRAIN ATTACHMENT HOLE JUST AFT OF PANEL 510 AB, BETWEEN WS 0.00 AND WS 22.50, AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.Dec 12, 2008 · N785CA · Cndair CL6002B19SDR COMA2008121750030Skin · damagedRT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 640 DB AT WS 85.50 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.Dec 12, 2008 · N785CA · Cndair CL6002B19SDR COMA2008121750029Skin · damagedLT WING LOWER DRAIN ATTACHMENT HOLES JUST FWD OF PANEL 540AB AT WS.0.00, FWD AND AFT SCREW HOLES ARE DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.Dec 12, 2008 · N785CA · Cndair CL6002B19SDR HAEA20000206Skin · damagedLT TIP TANK DAMAGED AND DENTED ON AFT LOWER SURFACE. TIP TANK REMOVED AND AFT CONE REMOVED TO EVALUATE DAMAGE. DISCOVERED AFT CENTER BULKHEAD DEFORMED, INNER ATTACH DOUBLER DEFORMED AND LOWER SEAM RIVETS SHEARED. TIP TANK REQUIRES REPAIR FOR RETURN TO SERVIDec 12, 2008 · N330TW · Lear 24ESDR SWIA200820639Skin · dentedFLT 1010 - TWO DENTS ON RIGHT LEADING EDGE AT WS 201.0 EXCEED LIMITS OF SRM. REPLACED LEADING EDGE SKIN PER SRM.Dec 11, 2008 · N405SW · Cndair CL6002B19SDR SWAA087058Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING L/E SKIN CRACKED AT I/B END. REPAIRED SKIN PER SRM.Dec 11, 2008 · N707SA · Boeing 7377H4SDR SWAA087022Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING SKIN CRACKED AT FIXED L/E ABOVE SPRING DOOR. REPAIRED SKIN PER SRM.Dec 11, 2008 · N333SW · Boeing 7373H4SDR DHLA 2009770AT527Skin Panel · crackedRIGHT WING FRONT SPAR SECTION LEADING EDGE SKIN CRACKED AT WS 491. REPAIRED RIGHT WING FIXED LEADING EDGE SKIN SECTION FROM LE STA 151.40 TO LE STA 195.65 IAW COOPESA EO COO-2-57-461-08 DTD 12/19/08.Dec 9, 2008 · N770AT · Boeing 7272B7SDR GUUA94157120908ASkin · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 139 THROUGH 158. REMOVED DAMAGED SKIN AND FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Dec 9, 2008 · N17541 · Beech 1900DSDR FDEA200812095114Skin · bulgedRIGHT WING LOWER SKIN, LOWER SURFACE OTBD OF RIB 11 (OTBD OF THE FLAP TRACK) 19 INCHES FWD OF THE REAR SPAR, THE SKIN IS BULGING, FWD SIDE OF THE FASTENERS. REMOVED CORROSION. FLAP PEENED AREA. ALODINED, PRIMED AND PAINTED IAW EA 6-5730-123533. REMOVED ANDDec 9, 2008 · N716FD · Airbus A300B4622RSDR DU4R2008269Skin · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AFT SPAR UPPER CHANNEL, SKIN FROM FUSELAGE TO WING TIP.Dec 7, 2008 · N868AN · Boeing 75723APFSDR DU4R2008266Skin · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AT NUMEROUS FASTENERS IN UPPER SKIN IN PREVIOUSLY WORKED SKIN AND UNWORKED SKIN.Dec 7, 2008 · N868AN · Boeing 75723APFSDR ASOA200801662Skin · damagedLT WING LWR PLANK ACCESS HOLE 540CB HAS EDDY CURRENT INDICATION NOTED 60 PERCENT FULL SCREEN HEIGHT APPROX 0.1 INCH LONG ON LANDING OF I/B SECTION OF RADIUS, NON-CRITICAL AREA APPROX 1 INCH AFT OF CENTER LINE. FAILS NDT INSPECTION. REPAIRED LT WING PLANK ACCDec 5, 2008 · N979EV · Cndair CL6002B19SDR FDEA200812045075Skin · crackedRT WING LOWER LEADING EDGE CRACKED AT CUTOUT FOR PANEL 613AB, CRACK EXTENDS AT BOTH ENDS OF FASTENER HOLE. DRILLED CRACK STOP HOLE IAW SRM 53-15-63 PG 202 STEP 2. FABRICATED DOUBLERS IAW SRM 53-15-63 PG 209-210. ALODINED, PRIMED, AND PAINTED IAW AMM 51-23-1Dec 4, 2008 · N716FD · Airbus A300B4622SDR FDEA200812035055Skin · cracked07 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. REAMED AND REPAIR CARRIED OUT AS PER EA NR 1-5710-122655. REPAIR CDec 3, 2008 · N575FE · Doug MD11FSDR FDEA200812035054Skin · cracked08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. EACH CRACKED FASTENER HOLES REAMED AND REPAIR CARRIED OUT AS PER EA Dec 3, 2008 · N575FE · Doug MD11FSDR FDEA200812025048Panel · corrodedLT WING T/E PANEL NR 575DB HAS FRETTING CORROSION, WORN AREAS, AROUND FASTENER MATTING SURFACE AFT OF RIB 7A. REPAIRED LT WING T/E PANEL 575DB BY BONDING A PICTURE FRAME DOUBLER TO PANEL IAW EA 6-5750-123683 AND SRM 51-77-10. REMOVED AND REATTACHED PANEL TO Dec 2, 2008 · N716FD · Airbus A300B4622SDR COMA2008120150018Panel · corrodedLEFT WING PLANK FUEL PANEL CUTOUT AT 540BB HAS FRETTING CORROSION ON INBOARD SIDE. BLENDED OUT AND REMOVED FRETTING DAMAGE ON FUEL PANEL CUTOUT 540BB INBD SIDE PER REO 601R57-21-030.Nov 30, 2008 · N442CA · Cndair CL6002B19SDR COMA2008120150017Skin · damagedRIGHT WING LOWER PLANK BOOST PUMP NR 8 SCREW HOLE IS DAMAGED. REMOVED DAMAGE AND INSTALLED A SERVICEABLE FREEZE PLUG BUSHING IAW REO 601R-57-21-169 REV (D).Nov 30, 2008 · N442CA · Cndair CL6002B19SDR FDEA200811284994Skin · chafedRIGHT WING LEADING EDGE SURFACE FOUND CHAFED AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA. RT WING LEADING EDGE CHAFED SURFACE AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA REPAIR CARRIED OUT AS PER EA NO 1-5740-122639 PART 1. REPANov 28, 2008 · N575FE · Doug MD11FSDR FDEA200811285033Skin · crackedRT INBD FLAP INBD UPPER SKIN NR A57960007000 IS CRACKED. FABRICATED NEW SKIN IAW EA 6-5750-123529 AND DWG A57960007. ALODINED AND PRIMED IAW SRM 51-21-10. INSTALLATION OF SKIN TO BE ACCOMPLISHED ON J/C NR 6-5750-7-5003 PT 1.Nov 28, 2008 · N716FD · Airbus A300B4622SDR UIEA200800344Panel · departedON SHORT FINAL APPROACH, THE AIRCRAFT WAS ADVISED BY DXB ATC THAT THERE WAS A HOLE IN THE LEFT WING. DXB SAFETY RECOVERED AND BOUGHT PANEL THAT LIBERATED ITSELF FROM THE AIRCRAFT TO THE DXB MAINTENANCE OFFICE. REPLACED PANEL AND PERFORMED RIB REPAIR PER SB 7Nov 26, 2008 · N497MC · Boeing 74747UFSDR FDEA200811255074Skin · crackedRT WING LWR SKIN CRACKED APPROX 3/16 INCH BEYOND PREVIOUS STOP PLUG REPAIR. CRACK IS PROGRESSING AFT TOWARD FASTENER HOLE NR 19 AND TRANSITION RADIUS BETWEEN RIBS 8 AND 9. COMPLIED WITH EA 6-5730-123509 PART 1, WINGS CRACK IN RT BOTTOM SKIN AT FRONT SPAR, 63Nov 25, 2008 · N722FD · Airbus A300B4622RSDR ASOA200801571Skin · corrodedINDICATION NOTED AT LOWER WING PLANK ACCESS HOLE 640CB WHILE PERFORMING ASA TASK NR 000-57-900-610 AFT SIDE OF HOLE. INDICATION APPEARS TO BE CORROSION APPROX .040 IN DEPTH. INDICATION IS MAPED IN AIRCRAFT. REMOVED DAMAGE AT RT LOWER WING PLANK ACCESS HOLE Nov 25, 2008 · N867AS · Cndair CL6002B19SDR ASOA200801562Skin · corrodedINDICATION NOTED AT LOWER WING PLANK ACCESS HOLE 640CB WHILE PERFORMING ASA TASK NR 000-57-600-610. INDICATION APPEARS TO BE CORROSION APPROX .040 DEEP, INDICATION IS MAPPED ON AIRCRAFT. REPAIRED LOWER WING PLANK ACCESS HOLE 640CB IAW REO 601R-57-21-1033. ANov 25, 2008 · N867AS · Cndair CL6002B19SDR 08FDEA04964Skin Panel · crackedWHILE ACCOMPLISHING "OK TO WORK" STEP ON SNRM (N00791)) FOUND WING L/E SKIN CRACKED (LT WING) AT FSS 122, LWR SURFACE OF SKIN. REMOVED AND REINSTALLED ANTI-ICE DUCT (LT L/E WING ROOT) REF MM 36-00-001-2, LEAK CHECK GOOD. REPAIRED CRACK REF SRM 57-30-4 FIG 8.Nov 24, 2008 · N287FE · Boeing 7272D4SDR UIEA200800343Panel · crackedRT WING UPPER L/E PANEL HAS A 19 INCH COMPOSITE CRACK AT ILES 657.22, 5.0 INCHES FROM PANEL FRONT EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 18, SHEETS 2 AND 5 AND SRM 51-40-12. REF ATLAS AIR EO 4757A467.Nov 21, 2008 · N522MC · Boeing 7472D7BSDR UIEA200800342Panel · delaminatedRT WING PREVIOUS REPAIR ON UPPER WING SURFACE L/E PANEL AN AREA OF 6.0 BY 38.0 INCHES IS DELAMINATED AT ILES 522.06 AND 7.5 INCHES FROM PANEL FRONT EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 2, 5 AND SRM 51-40-12. REF. ATLNov 21, 2008 · N522MC · Boeing 7472D7BSDR UPS08854186Skin · crackedINSPECTION TYPE:SV LT WING O/B LEADING EDGE I/B SECTION LOWER EXTERIOR SKIN CRACKED AT DRAIN HOLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5730-31529-A AND SAA EA 008-5720-01-A1571.Nov 20, 2008 · N803UP · Doug DC873FSDR 08FDEA04938Skin · dentedDURING INSPECTION RT WING LWR SURFACE FOUND SCRATCH 22 INCHES LONG AND DEEP DENT 3 INCHES BY 3 INCHES DEEP .161 INCH ON LWR SKIN OF OUTBD AILERON. DAMAGE IS "NOT/FLIGHT AIRCRAFT STRIKE DAMAGE". REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 2 SHT 2 NOTE 8.Nov 20, 2008 · N317FE · Doug DC1030FSDR UPS08854074Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 729-W4-10 DOES NOT MEET SRM CRITERIA. PREVIOUSLY REPAIRED, FOUND NO DEFECTS 51-40-02.Nov 18, 2008 · N700UP · Doug DC871FSDR 08FDEA04918Skin · damagedPREVIOUSLY INSTALLED REPAIR, WS 823, WBL 740, TANK INTERNAL, RT WING, LOWER SURFACE, IDENTIFIED AS A TIME-LIMITED REPAIR. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5100, PART 1. COMPLIED WITH ATTACHMENT "B" OF EO F-5100-7-5001, PART 1. REPLACED RT WING, LNov 18, 2008 · N918FD · Boeing 75723ASDR KCSA081589Skin · corrodedLT WING UPPER SURFACE ILES-472 AT L/E RIB HAS CORROSION.Nov 18, 2008 · N708CK · Boeing 747212BSDR C8GA20080092Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT WING L/E WS 530 AT HOOK CUTOUT AFT REPAIR HAS CRACK. REMOVED PREVIOUS REPAIR, FABRICATED NEW PLATE FROM AISI 301 1/2 HARD .020 INCH DIM 8 INCH BY 6 INCH. INSTALLED REPAIR IAW SRM 57-30Nov 17, 2008 · N715AA · Boeing 727223SDR HALA2008111700877Panel · debondedLT WING T/E PANEL AT WS314.3 TOP SURFACE RAISED AND RIVET PULLED. SUSPECTED CORROSION UNDER PANEL. FOUND TO BE DISBOND OF COMPOSITE PANEL. REPAIRED PANEL IAW SRM 57-51-01 AND 51-70-07, PARA 5K REV 77.Nov 17, 2008 · N582HA · Boeing 76733ASDR HALA2008111700864Skin · damagedFRETTING DAMAGE ON RT WING AT RBBL 97.42 LOWER SPLICE PLATE. FRETTING DAMAGE BLENDED IAW 767 SRM 57-20-90/1AO1, THEN ROTO-PEEING 767 CM 20-10-03. SURFACE ALODINED AND PRIMED, SEALENT RE-APPLIED TO EDGES.Nov 17, 2008 · N582HA · Boeing 76733ASDR UPS08M53946Skin · crackedINSPECTION TYPE:1C RT WING ON TELESCOPIC ANTI-ICE DUCT AT SLAT NR 3 HAS CRACK ON DOOR CUTOUT UPPER LEFT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD11 VOL 1 SRM 57-10-00 FIG 43.Nov 17, 2008 · N254UP · Doug MD11FSDR UPS08M53932Skin Panel · damagedINSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-W3-006 LT WING INBOARD FIXED L/E PNL UPPER SURFACE STA XIS 244 HAS LOOSE FASTENERS AND WRINKLING SKIN EO MD11-5110-30530 APPENDIX C AND NO SRM REF APPENDIX E. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED DOUNov 17, 2008 · N254UP · Doug MD11FSDR COMA0860462Skin · corrodedLT WING FUEL ACCESS PANEL CUTOUT AT 510AB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 510AB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.Nov 13, 2008 · N784CA · Cndair CL6002B19SDR COMA0860463Skin · corrodedRT WING FUEL ACCESS PANEL CUTOUT AT 640BB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE NON CRITICAL AREA AT FUEL ACCESS PANEL 640BB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.Nov 13, 2008 · N784CA · Cndair CL6002B19SDR COMA0860465Skin · damagedFUEL DRAIN FWD OF LT WING FUEL PANEL 510AB CUTOUT HAS DAMAGE ON FWD SCREW ATTACH HOLE. REAMED AND INSTALLED A SERVICEABLE FREEZE PLUG BUSHING FOR FUEL DRAIN FWD OF LT WING FUEL PANEL 510AB CUTOUT FWD SCREW ATTACH HOLE IAW COMAIR EA # 10-5721-02413.Nov 13, 2008 · N784CA · Cndair CL6002B19SDR COMA0860464Skin · damagedFUEL DRAIN AFT OF LT WING FUEL PANEL 510AB CUTOUT HAS DAMAGE ON AFT SCREW ATTACH HOLE. REAMED AND INSTALLED A SERVICEABLE FREEZE PLUG BUSHING FOR FUEL DRAIN AFT OF LT WING FUEL PANEL 510AB CUTOUT AFT SCREW ATTACH HOLE IAW COMAIR EA # 10-5721-02413.Nov 13, 2008 · N784CA · Cndair CL6002B19SDR KCSA081575Skin · corrodedRT WING LOWER SKIN CORRODED AT BOOST PUMP CUTOUT AT WS 682.Nov 13, 2008 · N708CK · Boeing 747212BSDR UPS08854211Skin · damagedINSPECTION TYPE:SV LT WING CENTER L/E LWR SKIN HAS 2 FLUSH REPAIRS AT STA XFS 422. REPAIRED IAW UPS EO DC8-5720-31609-A.Nov 11, 2008 · N729UP · Doug DC871F
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