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 UPS08852202Skin · damagedINSPECTION TYPE:C3 LEFT WING CENTER L/E REPAIR DOUBLER HAS OVERSIZED SCREW HOLES AT OUTBOARD END OF SLOT VANE. FABRICATED AND REPLACED FILLER AND DOUBLER AT LEFT WING CENTER L/E AT OUTBOARD END OF SLOT VANE IAW EO DC8-5720-7767-A.Apr 21, 2008 · N894UP · Doug DC873FSDR UPS08852114Skin · damagedINSPECTION TYPE:C3 LT WING CENTER LE LOWER OUTBD EXTERIOR SKIN HAS OVERSIZED SCREW HOLES AT SLOT CUTOUT. REPAIRED LT WING LE LOWER OUTBD EXTERIOR SKIN SCREW HOLES IAW SRM 57-03 -03-0 FIG 005 AND EO DC8-5720-7767-A.Apr 21, 2008 · N894UP · Doug DC873FSDR UPS08852120Skin · crackedINSPECTION TYPE:C3 LT WING OUTBD LE 5 CRACKS AT 3 SCREW HOLES XFS 603.75 TO XFS 606.75 UPPER SURFACE INBD END, EXTERIOR SKIN. REPAIRED LT WING OUTBD LE EXTERIOR SKIN FROM XFS 603.75 TO XFS 606.75 IAW SRM 57-02-01-0 FIG 038 AND SRM 57-02-01-0.Apr 20, 2008 · N894UP · Doug DC873FSDR IXXA08SMN179SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT AND RIGHT INNER WING TRAILING EDGE STRUCTURE HAS IMPROPER REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. INSTALLED REPAIR PART KIT ON LT AND RT INNER WING TRAILING EDGE STRUCTURE. CLOSED MLG DOORS AND RApr 19, 2008 · N821BX · Doug DC871FSDR IXXA08SMN172SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN CRACKED BETWEEN STATION XF 375.000 - 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED Apr 19, 2008 · N821BX · Doug DC871FSDR IXXA08SMN180SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING NR 1 LOWER PART STUB WING HAS IMPROPER REPAIR REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED EXITING REPAIR. FABRICATED EXTERNAL DOUBLER, AND INTERNAL DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TRApr 19, 2008 · N821BX · Doug DC871FSDR IXXA08SMN181SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LOWER LEADING EDGE HAS IMPROPER REPAIR AT STATION XFS 360.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CApr 19, 2008 · N821BX · Doug DC871FSDR 2008UALA02281Panel · damagedMOST INBOARD LOWER RT LEADING EDGE PANEL INBD CORNER BROKEN OFF. APPROX. 3 INCH BY 1-2 INCH REINFORCED LEADING EDGE SECTION MISSING. REMOVED FOR REPAIR. REPAIRED BY SHOP. REINSTALLED PANEL. ACFT OK FOR SERVICE.Apr 19, 2008 · N666UA · Boeing 767322SDR IXXA08SMN159SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER SKIN IMPROPER REPAIR AT STATION XF 375.000 - STATION XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDEDApr 18, 2008 · N821BX · Doug DC871FSDR IXXA08SMN157SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CRACKED AT STATION XFS 335.000 - XFS 341.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FAApr 18, 2008 · N821BX · Doug DC871FSDR IXXA08SMN160SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.000, STRINGER 7. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED NEW SKIN, ANDApr 18, 2008 · N821BX · Doug DC871FSDR IXXA08SMN138SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING DOUBLER SHOWS CRACK AT STATION XS 515.720. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND Apr 17, 2008 · N602AL · Doug DC873FSDR 08FDEA01437Skin · wornHYDRAULIC LINES IN WING WORN OUT. REPAIR PERFORMED IAW SB 29-6057 (INSTALLATION OF ANTI-ROTATING DEVICES) ON BOTH WINGS, RIB 8-9.Apr 17, 2008 · N730FD · Airbus A300B4622RSDR 08FDEA01436Skin · wornSEVERAL HOLES ELONGATED ON LT WING BOTTOM SKIN AND SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (REAM UP AND BUSHING INSTALLATION) IAW RAS/BAE/1006453/2008 ISS A, APPROVED BY EA 6-2910-115254.Apr 17, 2008 · N730FD · Airbus A300B4622RSDR 2008UALA02237Skin · crackedNR 1 SLAT, OUTBOARD TRACK HAS CRACK ON WING CUTOUT, ABOUT 1.25 INCH LONG. REMOVED 3 RIVETS AND 1 LOCK FASTENER. REMOVED DAMAGE LAID UP REPAIR AND STARTED CURE CYCLE. REF SRM 57-41-01. CURED THEN CLOSED UP. AC OK FOR SERVICE.Apr 16, 2008 · N779UA · Boeing 777222SDR UPS08M52431Doubler · crackedINSPECTION TYPE:C RT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 550 FOUND CRACKED (2522). AFFECTED SKIN DOUBLER ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA & FOUND NO CRACK. THREE EACH A REPAIApr 15, 2008 · N295UP · Doug MD11SDR UPS08M52411Doubler · crackedINSPECTION TYPE:C RIGHT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 556 FOUND CRACKED (2522). RIGHT FIXED WING L/E AFT SKIN DBLR ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDEApr 15, 2008 · N295UP · Doug MD11SDR UIEA200800151Panel · damagedLT WING UPPER SURFACE NR 5 SPOILER CENTER HINGE GAP PANEL DAMAGED, ALSO, INBOARD, OUTBOARD AND CENTER HINGE CUT-OUT AND FORWARD PANEL OF CENTER HINGE DAMAGED, SKIN PULLED AND CRACKED. PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG. 2, SHEETS Apr 15, 2008 · N505MC · Boeing 7472D3BSDR UIEA200800150Panel · delaminatedRT WING UPPER FIXED TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS AN AREA OF 5.0 INCH BY 2.0 INCH OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1, 2 AND 5. PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. REApr 15, 2008 · N505MC · Boeing 7472D3BSDR 08FDEA01411Skin · crackedLT WING, ANTI-ICE TELESCOPE TUBE CUT-OUT AT L/E FIXED COMPARTMENT FOUND OUTBD CORNER CRACKED. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 43 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Apr 15, 2008 · N619FE · Doug MD11FSDR A6WA200840324Skin · crackedRIGHT WING L/E AT WS 185.95 QTY 1 L/E SCREW HOLE IS CRACKED IN THE L/E EXTERIOR SKIN AND EDGING. (M) REPLACED IAW REO 601R-57-41-510. (A)Apr 14, 2008 · N404AW · Cndair CL6002B19SDR DHL2008760511Skin · crackedSTOP DRILLED CRACKED AT RWS 510.0, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 51-10-1, 57-30-4 FIG 10, 51-10-2 FIG 1, 51-30-2, AND B727 NDT PRT 6, 57-00-00 FIG 23.Apr 14, 2008 · N760AT · Boeing 7272B7SDR 08FDEA01408Doubler · crackedRIGHT WING LEADING EDGE SKIN RIB DOUBLER AT STATION XOS 799 FOUND CRACK. REMOVED PER SRM 51-33-01 VOLUME II AND FABRICATED NEW DOUBLER PER DRAWING ARB3954 AND INSTALLED NEW DOUBLER PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Apr 14, 2008 · N525FE · Doug MD11FSDR 08FDEA01398Doubler · crackedRIGHT WING LEADING EDGE SKIN RIB DOUBLER AT STATION XOS 667 FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II AND FABRICATED NEW RIB DOUBLER PER DRAWING ARB3954 AND INSTALLED NEW DOUBLER PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-10Apr 14, 2008 · N525FE · Doug MD11FSDR UPS08M52287Skin · crackedINSPECTION TYPE:C RIGHT WING L/E LWR SURFACE ACCESS PANEL CUTOUT FWD APPROX STA XORS 813 FOUND CRACKED. ATTACH DOOR, FASTENERS & BRACKET REMOVED FROM CRACKED ACCESS PANEL CUTOUT. REPAIR DOUBLER FAB & FASTENER HOLES PICK-UP & PAINTED. REPAIR DOUBLER & ATTACHApr 11, 2008 · N295UP · Doug MD11SDR C2XA08CL048Skin · crackedWING SKIN CRACK ON RIGHT WING AT I/B SPOILER CENTER HINGE CUTOUT. REPAIRED CRACK IAW IC 2008-145/02561. AIRCRAFT RELEASED FOR SERVICE.Apr 11, 2008 · N12934 · Emb EMB145EPSDR MASA200800314Skin · crackedRIGHT WING PLANK IS CRACKED. REPAIRED PLANK.Apr 11, 2008 · N77302 · Cndair CL6002B19SDR UPS08M52410Skin · crackedINSPECTION TYPE:C, LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 538 FOUND CRACKED (2477). LEFT WING NR 4 SLAT CABLE PULLEY REMOVED & L/E FIX WING AFT SKIN FASTENERS REMOVED. INNER SKIN BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CApr 10, 2008 · N295UP · Doug MD11SDR UPS08M52355Skin · crackedINSPECTION TYPE:C LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 522 FOUND CRACKED (2478). ATTACHED RIBS 2 EA REMOVED. INNER SKIN BEADED SKIN TRIM OFF. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. THREE EA REPAIR ANGLES, REPAIR DOUBLERS & FILApr 10, 2008 · N295UP · Doug MD11SDR VNAA0804008Winglet · crackedCREW REPORTED A CRACK IN THE RIGHT HAND WINGLET. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND WINGLET TO BE WITHIN LIMITS IN ACCORDANCE WITH THE CRJ200 STRUCTURAL REPAIR MANUAL. MAINTENANCE APPLIED SPEED TAPE. AIRCRAFT WAS RELEASED FOR SERVICE.Apr 10, 2008 · N259PS · Cndair CL6002B19SDR COMA0860219Skin · crackedLEFT WING PLANK CRACKED ON BOTTOM SIDE JUST O/N OF JACK PAD. PERMANENT REPAIR OF THE LOWER WING PLANK WS 148.019 LEFT IAW REO 601R-57-21-130.Apr 10, 2008 · N958CA · Cndair CL6002B19SDR I5HA0858002Skin · corrodedDURING A ROUTINE MAINT INSP THE UPPER RT OB WING SKIN TE WAS FOUND CORRODED WITH CRACKS COMING AROUND SEVERAL RIVETS. THE RT UPPER OB WING SKIN WAS REMOVED, ALL THE CORROSION WAS REMOVED, THE WING STRUCTURE INSPECTED, AND THE SKIN WAS REPLACED IAW THE SRM.Apr 10, 2008 · N582P · Cvac 440SDR UIEA200800152Skin Panel · crackedLEFT WING LEADING EDGE NOSE CAP UPPER CHORD FOUND CRACK JUST INBOARD OF NR 6 VARIABLE CAMBER FLAP UPPER STOP FITTING. FABRICATED AND REPAIRED DAMAGED AREA IAW SRM 57-20-03.Apr 9, 2008 · N517MC · Boeing 747243BSDR UPS08852020Skin · damagedINSPECTION TYPE:C1 3 SCREWS PULLING THRU SKIN BOTTOM OF RT WING TIP. REMOVED SCREWS, FABBED AND INSTALLED REPAIR DOUBLER. REINSTALLED SCREWS IAW SRM 51-3-0, 57-3-3 FIG 23, 51-1-8,51-1-21A, 51-1-11.Apr 8, 2008 · N803UP · Doug DC873FSDR 08FDEA01346Skin · corrodedCORROSION FINDINGS ON EXISTING REPAIR BETWEEN RIB 7-8, AFT OF REAR SPAR LT WING BOTTOM SKIN REPAIR PERFORMED BY RENEWING DOUBLER REPAIR, BLEND OUT CORROSION IAW RAS/BAE/1006289/2008 ISS A, APPROVED BY EA 6-5720-114855.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01345Skin · damagedANTI-ROTATING DEVICE CAN NOT BE INSTALLED IAW SB 29-6057 ON LT WING HOLE NR 2 AND NR 4. REPAIR PERFORMED BY ADDITIONAL DRILLING HOLE FOR SECOND FASTENER AND CUTTING ANTI ROTATING DEVICE IAW, TA-SEE53-2008-226024-1, APPROVED BY AND EA 6-2910-115253.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01344Skin · wornFOUND ON LT WING ELONGATED HOLES DURING INSPECTION IAW SB 29-6058. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY RAS/BAE/1006287/2008 ISS A AND EA 6-2910-115253.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01343Skin · wornFOUND ON RT WING ELONGATED HOLES DURING INSPECTION IAW SB 29-6058. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH INSTALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY TA-SEE53-2008-226024-1 AND EA 6-2910-115253.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01341Skin · corrodedFOUND ON LT OUTER WING CORROSION ON SKIN INSIDE AROUND HYDRAULIC FITTING HOLES 3 AND 4. REPAIR PERFORMED BY BLEND OUT CORROSION, REPAIR IAW. DRAWING R571-50532 AND INSTALLING A RETAINING PLATE IAW RAS/BAE/1006804/2008 ISS A, APPROVED BY EA 6-5720-117167.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01338Panel · corrodedRIGHT WING FUEL PANEL 635 BT; INTERNAL SURFACE HAS AREAS OF CORROSION. FABRICATED FUEL PANEL P/N IAW DAC DWG ARB 0872-38 AND PART MARKED.Apr 7, 2008 · N365FE · Doug MD1010FSDR ASAA0852831Skin · damagedREF L P 6418789 BIRD STRIKE RIGHT WING REQUIRES REPAIR. BIRD STRIKE RIGHT WING REF TO L P 6418789 REPAIRED IAW B737 800 SRM CH 57 41 01AND BOEING DRAWING 116A4521.Apr 6, 2008 · N577AS · Boeing 737890SDR ASMF200804001Skin · dentedDURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN THE LT WING LEADING EDGE. MAINT PERFORMED A BIRD STRIKE INSPECTION IAW MM 05-51-18 DETECTING A DENT OF 0.562 INCH DEPTH, 11.5 INCH LENGTH AND 3.5 INCH WIDTH AT STATION WS 192, OUT OF LIMITS IAW SRM 57-41-01. Apr 6, 2008 · N997AM · Boeing 73776QSDR UIEA200800138Skin · corrodedRT WING WBL 470 TO WS 917 WING UPPER SKIN FROM FRONT SPAR TO REAR SPAR FOUND CORRODED. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.Apr 4, 2008 · N517MC · Boeing 747243BSDR UIEA200800137Skin · corrodedRT WING WBL 128 TO WS 510 FRONT SPAR TO REAR SPAR UPPER SKIN FOUND CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.Apr 4, 2008 · N517MC · Boeing 747243BSDR UIEA200800129Skin · corrodedLEFT WING FROM WS 150 TO 470 UPPER SKIN CORROSION EVIDENT BETWEEN FRONT SPAR AND MID SPAR. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.Apr 4, 2008 · N517MC · Boeing 747243BSDR UIEA200800125Skin · corrodedLEFT WING FROM WBL 150 TO 470 UPPER SKIN CORROSION EVIDENT BETWEEN NR 1 BEAM TO THE REAR SPAR. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.Apr 4, 2008 · N517MC · Boeing 747243BSDR UIEA200800124Skin · corrodedLEFT WING UPPER SURFACE CORROSION FOUND FROM WS 1120-1540 BETWEEN FRONT SPAR AND REAR SPAR. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02. Apr 4, 2008 · N517MC · Boeing 747243BSDR UIEA200800109Panel · delaminatedLT WING UPPER FIXED LEADING EDGE ON UPPER SURFACE HAS AN AREA OF 30.0 INCHES BY 10.0 INCHES OF DELAMINATION. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09, FIG 18, SHEET 3 AND 5, PREPREG 250 DEGREES F CURE PER SRM 51-40-12. ALSO, REFERENCE ATLASApr 4, 2008 · N523MC · Boeing 7472D7BSDR 08FDEA01312Panel · damagedLEFT WING LOWER SURFACE L/E DROP PANEL (RIB 28) INTERIOR SKIN IS MISSING FOIL. REPAIRED LOWER SURFACE L/E DROP PANEL BY REMOVING DAMAGED FOIL, APPLYING NEW FOIL REPAIR, ALODINED FOIL REPAIR, AND APPLING FR PRIMER IAW SRM 57-41-12, 51-21-00, AND 51-75-10.Apr 4, 2008 · N425FE · Airbus A310203SDR UIEA200800139Panel · corrodedRIGHT WING LEADING EDGE FIXED PANEL AT WS 414 FOUND CORROSION/BULGE AT THE RABBET AREA. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.Apr 3, 2008 · N517MC · Boeing 747243B
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