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 CWQR200902Stiffener · misinstalledDURING A SCHEDULED INSP, FOUND THE LANDING ACTUATOR CHAFING STIFFENER P/N 6621211-25 LOCATED IN RT MAIN GEAR WELL. CONTACTED MFG FIELD ENGINEERS, DISCOVERED THE THE LT SIDE STIFFENER WAS INSTALLED ON THE RT SIDE FROM THE FACTORY. INSTALLED CORRECT STIFFENER ANMar 10, 2009 · N623QS · Cessna 560XLSDR CWQR200901Stiffener · misinstalledDURING A SCHEDULED INSPECTION, FOUND THE LANDING ACTUATOR CHAFING STIFFENER P/N 6621211-26 LOCATED IN LT MAIN GEAR WELL. CONTACTED MFG FIELD ENGINEERS, DISCOVERED THE THE RT SIDE STIFFENER WAS INSTALLED ON THE LT SIDE FROM THE FACTORY. INSTALLED CORRECT STIFFEMar 10, 2009 · N693QS · Cessna 560XLSDR MZZA2009031000031Skin · corrodedCORROSION AT RT WING CENTER WING FWD LOWER SKIN AT STA 540 WBL 52 UNDER DRAG BRACE. REPAIR CARRIED OUT IAW EC/RA 5730-02550.Mar 10, 2009 · N27246 · Boeing 737824SDR WRLA2009063AAccess Panel · corrodedDURING A6-CHECK IN ATL INSPECTION FOUND CORROSION ON WING CENTER SECTION SKIN AT FWD OUTBOARD CORNER OF LT MLG WHEEL WELL. REMOVED CORROSION PER SRM 57-20-00 FIG 21. DRILLED UP AND INSTALLED NEW ANGLE (ANB7392-1) PER SRM 57-20-00 FIG 21. LEAK CHECKED OK. DMar 9, 2009 · N138WA · Doug DC1030SDR IPXA09M55287Skin · crackedINSPECTION TYPE:4C LT WING FIXED L/E TELESCOPIC DUCT CUTOUT UPPER SURFACE AFT O/B CORNER IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW MD-11 SRM 57-10-00 FIG 43.Mar 9, 2009 · N276UP · Doug MD11FSDR IPXA09M55154Skin · crackedINSPECTION TYPE:4C FIXED LEADING EDGE RT ANTI-ICE DUCT CUTOUT CRACK AT TWO UPPER CORNER. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 42.Mar 9, 2009 · N276UP · Doug MD11FSDR FDEA200903090868Skin · delaminatedLT WING INT T/E FOUND SKIN PANEL UNBONDED LWR SIDE. REPAIRED PANEL IAW SRM 51-71-00, CHAP 16, VOL II.Mar 9, 2009 · N68053 · Doug MD1010FSDR DLM88090392Access Panel · corrodedACCESS PANEL 1303C CORRODED.Mar 6, 2009 · N971DL · Doug MD88SDR IPXA09855409Skin · corrodedINSPECTION TYPE:SV CORROSION FOUND INSIDE FUEL TANK RT WING LOWER AFT (REF, SEQ 752-W2-03) BETWEEN STA XRS 225-238 FWD OF REAR SPAR ON WING SKIN. REMOVED CORROSION IAW DC8 SRM 51-01-08 AND 57-02-00 FIG 007 SHT 1. INSTALLED REPAIR DOUBLER IAW REO - G12704REV Mar 5, 2009 · N752UP · Doug DC871FSDR MALA090034Skin · dentedSEVERAL DENTS NOTED RT WING TRAILING EDGE UPPER SKIN. REPAIRED.Mar 4, 2009 · N435XJ · Saab 340BSDR FDEA200903040843Skin · wornRT WING L/E FOUND NR 2EA DEEP WEAR ON EXT SKIN .050 INCH BY .25 INCH DEEP .60 INCH. REPAIRED AREA IAW SRM 57-10-00, FIG 39 AND 15, VOL I.Mar 4, 2009 · N68053 · Doug DC1010FSDR FDEA200903040842Skin · crackedRT WING EXT SKIN L/E FOUND CRACK ON UPPER EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.Mar 4, 2009 · N68053 · Doug DC1010FSDR A6WA200940099Skin · corrodedCORROSION ON UPPER PLANK ACCESS DOOR CUTOUT OF 640AT REO 601R-57-21-1076. (K)Mar 3, 2009 · N413AW · Cndair CL6002B19SDR A6WA200940098Skin · corrodedCORROSION ON UPPER PLANK ACCESS DOOR CUT OUT OF 640BT. REO 601R57-21-1076.Mar 3, 2009 · N413AW · Cndair CL6002B19SDR A6WA200940100Skin · corrodedCORROSION ON UPPER PLANK ACCESS DOOR CUTOUT OF 540AT REO 601R-57-21-1076. (K)Mar 3, 2009 · N413AW · Cndair CL6002B19SDR DLM88090362Access Panel · corrodedFLANGE CORRODED ON FUEL TANK ACCESS PANEL 1363C LT LWR WING. REPLACED PANEL ON ATS CARD 01721.Mar 3, 2009 · N971DL · Doug MD88SDR DLM88090361Access Panel · corrodedFLANGE CORRODED ON LEFT WING LWR FUEL TANK ACCESS PANEL 1379C. REPLACED PANEL ON ATS CARD 01720.Mar 3, 2009 · N971DL · Doug MD88SDR GLBA20090304ISkin · dentedDURING ROUTINE SHEDULED MAINTENANCE THE LT WING, OUTBOARD LEADING EDGE WAS FOUND DENTED AND REQUIRES REPLACEMENT. REPAIRED LT LEADING EDGE SECTION FROM WS 223-271. WORK PERFORMED PER FR-CO-01895 REV.2. STEPS 1 -15, 16 LEAK CHECK OF AFFECTED AREAS PERFORMEMar 3, 2009 · N165YV · Beech 1900DSDR FDEA200903030834Skin · delaminatedRIGHT WING UPPER SKIN EXTERIOR SURFACE T/E AREA HAS COMPOSITE LAYERS PEELING BETWEEN RIB 1 AND RIB 2. REPAIRED THE RIGHT WING UPPER SKIN BY REMOVING THE DAMAGE, POTTING THE PANEL AND THE HONEY COMB CORE. APPLYING FIBERGLASS OVERLAYS AND CURING IAW A300-600 SMar 3, 2009 · N740FD · Airbus A300B4622RSDR DLM88090394Access Panel · corrodedACCESS PANEL CORRODED ON FLANGE.Mar 2, 2009 · N971DL · Doug MD88SDR DLM88090393Access Panel · corrodedACCESS PANEL FLANGE CORRODED.Mar 2, 2009 · N971DL · Doug MD88SDR QXEA2009030300158Panel · corrodedPDX -C1- CENTER WING AFT PANELS 262AT, 262HT, 262FT MATING SURFACE ON FWD SIDE HAS FRETTING CORROSION. HFEC INSPECTED BLENDS FOR CRACKS IAW Q400 NDT6M PART 6, 51-00-000-250-801 AND STEP 3 GENERAL NOTES OF RD 8/4-53-521. NO CRACKS NOTED. PERFORMED REPAIR ON Mar 2, 2009 · N423QX · Bombdr DHC8402SDR FDEA200903020800Panel · wornTHE OTBD CORNER UPPER SURFACE IS WORN AT LEFT WING 2ND FROM INBD TRAILING EDGE DROP DOWN PANEL NR 572 CB. REPAIRED OTBD FWD UPPER CORNER OF THE PANEL BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REMar 2, 2009 · N740FD · Airbus A300B4622RSDR FDEA200903020799Panel · delaminatedFOIL IS DISBONDED ON THE UPPER SURFACE OF THE 2ND PANEL FROM INBD, LEFT WING DROP DOWN TRAILING EDGE PANEL NR 572 CB. REPAIRED FLAP DIFFUSER PANEL INNER SKIN BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACMar 2, 2009 · N740FD · Airbus A300B4622RSDR FDEA200903020798Panel · delaminatedLEFT WING TRAILING EDGE PANEL NR 572 GB HAS THE TOP LAMINATE PEELING. REPAIRED PANEL NR 572 GB BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW DWG SR 27-53-011 AND EA 6-5720-127921.Mar 2, 2009 · N740FD · Airbus A300B4622RSDR FDEA200903020797Panel · delaminatedLEFT WING TRAILING PANEL NR 572 LB HAS THE TOP SURFACE LAMINATE PEELED. REPAIRED PANEL NR 572 LB BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW FEDEX DWG SR 27-53-011 AND FEDEX EA 6-5Mar 2, 2009 · N740FD · Airbus A300B4622RSDR IPXA09856076Skin · misrepairedINSPECTION TYPE:SV SS 718-W3-09, LT WING LEADING EDGE LOWER SURFACE REPAIR DOUBLER AT XFS 164 DOES NOT PASS REPAIR QUESTIONAIRE DC8-5100-304018 APPENDIX-H. (REPAIR DO DOUBLER IS NOT ALUMINUM). REPAIRED PER TIMCO REO-G12767 REV B, AND UPS EO DC8-5730-33603-A.Mar 1, 2009 · N718UP · Doug DC871FSDR QXEA2009030300152Panel · corrodedPDX - C1 - CENTER WING FWD PANELS 261CT, 261LT, 261HT MATING SURFACE ON AFT SIDE HAS FRETTING CORROSION. HFEC INSPECTION BLENDED AREAS FOR CRACKS IAW Q400 NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. THIS COMPLETES STEP 3, GENERAL NOTES RD 8/4-53-521. PMar 1, 2009 · N423QX · Bombdr DHC8402SDR MALA090033Skin · dentedSEVERAL DENTS NOTED LT WING TRAILING EDGE UPPER SKIN. REPAIRED.Feb 28, 2009 · N435XJ · Saab 340BSDR FDEA200902280769Skin · crackedRT WING L/E FOUND CRACK ON LOWER EXT SKIN. REPAIRED AREA IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.Feb 28, 2009 · N68053 · Doug DC1010FSDR UIEA200900018Panel · delaminatedLT WING UPPER SURFACE L/E FIXED PANEL AT ILES 664.97 HAS AN AREA OF 6.0 BY 18.0 INCHES OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 18 SHEET 2 AND 5. PREPREG 250* F CURE PER SRM 51-40-12. REFERENCE ATLAS AIR EO 4757A477.Feb 27, 2009 · N540MC · Boeing 747243BSDR IPXA09856150Skin · misrepairedINSPECTION TYPE:SV SS 718-W4-14, RT WING L/E LOWER SURFACE XFS 347, EXT REPAIR DOES NOT CORRELATE TO A SRM OR APP "H" (STOP DRILL NOT .25 INCH). REPAIRED PER TIMCO REO-G12774 REV D, AND UPS EO DC8-5730-33659A.Feb 24, 2009 · N718UP · Doug DC871FSDR FDEA200902240678Skin · misrepairedEXISTING REPAIR, LT WING, INBD FLAP INBD SEGMENT, INBD UPPER LEADING EDGE SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT, INBD UPPER LEADING EDGE SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW ANY SRM REPAIR SCHEME. LT WINFeb 24, 2009 · N582FE · Doug MD11FSDR IPXA09M54884Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 294-W3-010 IS NOT ON MRCSSR AND NOT PER SRM CUTOUT DOES NOT MEET MINIMUM REPAIR. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 7 VOL 1.Feb 24, 2009 · N294UP · Doug MD11FSDR FDEA200902230637Skin · corrodedRT WING, UPPER SKIN CORROSION AT APPROX XORS= 260, STRINGER 31. REPAIRED AS PER SRM 51-00-01 FIG 6 VOL. I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 23, 2009 · N582FE · Doug MD11FSDR KCSA091019Skin · corrodedCENTER WING UPPER SKIN CORRODED AT BS 1140 RBL 37.Feb 23, 2009 · N746CK · Boeing 747246FSDR IPXA09M54864Skin · damagedINSPECTION TYPE:1C REPAIR SURVEY SEQ 294-W4-04 RT WING FIXED L/E BETWEEN XIS 190-197 HAS AN EXISTING REPAIR WITH SINGLE ROW OF FASTENERS AROUND THE FLUSH REPAIR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 VOL 1 FIGFeb 20, 2009 · N294UP · Doug MD11FSDR IPXA09M54841Repair · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ 294-W3-002 LT WING FIXED L/E UPPER SKIN BETWEEN XOS 452.1-467.1 PREVIOUS REPAIR IS GOUGED AT SLAT TRACK CUTOUT. REMOVED REPAIR, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 43.Feb 19, 2009 · N294UP · Doug MD11FSDR FDEA200902190579Skin · crackedLT WING OTBD FLAP OTBD HINGE FOUND CRACK ON SKIN. REMOVED PART.Feb 19, 2009 · N68053 · Doug DC1010FSDR FDEA200902190578Skin · crackedLT WING OTBD FLAP INBD HINGE (ONBOARD) FOUND CRACK ON SKIN (REMOVED PART). REPAIRED AREA IAW SRM 57-00-01, FIG 4, SHT 2, VOL I.Feb 19, 2009 · N68053 · Doug DC1010FSDR FDEA200902190576Skin · corrodedMAIN DECK CARGO COMPARTMENT, CENTER WING UPPER SKIN PANEL STA 1229, X = - 50 TO X = - 80 FOUND WITH CORROSION AROUND FASTENER HEAD. REPAIRED AS PER E.A. NO. 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11FSDR FDEA200902190575Skin · corrodedMAIN DECK CARGO COMPARTMENT, CENTER WING UPPER SKIN PANEL STA 1229 X = -80 TO X = -100 FOUND WITH CORROSION AROUND FASTENER HEAD. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 19, 2009 · N585FE · Doug MD11FSDR IPXA09M54902Doubler · crackedINSPECTION TYPE:1C RT WING FIXED L/E BEADED DOUBLER XFW 669 HAS 5 INCH CRACK. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27.Feb 17, 2009 · N294UP · Doug MD11FSDR FDEA200902170571Skin · cracked17 FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT- OUT BETWEEN XORS 690 AND XORS 700. COMPLIED WITH EA 1-5710-127455, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.Feb 17, 2009 · N585FE · Doug MD11FSDR FDEA200902170570Skin · cracked09 FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT- OUT BETWEEN XORS 690 TO XORS 700. REAMED AND REPAIR CARRIED OUT AS PER EA 1-5710-127454, REPAIR CLASSIFIED AS MINOR AFeb 17, 2009 · N585FE · Doug MD11FSDR UALA2009021700508Panel · crackedRT INBOARD L/E PANEL CRACKED APPROX 30 INCHES LONG. COMPLETED MFG OF NUT PLATE STRIPS. INSTALLED PANELS. SEALED UP PANEL. ACCOMPLISHED ON DOCK WU S5927I AT SMB.Feb 17, 2009 · N180UA · Boeing 747422SDR UPS09M54803Doubler · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQ W4-002, EXISTING REPAIR DOUBLER IS GOUGED AT STA XIS 239-255 ON RT WING FIXED L/E AND NOT ON MRCSSR. REMOVED EXISTING REPAIR AT STA XIS 239-255 RT WING FIXED L/E, FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11 VOL 1 Feb 16, 2009 · N274UP · Doug MD11FSDR S9BA2009006Skin · crackedAFTER REMOVING OTBD PLANK DOUBLERS AT WS 118 TO 138 OF THE RT WING, FOUND TWO CRACKS IN THE UPPER WING SKIN. ONE .7500 CRACK AT WS 123.5 AND 47 INCHES AFT OF NOSE SPAR AND ONE .5 INCH CRACK AT WS 123.5 AND 43 INCHES AFT OF THE NOSE SPAR. ACCOMPLISHED REPAIRS Feb 13, 2009 · N888PV · Dhav DHC6300SDR UPS09M54801Doubler · chafedINSPECTION TYPE:4C DEEP CHAFE DAMAGE ON REPAIR DOUBLER AT I/B SIDE OF OPENING FOR RT WING O/B SLAT DEICE TELESCOPE TUBE, NEAR STA XOS 465, REPAIR SEQ 274-W4-05. REMOVED EXISTING REPAIR AT RT WING O/B SLAT DEICE TELESCOPIC DOOR AT XOS 465, FABRICATED AND INSTAFeb 12, 2009 · N274UP · Doug MD11FSDR GLBA20090220ASkin · distortedMAJOR REPAIR - LEFT HAND INBOARD WING UPPER AFT WING SKIN OUT OF CONTOUR AT STATIONS F.S. 301 W.S. 70 .022" F.S. 311 W.S. 70 .032", F.S. 319 W.S. 70 .035" F.S. 329 W.S. 70 .035". MAINTENANCE REPLACED LT UPPER INBOARD SKIN IAW E.O.-09-165-01.Feb 12, 2009 · N165YV · Beech 1900D
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