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"

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SDR IPXA09855637Skin · crackedINSPECTION TYPE:SV SSN 852-W4-13 REPAIR DOUBLER CRACKED RT LEAD EDGE LWR SKIN ABOVE NR 4 PYLON XFS 530 35 INCH FWD OF WING FWD SPAR. REPAIR ACCOMPLISHED IAW DC8 SRM 57-02-01A FIG 2 SHT 1.Apr 19, 2009 · N852UP · Doug DC873FSDR FDEA200904181359Skin · crackedCENTER WING JOINT AT FRAME 40; LEFT SIDE AT THE UPPER SKIN LEVEL TENSION BOLT JUNCTION; ALL THREE FASTENER HOLES HAVE CRACK INDICATIONS. REMOVED DAMAGE BY REAMING, TREATED BARE METAL AND INSTALLED OVERSIZED BOLTS IAW EA 6-5710-127939 " WINGS, CENTER WING JOINApr 18, 2009 · N726FD · Airbus A300B4622RSDR IPXA09855655Doubler · damagedINSPECTION TYPE:SV 852-W4-10 REPAIR DOUBLER CHAFED/GOUGED AND HAS FASTENERS WITH SHORT E D RT WING LEADING EDGE LOWER SKIN XFS 257, 47 INCHES FWD OF WING FRONT SPAR (ABOVE NR 3 PYLON). REPAIRED PER DC8 SRM 57-2-1A FIG 2.Apr 16, 2009 · N852UP · Doug DC873FSDR IPXA09855636Skin · damagedINSPECTION TYPE:SV SSN 852-W4-10 REPAIR DOUBLER CHAFED/GOUGED AND HAS FASTENERS WITH SHORT ED RT WING LEAD, EDGE LWR SKIN XFS 257 47 INCH, FWD OF WING FWD SPAR ABOVE NR 3 PYLON. REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1A FIG 2.Apr 16, 2009 · N852UP · Doug DC873FSDR FDEA200904161315Skin · corrodedSEVERAL CORROSION SPOTS AND CORROSION AROUND FASTENERS ON THE RT WING UPPER SURFACE BETWEEN RIB 1 AND 14. REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/BAE/1009447/2009 ISSUE "A".Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161312Skin · corrodedCORROSION AND CHAFING, BOTTOM SKIN PANEL 1 AND 2, PYLON AND FLAP TRACK 2 REINFORCEMENT PLATE. REPAIR PERFORMED IAW EA 6-5720-129136, TD/J1/S1/09343/2009 ISSUE "A", TD/J1/S1/09620/2009 ISSUE "A" AND RAS/BAE/1009343/2009 ISSUE "A".Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161309Plate · chafedCHAFING MARKS IN THE LOWER WING PYLON REINFORCING PLATE. REPAIR PERFORMED IAW EA 6-5710-129142, TD/J1/S1/09291/2009 ISSUE "C" AND RAS /BAE/1009291/2009 ISSUE "A".Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161321Skin · corrodedSEVERAL CORROSION SPOTS AROUND SOME FASTENERS AT TOP SKIN JOINT EXTERNAL SURFACE IN THE AREA OF RIB 9 FRONT AND REAR SPAR REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161320Skin · corrodedSEVERAL CORROSION SPOTS RT WING TOP SKIN PANEL SURFACE FRONT SPAR ATTACHMENT BETWEEN RIB 1 AND 14 AND REAR SPAR ATTACHMENT BETWEEN RIB 1 AND 9 REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161319Skin · corrodedSEVERAL CORROSION SPOTS AND CORROSION AROUND FASTENER RT WING TOP SKIN PANEL UPPER SURFACE BETWEEN RIB 14 AND 29 REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161318Skin · corrodedCORROSION SPOT BETWEEN RIB 14 AND 15 / BETWEEN FRONT SPAR AND STRINGER 9 AT RT WING TOP SKIN, ARROUND FASTENER EXTERNAL SURFACE REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161316Skin · corrodedCORROSION SPOTS AROUND FASTENERS ON THE RT WING TOP SKIN RIB 8 REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/1009447/2009 ISSUE "A"Apr 16, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904161314Skin · crackedRIGHT WING LEADING EDGE NR 3 SLAT MOST OUTBOARD TRACK CUT-OUT INBOARD CORNER SKIN FOUND CRACKED. AREA TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.Apr 16, 2009 · N614FE · Doug MD11FSDR COMA2009041650118Skin · damagedRIGHT FUEL BOOST PUMP CONTAINER DRAIN SCREW HOLES IN WING PLANK ARE DAMAGED. REMOVED DAMAGE, REAMED AND INSTALLED A SERVICEABLE FREEZE PLUGS AT RT FUEL BOOST PUMP CONTAINER DRAIN FWD AND AFT SCREW HOLES PER EA 10-5721-02569.Apr 15, 2009 · N915CA · Cndair CL6002B19SDR COMA2009041650117Skin · damagedLEFT FUEL BOOST PUMP CONTAINER DRAIN, AFT SCREW HOLE IN WING PLANK IS DAMAGED. REMOVED DAMAGE, REAMED AND INSTALLED A SERVICEABLE FREEZE PLUG AT LT FUEL BOOST PUMP CONTAINER DRAIN, AFT SCREW HOLE PER EA 10-5721-02569.Apr 15, 2009 · N915CA · Cndair CL6002B19SDR DHLA2009801008Skin · corrodedNR 4 STUB WING UPPER EXTERNAL SKIN CORRODED, STA.XFS 530.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3,09191 DATED 04-30-09, EVA DB57-00258 REV IR DATED 04-22-09, DWG ED9935 DATED 04-16-09. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-21, SRM 51-1-700. REMOApr 13, 2009 · N801DH · Doug DC873FSDR COMA2009041550116Skin · crackedRT WING PLANK CRACKED ON BOTTOM SIDE JUST O/B OF JACK PAD. DAMAGED AREA TRIMMED OUT TO REMOVE CRACK AND REPAIR DOUBLERS INSTALLED PER REO 601R-57-21-130.Apr 13, 2009 · N958CA · Cndair CL6002B19SDR FDEA200904131271Access Panel · cracked01 FASTENER HOLE FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. FASTENER HOLE FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEApr 13, 2009 · N605FE · Doug MD11FSDR FDEA200904131270Access Panel · cracked04 FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION, AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. FASTENER HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENTApr 13, 2009 · N605FE · Doug MD11FSDR DHLA2009801010Skin · damagedRT WING CTR L/E REPAIR DOUBLER HOLES ELONGATED, STA X0LDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09175 DATED 04-28-09, EVA DE53-00257 REV IR DATED 04-21-09, DWG ED 4934 DATED 04-15-09. REMOVED DAMAGED REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-2Apr 11, 2009 · N801DH · Doug DC873FSDR IPXA09M55669Skin Panel · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ W3-03, LT WING FIXED LE/PYLON INTERSECTION LOWER SKIN HAS AN EXISTING EXTERNAL PLATING REPAIR THAT CANNOT BE CORRELATED TO THE SRM AND IS NOT ON THE MRCSSR. REPAIRED LT WING L/E LOWER SURFACE AT NR 1 PYLON REF EO MD11-5730Apr 10, 2009 · N291UP · Doug MD11FSDR IPXA09M55668Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ W4-06, RT WING FIXED L/E/PYLON INTERSECTION LOWER SKIN, HAS AN EXTERNAL PLATING REPAIR THAT CANNOT BE CORRELATED TO THE SRM AND IS NOT ON THE MRCSSR. REPAIRED RT WING L/E LOWER SURFACE AT NR 3 PYLON REF EO MD11-5730-33256-Apr 10, 2009 · N291UP · Doug MD11FSDR HALA2009040900150Access Panel · corrodedCORROSION ON FUEL TANK PANEL 541WB, ON CUT-OUT MATING SURFACE. PANEL REPLACED, CORROSION OUTSIDE SRM 57-20-01/201 REV 79 LIMITS.Apr 9, 2009 · N585HA · Boeing 7673G5SDR UALA2009041001043Panel · damagedRT WING LOWER WING FIXED TRAILING EDGE PANEL 651VB HAS A 1.5 INCH CRACK RUNNING FORE TO AFT. CRACK IS LOCATED 5.5 INCHES FROM INNER EDGE OF PANEL AND 0.75 INCHES OUTBOARD OF NEAREST FASTENER. REMOVED TRAILING EDGE RT WING PANEL. ROUTED PANEL TO SHOP 273. PApr 9, 2009 · N641UA · Boeing 767322SDR ASAA0995042Panel · damagedPANEL 667ET HAS AN ELONGATED HOLE. REPAIRED HOLE PER EA 900-57EA-01164 / ER 09-2331 REV A.Apr 9, 2009 · N306AS · Boeing 737990SDR FDEA200904091231Skin · wornFOUND ELONGATED HOLES ON LT PYLON/WING SUPPORT BRACKET AND BOTTOM SKIN RIB 8. REPAIR PERFORMED IAW DRAWING R571-50532 AND RAS/BAE/1009499/2009 ISS A, APPROVED BY EA 6-2900-129110.Apr 9, 2009 · N750FD · Airbus A300B4622RSDR FDEA200904091230Skin · wornFOUND ELONGATED HOLES ON RT PYLON/WING SUPPORT BRACKET AND BOTTOM SKIN RIB 8. REPAIR PERFORMED IAW DRAWING R571-50532 AND RAS/BAE/1009499/2009 ISS A, APPROVED BY EA 6-2900-129110.Apr 9, 2009 · N750FD · Airbus A300B4622RSDR IPXA09555595Skin · tornINSPECTION TYPE:C2 RT WING FIXED LE UPPER SURFACE IS TORN BETWEEN NR 7 AND NR 8 LE SLATS. REPAIRED RT WING FIXED LE UPPER SURFACE BETWEEN NR 7 AND NR 8 SLATS IAW STANDARD REPAIR MANUAL EO B757-5740-11855-D.Apr 8, 2009 · N402UP · Boeing 75724APFSDR COMA2009041350115Skin · crackedRT WING PLANK AT WS 148.019 JACKING POINT IS CRACKED. REMOVED DAMAGE AND INSTALLED PERMANENT REPAIR PARTS PER REO 601R-57-21-130 REV H.Apr 8, 2009 · N720SW · Cndair CL6002B19SDR COMA2009040850112Skin · crackedRT LOWER WING PLANK HAS CRACK INDICATION AT FUEL TANK ACCESS HOLE, FOR PANEL 650BB. BLENDED ACCESS HOLE CUTOUT TO REMOVE CRACK INDICATION IAW REO 601R-57-21-30, REV G.Apr 8, 2009 · N958CA · Cndair CL6002B19SDR DHLA2009801002Skin · delaminatedRT WING, PANEL NR 577A EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED WING PANEL NR 577A IAW SRM 51-3-0, SRM 51-3-1.Apr 7, 2009 · N801DH · Doug DC873FSDR DHLA2009801001Skin · delaminatedLT WING PANEL EXT SKIN DELAMINATED (STA XW 0 - XW 37.000). REMOVED AND REPLACED DELAMINATED LT WING PANEL IAW SRM 51-3-0 SRM 51-3-1.Apr 7, 2009 · N801DH · Doug DC873FSDR IPXA09M55585Doubler · crackedINSPECTION TYPE:1C LT WING FIXED LE COMPARTMENT BEADED DOUBLER CRACK IN 2 PLACES AT STA 562 XORS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES, DOUBLER AND FILLER IAW MD-11 SRM 57-10-00 FIG 27.Apr 7, 2009 · N291UP · Doug MD11FSDR WRLA2009114Structure · crackedDURING C-CHK IN TPE INSPECTION FOUND CRACK ON LEFT WING T/E BEAL SEAL LAND Y=1474 & Z=100 (REF NRC U05016). REPLACED LEFT WING T/E BEAL SEAL LAND AT Y=1474 & Z=100 PER MD-11F SRM 51-33-01 VOL 2 REV 40. CONDITION CHECK NORMAL & JOB COMPLETE.Apr 6, 2009 · N279WA · Doug MD11SDR IPXA09M55625Skin · crackedINSPECTION TYPE:1C LEFT WING TELESCOPIC DUCT CUTOUT UPPER CUTOUT CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-10-00 FIG 43 SHT 1-5.Apr 6, 2009 · N270UP · Doug MD11FSDR IPXA09M55617Skin · misrepairedINSPECTION TYPE:1C RT WINGLET REQUIRE LE BULLNOSE REMOVED TO EVALUATE AND NDT EXISTING REPAIR, SEQ W4-01, REPAIR NOT PER SRM. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5720-31992-A.Apr 6, 2009 · N270UP · Doug MD11FSDR UALA2009040700994Skin · crackedSKIN CRACKS FOUND ON F/O WALKAROUND UNDER LT WING OUTSIDE ENGINE POD. CLOSE INSPECTION FOUND ACCESS PANEL 521AB (ACCESS PLATE FOR LEADING EDGE SLAT OUTBOARD OF NR 1 ENG PYLON) WITH TWO CRACKS. REPLACED PANEL 521AB.Apr 6, 2009 · N513UA · Boeing 757222SDR IPXA09M55375Cap · erodedINSPECTION TYPE:N/A LT WINGLET TIP UPPER CAP LEADING EDGE EROSION D396229. C/W REPAIR OF LT WINGLET TIP UPPER CAP IAW EO MD11 5720 32859 ON NR 354833. THIS CLEARS DEFERRAL.Apr 6, 2009 · N260UP · Doug MD11FSDR IPXA09855352Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 752-W3-8 LT WING CENTER L/E LWR SURFACE REPAIR STA XFS 426 DOUBLER IS NOT ALUMINUM MATERIAL REF APPX H ITEM A-31. REPAIR ACCOMPLISHED PER REO-G1600 AND EO DC8-5720-32217-A.Apr 6, 2009 · N752UP · Doug DC871FSDR FDEA200904061192Skin · crackedRIGHT WING LEADING EDGE, ANTI-ICE TELESCOPIC DUCT DOOR CUTOUT, CRACKS FOUND AT UPPER CORNER EDGES, STA XOS 464 AND STATION XOS 470. REPAIR CARRIED OUT AS PER SRM 57- 10-00 FIGURE 43 VOLUME I, REVISION 40. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30-5Apr 6, 2009 · N605FE · Doug MD11FSDR ASOA200900391Skin · damagedLT WING LOWER PLANK ACCESS HOLE 540CB HAS MULTIPLE HFEC INDICATIONS 0.1 INCH IN LENGTH, 50 PERCENT 80 PERCENT FSH ON THE FWD CRITICAL AREA OF THE LANDING. INDICATIONS ARE MARKED ON THE ACFT. FAILS NDT AT THIS TIME. C/W EC/TC EO 600-57-81 & C/W IAW REO 601R-Apr 5, 2009 · N829AS · Cndair CL6002B19SDR ASOA200900390Skin · damagedLT WING LOWER PLANK ACCESS HOLE 540DB HAS MULTIPLE HFEC INDICATIONS 0.1 INCH IN LENGTH, 50 PERCENT 80 PERCENT FSH ON BOTH FWD AND AFT CRITICAL AREAS OF THE LANDING. INDICATIONS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. C/W EC/TC EO 600-57-81 C/W Apr 5, 2009 · N829AS · Cndair CL6002B19SDR ASOA200900389Skin · damagedRT WING LOWER PLANK ACCESS HOLE 640CB HAS MULTIPLE HFEC INDICATIONS NOTED ON THE O/B NON-CRITICAL AREA OF THE LANDING. INDICATIONS ARE APPROX 0.1 INCH LONG WITH 50 PERCENT 80 PERCENT FSH SIGNALS. AREAS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. C/Apr 5, 2009 · N829AS · Cndair CL6002B19SDR ASOA200900388Skin · damagedRT WING LOWER PLANK ACCESS HOLE 640DB HAS MULTIPLE HFEC INDICATIONS NOTED ON BOTH FWD AND AFT LANDINGS IN THE CRITICAL AREAS. INDICATIONS ARE APPROX 0.1 INCH LONG WITH 50 PERCENT 80 PERCENT FSH SIGNALS. AREAS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIApr 5, 2009 · N829AS · Cndair CL6002B19SDR ASOA200900387Skin · damagedRT WING LOWER PLANK ACCESS HOLE 640FB HAS MULTIPLE HFEC INDICATIONS NOTED ON THE AFT PORTION OF THE LANDING. INDICATIONS ARE APPROX 0.1 INCH IN LENGTH WITH 50 PERCENT 80 PERCENT FSH SIGNALS. AREAS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. INDICATApr 5, 2009 · N829AS · Cndair CL6002B19SDR IPXA09M55334Doubler · crackedINSPECTION TYPE:N/A NRC 354831 ISSUED FOR MAJOR REPAIR LT WING L/E INTERNAL DOUBLER CRACKED AT STA 908. REPAIRED LT WING L/E STRINGER DOUBLER AT STA 908 PER EO MD11-5720-32 954-A ON NRC 354831.Apr 4, 2009 · N260UP · Doug MD11FSDR IPXA09M55333Skin · crackedINSPECTION TYPE:N/A NRC 354202 ISSUED FOR MAJOR REPAIR REFERENCE L/P 169230 ITEM 1 LT WING L/E SKIN CRACK AT STA 908. REPAIRED LT WING L/E SKIN AT STA 908 PER EO MD11-5720-32954 ON NRC 3 54202.Apr 4, 2009 · N260UP · Doug MD11FSDR IPXA09855328Skin Panel · misrepairedINSPECTION TYPE:SV SURVEY SEQ 752-W4-17 REPAIR AT RT WING UPPER SURFACE STA XRS 467AAT FRONT SPAR DOES NOT CORRELATE TO AN SRM REPAIR. REPAIR ACCOMPLISHED PER TIMCO REO-12644 AND IPXA EO DC8-5710-32906-A.Apr 4, 2009 · N752UP · Doug DC871FSDR LR7A2009040900048Skin · corrodedDURING SCHEDULED C-4 CHECK PER JOB CARD HC5711, FOUND LT OUTTER WING LOWER T/E SKIN LOOSE RIVETS, SCRATCHES, SURFACE CORROSION WITH MULTIPLE EXISTING REPAIR PATCHES AT OWS0 TO OWS84. REPAIRED BY REPLACING T/E SKIN IAW SMP583 CHAPTER 51-70.Apr 3, 2009 · N406LC · Lkheed 382GSDR FDEA200904031168Skin · corrodedFOUND CORROSION AROUND FASTENERS ON TOP SKIN OF FALSE SPAR, RIB 4-5A. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION AND REPLACEMENT OF FASTENERS IAW RAS/BAE/1009315/2009 ISS A, APPROVED BY EA 6-5720-129104.Apr 3, 2009 · N750FD · Airbus A300B4622R
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