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 IXXA06SMN259SSkin · dentedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND OUTER WING, OUTBOARD LEADING EDGE DENTED, FROM STATION XFS 885.000 TO STATION XFS 920.000. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. FABRICATED SKIN (AL 7075 T6 0.050Jul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN257SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB LEADING EDGE LOWER SKIN CORRODED FROM STA XFS566.250 TO STA XFS578.750. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 (XFS591.250). REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SRM 5Jul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN247SPanel · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING IB UPPER PANEL DENTED, AT STATION XW40.000. REMOVED DAMAGED SKIN IAW SRM 57-1-0 PAGE 1, SRM 51-1-21. FABRICATED SKIN WITH (AL 2024 T3 0.025) AND BONDED DOUBLER (AL 2024 T3 0.020) IAW SRM 57-7-1 FIG. 1 ITEM A, Jul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN263SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND WING CENTER LEADING EDGE UPPER SKIN WITH NON STANDARD REPAIR FROM STATION XFS 360.250 TO STATION XFS 410.250. REMOVED EXISTING REPAIR IAW DC-8 SRM 51-1-20D. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER (AJul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN262SRepair · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND LEFT HAND WING INBOARD LEADING EDGE UPPER SKIN WITH A NON STANDARD REPAIR AT STATION XCW69.00. REMOVED EXISTING REPAIR, IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. FABRICATED REPAIR DOUBLER (AL 7075 T6 0.071) IAW SEMAN DRAWJul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN255SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT HAND WING INBOARD LEADING EDGE UPPER SKIN CORRODED FROM STATION XW5.000 TO STATION XW22.000. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. REMOVED CORROSION IAW DC-8 SRM 1-1-8 FOUND OUT OF LIMITS. REMJul 28, 2006 · N605AL · Doug DC873FSDR IXXA06SMN249SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION FOUND RIGHT HAND WING OUTBOARD LEADING EDGE INTERNAL SURFACE UPPER SKIN WITH A NON STANDARD REPAIR FROM STATION XFS 560.000 TO STATION XFS 622.500. REMOVED EXISTING REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICJul 28, 2006 · N605AL · Doug DC873FSDR QXEA200601999Skin · corrodedPDX C4 LIGHT FRETTING AROUND RIGHT HAND FUEL PANEL 624CT APERATURE. REPARIED IAW DHC-8-200 RD 8-57-984.Jul 28, 2006 · N351PH · Dhav DHC8202SDR QXEA200601998Skin · corrodedPDX C4 LIGHT FRETTING AROUND LEFT HAND FUEL PANEL 524AT APERATURE. REPARIED IAW DHC-8-200 RD 8-57-611.Jul 28, 2006 · N351PH · Dhav DHC8202SDR QXEA200601997Skin · corrodedPDX C4 LIGHT FRETTING AROUND LEFT HAND FUEL PANEL 524BT APERATURE. REPARIED IAW DHC-8-200 RD 8-57-633.Jul 28, 2006 · N351PH · Dhav DHC8202SDR QXEA200601996Skin · corrodedPDX C4 LIGHT FRETTING AROUND LEFT HAND FUEL PANEL 524CT APERATURE. REPARIED IAW DHC-8-200 RD 8-57-984.Jul 28, 2006 · N351PH · Dhav DHC8202SDR UIEA200600189Panel · corrodedL/W-L/E WING PANEL CORRODED TWO SPOTS AREA IS I/B ON MOST I/B L/E NEAR FUSELAGE.Jul 28, 2006 · N506MC · Boeing 7472D3BSDR 06FDEA2730Skin · crackedRIGHT HAND WING, LEADING EDGE UPPER SURFACE TELESCOPIC DUCT CUTOUT FOUND CRACKED. COMPLIED WITH FEDEX E.A 1-5730-103251, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 28, 2006 · N592FE · Doug MD11SDR 06FDEA2729Skin · crackedLEFT HAND WING, ANTI-ICE DUCT LEADING EDGE CUTOUT INBOARD CORNER FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-103522. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 28, 2006 · N592FE · Doug MD11SDR 06FDEA2713Skin · gougedLT WING FIXED LEADING EDGE UPPER SURFACE AT STA XORS 164 FOUND WITH DEEP GOUGE. REPAIRED PER SRM 57-10-00 VOLUME, FIGURE 24. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.Jul 28, 2006 · N592FE · Doug MD11SDR S9B2006F00003Skin · corrodedCORRODED SKIN ALONG THE FIRST ROW OF RIVETS ON UPPER LEFT WING IB OF THE NACELLE BETWEEN STATIONS 60 AND 72.5. CORRODED SKIN WAS TRIMMED OUT AND AN EXTERNAL PATCH RIVETED IN PLACE IAW RD6-57-077. (K)Jul 26, 2006 · N888PV · Dhav DHC6300SDR ASAA0640818Skin · gougedFOUND RT OB AFT FLAP LE GOUGED. REPAIRED PER SRM 57 43 01 FIG 201.Jul 26, 2006 · N760AS · Boeing 7374Q8SDR WRLA2006034Access Panel · corrodedDURING "C" CHECK IN SAT FOUND LEFT WING I/B T/E ACCESS PANEL 541CR HAS THREE AREAS OF CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 IN ALL THREE AREAS. FABRICATED REPAIR DOUBLERS AND BONDED THE 3 AREAS IAW SRM 51-71-00. SEALED AND PRIMED REPJul 23, 2006 · N303 · Doug DC1030FSDR 06FDEA2662Skin · crackedRIGHT WING EXTERIOR, LEADING EDGE LOCATION WITH TELESCOPIC DUCTING CUTOUT TOP CORNER INBOARD AND OUTBOARD FOUND CRACKED. CRACKED AREA TRIMMED OFF AND REPAIR CARRIED OUT PER FEDEX E.A. 1-5730-102132, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 23, 2006 · N591FE · Doug MD11SDR TRAX200600547Skin · corrodedFOUND CORROSION ON FUEL TANK ACCESS LANDS OF LT WING ACCESS 510AB AND 540BB.Jul 22, 2006 · N977EV · Cndair CL6002B19SDR ASAA0640799Skin · dentedRT WING T/E O/B AFT FLAP T/E DENTED A=1.4 Y=.089 A Y=15.73. REMOVED REPAIRED AND REINSTALLED RT WING OB AFT FLAP IAW SRM 51 70 10 57 53 02.Jul 22, 2006 · N792AS · Boeing 737490SDR SWAA062598Skin · crackedDURING SCHEDULED 14Y CHECK, FOUND LT WING SKIN CRACKED AT LOWER SURFACE MID SPAR, OUTBOARD STRUT. REPAIRED SKIN PER EA.Jul 22, 2006 · N524SW · Boeing 7375H4SDR IXXA06SMN233SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LEFT WING LEADING EDGE UPPER SKIN CORRODED, AT STATION XF 566.250. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-1 FIG 2G. TRIMMED OJul 21, 2006 · N605AL · Doug DC8*SDR 06FDEA2649Doubler · crackedLEFT WING, LEADING EDGE AT ABOUT STA XORS 647 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT PER FEDEX E.A. 1-5730-102133, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 21, 2006 · N591FE · Doug MD11SDR IXXA06SMN232SRepair · improperDURING ROUTINE C CHECK INSPECTION, LT WING L/E HAS NON STANDARD REPAIR, XFS 544.000 - XFS 560.000.Jul 21, 2006 · N605AL · Doug DC8*SDR IXXA06SMN229SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT WING - PNEU HOLE LWR SKIN CRACKED ¾ APPROX XFS 597.500.Jul 21, 2006 · N605AL · Doug DC8*SDR IXXA06SMN231SRepair · improperDURING ROUTINE C CHECK INSPECTION, RT WING. - OTBD L/E EXTERNAL SECTION WITH NON STANDARD REPAIR XFS 872.000 - XFS 885.000.Jul 21, 2006 · N605AL · Doug DC8*SDR IXXA06SMN230SRepair · improperDURING ROUTINE C CHECK INSPECTION, RT WING.- OTBD L/E EXTERNAL PART NON STANDARD REPAIR WITH CHERRY MAX; XFS 603.750 XFS 610.000.Jul 21, 2006 · N605AL · Doug DC8*SDR EIA2006192Skin Panel · corrodedCENTER TANK LOWER SKIN ABOVE NR 3 HEAT EXCHANGER HAS EXFOLIATION CORROSION. REMOVED CORROSION AND FABRICATED REPAIR PER ECRA 470-57-291-2.Jul 20, 2006 · N470EV · Boeing 747273CSDR EIA2006187Skin Panel · corrodedRT WING LOWER SKIN, PREVIOUS REPAIR, FWD CHORD, WS 1320 - 1310 HAS EXFOLIATION CORROSION, TWO LOCATIONS. REPAIRED PER ECRA 470-57-285-2 AND B747 SRM 57-30-03.Jul 20, 2006 · N470EV · Boeing 747273CSDR UIEA200600182Skin · delaminatedLT WING UPPER SURFACE LEADING EDGE PANEL AT OLES STA. 1336.0 AND 1495.0 HAS 2 EACH SMALL AREAS OF DELAMINATION. AREAS ARE BOTH 2.0 INCH BY 2.0 INCH. ACCOMPLISHED PREPREG 250 DEGREE PERMANENT HOT BOND REPAIR SRM 51-40-12 AND SRM 51-40-09 FIG. 18. ALSO, REFERENJul 20, 2006 · N536MC · Boeing 747228FSDR KCSA061230Skin · corrodedCORROSION ON WING CENTER SECTION UPPER SKIN AT STA 1210 AND 1220 RBL 98 UNDER MAIN DECK FLOOR.Jul 20, 2006 · N706CK · Boeing 747249FSDR A6WA200640286Skin · corrodedFOUND LEFT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 540FB, HOLE NR 8 AT WS 139 HAS MINOR CORROSION APPROX .003 INCH DEEP ON 90 PERCENT OF CIRCUMSTANCE. REPAIRED THE LEFT WING LOWER PLANK PANEL CUTOUTS IAW BSC EO 601R-57-9567A. (M)Jul 18, 2006 · N449AW · Cndair CL6002B19SDR A6WA200640285Skin · corrodedFOUND LEFT WING PLANK ACCESS CUTOUT FLANGE AT FUEL PANEL 510AB HOLE NR 2 AT WS 11.00 HAS MINOR CORROSION APPROX .002 INCH DEEP ON 60 PERCENT OF CIRCUMFERENCE. MAINTENANCE REPAIRED THE LEFT WING PLANK FUEL PANEL CUTOUT IAW BSC EO 601R-57-9567A. (M)Jul 18, 2006 · N449AW · Cndair CL6002B19SDR 06FDEA2626Skin · gougedLT WING LEADING EDGE SKIN IS GOUGED AT PYLON PANEL ATTACH LT SIDE. REPAIR CARRIED OUT AS PER EA 1-5720-102311. LEADING EDGE SKIN CHAFING DAMAGE COMMON TO THE LT WING PYLON. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.Jul 18, 2006 · N527FE · Doug MD11SDR 06FDEA2610Skin · crackedFOUND LT WING TIP UPPER SIDE AT STA XW925 HAS REPAIR DOUBLER (12 BY 5) AND TRIPLER(6.5 BY 4). REMOVE PANEL IAW SRM 51-31-01 VOL2. REMOVED 2 DOUBLER IAW SRM 51-31-01VOL 2. REMOVED SEALANT IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDT SPM 8. FOUND CRJul 18, 2006 · N365FE · Doug DC1010SDR MWEA060151Skin · corrodedEVIDENCE OF CORROSION ON RIGHT WING LEADING EDGE SKIN, LOWER SURFACE JUST FORWARD OF FUELING PANEL, WS 245-280 3 AREAS. FABRICATED AND INSTALLED DOUBLER.Jul 17, 2006 · N803ME · Doug DC981SDR 2006UALA01406Skin · corrodedLEFT WING TANK ENTRY CUTOUT AT PANEL LOCATION 7212L HAS CORROSION PITTING ON INTERIOR SURFACE. MAJOR REPAIR: REPAIR OF INTERNAL FLANGE ACCOMPLISHED USING A BLEND REPAIR.Jul 16, 2006 · N333UA · Boeing 737322SDR 06FDEA2501Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS670. REPAIR CARRIED OUT PER FEDEX EA 1-5730-100709. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 10, 2006 · N583FE · Doug MD11SDR UPS06847551Doubler · crackedINSPECTION TYPE:C1 RT WING L/E REPAIR DOUBLER CRACKED ABOVE NR 4 PYLON. REMOVED, FABRICATED AND INSTALLED DOUBLER AND INTERNAL DOUBLER IAW SRM 51-1-20D, 57-02-01A AND 51-1-26.Jul 8, 2006 · N894UP · Doug DC873FSDR 06FDEA2482Access Panel · crackedRT WING LEADING EDGE CAVITY THRU ACCESS PANEL 625AB CEILING AREA FINGER DOUBLER CRACKED AT XOS 692. REPAIRED AS PER FEDEX EA 1-5730-100704. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11SDR 06FDEA2481Finger Doubler · crackedRT WING LEADING EDGE CAVITY THRU ACCESS PANEL 619DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 643. REPAIRED AS PER FEDEX EA 1-5730-100703. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11SDR 06FDEA2480Finger Doubler · crackedLT WING LEADING EDGE CAVITY THRU ACCESS PANEL 519CB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 613. REPAIRED AS PER FEDEX E.A. 1-5730-100687. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11SDR 06FDEA2479Finger Doubler · crackedLT WING LEADING EDGE CAVITY THRU ACCESS PANEL 526DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 883. REPAIRED AS PER FEDEX E.A. 1-5730-100702. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11SDR 06FDEA2477Finger Doubler · crackedRT WING LEADING EDGE CAVITY THRU ACCESS PANEL 619DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 680. REPAIRED AS PER FEDEX E.A. 1-5730-100704.Jul 8, 2006 · N614FE · Doug MD11SDR 06FDEA2476Finger Doubler · crackedLT WING LEADING EDGE CAVITY THRU ACCESS PANEL 525DB CEILING AREA, FINGER DOUBLER CRACKED AT XOS 705. REPAIRED AS PER FEDEX E.A.1-5730-100701. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11FSDR 06FDEA2475Access Panel · crackedRT WING LEADING EDGE CAVITY THRU ACCESS PANEL 619DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS667. REPAIRED AS PER FEDEX E.A. 1-5730-100704. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11SDR NACA20060044Skin · crackedLT HAND WING LOWER SKIN STA. 210, STR. 22 WING SKIN CRACKED AFT OF CENTER SPAR. REPAIRED LT WING LOWER SKIN STA. 213, STR. 22 REF: NAC DRAWING: NAC2006-05 REV: 1R DATED 12 JULY 2006.Jul 7, 2006 · N99330 · Doug DC6ASDR IXXA06SMN217SSkin · crackedDURING ROUTINE C CHECK INSPECTION, 'LT CTR L/E EXTERNAL PLATING SKIN CORRODED, CRACKED 1"; XOLDI 6.22 - XW 408.000.Jul 7, 2006 · N41CX · Doug DC8*SDR IXXA06SMN214SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING T/E UPPER EXTERNAL SKIN CORRODED ON SOME AREAS STA XRS 74.000.Jul 7, 2006 · N41CX · Doug DC8*
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