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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA09556666Access Panel · damagedINSPECTION TYPE:C1 RT WING PANEL 621HB HAS DAMAGE TO INNER SURFACE 10 INCHES FROM I/B END 5.5 INCHES FROM T/E. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-41-01-1A FIG 101. REMOVED DAMAGE, NO CONTAMINATION, CLEANED, FABRICATED REPAIR PLIES BMS8-79 (1581. OK SDR IPXA09M56710Doubler · misrepairedINSPECTION TYPE: 1C REPAIR SURVEY SEQUENCE NR 281-W3-06 LT WING UPPER WINGLET L/E REPAIR DOUBLER DOES NOT CORRELATE TO SRM. REMOVED, FABRICATED, AND INSTALLED NEW REPAIR DOUBLER IAW EO MD11-5730-34297-A.SDR FDEA200907022457Skin · damagedFOUND ON RH WING LOWER SKIN PANEL RIB 9 AFTER DOUBLER REMOVAL SOME DAMAGES IN FASTENER HOLES IN THIS AREA. REPAIR PERFORMED BY NDT INSPECTION FOR CRACKS, OVERSIZING OF HOLES AND REINSTALLING DOUBLER IAW. RAS/BAE/1009704/2009 ISS.A , APPROVED BY EA 6-5710-13SDR FDEA200907022456Skin · damagedFOUND ON LH WING LOWER SKIN PANEL RIB 9 AFTER DOUBLER REMOVAL SOME DAMAGES IN FASTENER HOLES IN THIS AREA. REPAIR PERFORMED BY NDT INSPECTION FOR CRACKS , OVERSIZING OF HOLES AND DRILL MISSING HOLE 38 IAW. SB 57-6064 AND REINSTALLING DOUBLER IAW. RAS/BAE/1SDR GUUA93957070109ASkin · corrodedDURING MX DISCOVERED RT FUEL LEAK AT RT WING ACCESS PANEL 632AT. REPAIRED SKIN .SDR GUUA92757070109ASkin · delaminatedDURING SCHEDULED INSP, DISCOVERED LT AND RT WING SKIN DELAMINATED AROUND FUEL ACCESS PANELS 531CB, 532CB, 531DB, 532DB, 532FB, 541AB, 632AT,632CB AND 632DB. REPAIRED WING SKIN AROUND FUEL ACCESS PANELS.SDR CALA2009070200356Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1040 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200355Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1026 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE SDR CALA2009070200354Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1020 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200353Skin · corrodedCORROSION NOTICED ON RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1015 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200352Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1010 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200351Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1004 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200350Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGE STATION 999 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200349Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 994 WITH SOME METAL FLAKING REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 994 PESDR CALA2009070200348Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STA 983 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 983 PER ESDR CALA2009070200347Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 977 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 977 SDR CALA2009070200346Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STA 968 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 968 PER SDR CALA2009070200345Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 965 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 965 SDR CALA2009070200344Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 960 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 960 SDR FDEA200907012435Skin · looseRT WING EXT SURFACE FOUND NR 180 EA LOOSE FASTENERS ON UPPER EXT SKIN OUTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 & SRM 57-20-00 FIG 2 VOL I.SDR FDEA200907012434Skin · wornFOUND ELONGATED HOLES ON PYLON SUPPORT BRACKETS AND BOTTOM SKIN LT WING BUSH REPAIR PERFORMED IAW DRAWING R571-50532 AND SB A300-29-6058, APPROVED BY RAS/BAE/101319/2009 ISS A AND EA 6-2900-131225.SDR FDEA200907012433Skin · wornFOUND ELONGATED HOLES ON PYLON SUPPORT BRACKETS AND BOTTOM SKIN RT WING BUSH REPAIR PERFORMED IAW DRAWING R571-50532 AND SB A300-29-6058, APPROVED BY RAS/BAE/101319/2009 ISS A AND EA 6-2900-131225.SDR IPXA09M56701Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 281-W3-02 LT WING L/E TELESCOPIC REPAIR DOUBLER DOES NOT CORRELATE TO SRM AND DAMAGED INBOARD UPPER CORNER STA ZOS 4 61-XOS 473. REMOVED EXISTING REPAIR FROM LT WING L/E TELESCOPIC DUCT CUTOUT AT XOS 464 AND XOS 470. FABRSDR FDEA200906262319Skin · crackedRT WING LWR EXT SURFACE FOUND CRACKS AND NR 100 EA LOOSE FASTENERS ON LWR EXT SKIN OTBD FLAP. REPAIRED AREA IAW SRM 57-10-00 FIG 7, SHT 3, VOL I.SDR GUUA93557062509AAccess Panel · damagedPILOT REPORTED FUEL LEAK FOUND UNDER LT WING INSP PANEL OTBD OF ENGINE. ACCOMPLISHED EXTERNAL REPAIR DOUBLER ON LT WING FUEL PANEL 531EB.SDR FDEA200906252301Skin · damagedFOUND OLD BLEND OUT REPAIR ON RT WING TOP SKIN RIB 4-5 DEEPER THAN REPORTED. REPAIR PERFORMED BY NDT FOR CRACK FREE AND CORRSOION FREE CONDITION WITH REMAINING MATERIAL ACCEPTABLE IAW RAS/BAE/0934/2004 ISS. C , APPROVED BY EA 6-5730-131233.SDR GUUA93757062409ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT UPPER WING SKIN T/E CORROSION AND DEBOND BETWEEN WING STA 136.036 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.SDR FDEA200906232243Skin · crackedLT WING NR 3 SLAT, WING L/E TELESCOPIC DUCT DOOR CUT-OUT AREA FOUND CRACKED AT INBD AND OTBD SIDE. REPAIR CARRIED OUT AS PER E.A. 1-5730-131723, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232242Skin · crackedRT WING NR 3 SLAT, WING L/E TELESCOPIC DUCT DOOR CUT-OUT AREA FOUND CRACKED AT INBD AND OTBD SIDE. REPAIR CARRIED OUT AS PER E.A. 1-5730-131722, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906232241Access Panel · crackedRT WING L/E LOWER ACCESS FOUND CRACKED AT APPROX XOS 612. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I, REVISION 40. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 107.SDR C2XA09TY123Skin Panel · crackedTYS DURING A CURRENT 6C INSPECTION THE LEFT LOWER WING SKIN WAS FOUND CRACKED AT THE LOWER INBOARD FLAP SHROUD O/B HOLE. MAINTENANCE REPAIRED THE LEFT LOWER WING SKIN AROUND THE LOWER INBOARD FLAP SHROUD OUTBOARD HOLE IAW EC 5710-01160. ALL WORK ACCOMPLISHEDSDR HNAA2009082900266Skin · corrodedCATEGORY 1 CORROSION FOUND UNDER THE LT WING AUX BOOST PUMP EXTERNAL ANTI FRET RING ON THE LWR WING SKIN. LT AUX BOOST PUMP EXTERNAL AND INTERNAL SURFACE OF DOUBLER REPAIRED IAW RD8-57-4320 AND RD8-57-1907.SDR COEA2009062201816Skin · corrodedHEAVY CHECK: FOUND LEVEL 2 CORROSION ON LT WING FEEDER TANK CUTOUT FLANGE FOR UPPER ACCESS PANEL 522CT.SDR FDEA200906222198Panel · delaminatedFOUND DELAMINATION ON LT WING OUTER FIXED T/E TOP SKIN PANEL REPAIR PERFORMED IAW SRM 51-77-11 PARA 3.E AND 4 M, APPROVED BY RAS/BAE/1009714/2009 ISS.A AND EA 6-5750-131239.SDR GUUA92757062009AAccess Panel · corrodedDURING INSP OF LT WING FUEL LEAK, FOUND FUEL ACCESS PANEL 532AB HAS CORROSION AND DEBOND ON INTERNAL RING. INSTALLED REPAIR RINGS AT LT FUEL ACCESS PANEL 532AB.SDR ASAA0995967Skin · gougedLT WING FIXED LEADING EDGE BULL NOSE IS GOUGED JUST I/B OF NR 1 PYLON OUT OF LIMITS. BLENDED DAMAGED AREA REFINISHED AREA.SDR IPXA09M56444Skin · damagedINSPECTION TYPE:SV LT WING LWR SKIN APPROX XOS 650 HAS ELONGATED FASTENER HOLE APPROX 2 INCHES AFT OF L/E OF WING REF NRC 344110. FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5730-01-A1846 AND IPXA EO MD11-5730-33931-A REF NRC 344110.SDR FDEA200906182162Panel · crackedLT WING INBD T/E FIXED PANEL AT W STA 330, WIGGLE PLATE ASSY FOUND CRACKED. CRACKED PLATE REPLACED IAW SRM 51-40-02 REV 97 IAW DWG 113N1635. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR IPXA09M56568Skin · crackedINSPECTION TYPE:C LT WING FIXED L/E AREA, FOUND CRACK AT NR 3 SLAT TELESCOPIC DUCT UPPER DOOR CUTOUT SKIN AS MARKED. CRACKED AREA ON DUCT UPPER DOOR CUTOUT SKIN TRIMMED OFF & HFEC C/O ON TRIMMED OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER & FILLER FABRISDR IPXA09M56443Skin · damagedINSPECTION TYPE:SV LT WING L/E XOS 621-629 CENTER REPAIR CUTOUT HAS OBLONG FASTENER HOLE AT LWR I/B CORNER OF RIVET PATTERN REF NRC 344110. FABRICATED AND INSTALLED REPAIR IAW SAA EA 011-5730-01-A1846 AND IPXA EO MD11-5730-33931-A REF NRC 344110.SDR FDEA200906172139Skin · crackedLT OTBD FORE FLAP WBL 442, CRACK ON CUTOUT FWD OF ATTACH FITTING. TRIMMED OUT CRACKED AREA, DIM 0.100 INCH LENGTH IAW SRM 51-10-1. FOUND WITHIN LIMITS IAW SRM 57-50-1. FIG 3 TREATED AND PRIMED IAW SRM 51-10-2.SDR IPXA09M56569Skin · crackedINSPECTION TYPE:C RT WING FIXED L/E AREA, NR 3 SLAT TELESCOPIC DUCT UPPER DOOR CUTOUT SKIN CRACK AS MARKED. CRACK ON DOOR CUTOUT SKIN TRIMMED OFF WITH HFEC C/O, FOUND NO CRACK EVIDENT. REPAIR DOUBLER & FILLER FABRICATED. 10X INSP C/O, FOUND 'SATIS'. HFEC OSDR IPXA09M56384Skin · misrepairedINSPECTION TYPE:SV REMOVE EXISTING REPAIRS FROM LT WING AT XOS 609-621, XOS 621-629, AND XO XOS 629-644. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLERS PER EA 011-5730-01-A 1846.SDR FDEA200906162120Skin · crackedLT WING NR 14 SLAT TRACK CUT-OUT OTBD EDGE SURFACE FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG21 VOL1 REV40.SDR IPXA09M56581Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE: 275-W4-001: RT WING, LWR SURFACE STA XFS 906 TO XFS 932 REPAIR NEEDS VALIDATION. EXISTING REPAIR DOUBLER 02 EA AT AFFECTED AREA REMOVED. HFEC OPEN HOLE INSP C/O ON REWORKED AREA, FOUND NO CRACK EVIDENT. 10 VISUAL INSP C/O SDR FDEA200906152100Skin · chafedFOUND CHAFING MARKS ON LT WING L/E "D" NOSE JACK RIB 1-2 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR , NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1009485/2009 ISS.A , APPROVED BY EA 6-5740-129116.SDR FDEA200906152093Skin · crackedDURING INSPECTION RT WING EXT. STRUCTURE L/E FOUND CRACK ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2, VOL I.SDR FDEA200906152092Skin · crackedDURING INSPECTION LT WING EXT. STRUCTURE L/E FOUND CRACK ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.SDR IPXA09M56386Doubler · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ 257-W3-01 LT WING FIXED L/E EXISTING REPAIR DOUBLER GOUGED. REMOVED DOUBLER, CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW MD-11 SRM 57-10-00 FIG 43 SHT 1-5.SDR IPXA09M56346Skin · damagedINSPECTION TYPE:N/A LT WING UPPER WINGLET TIP SKIN DAMAGED. REPAIRED IAW EO MD-115720-33864.
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