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 DLM90071396Skin · gougedLT WING FIXED L/E JUST O/B OF SLAT-TRACK NR 4 SKIN IS GOUGED. REPAIRED L/E WING IAW SRM 57-20-01 FIG II VOL II ON N/R 5200-0045 AT HMV-2 IN OKC.SDR UIEA200700465Panel · delaminatedUPPER SURFACE OF LEFT WING INBOARD NR 2 ENGINE FIBERGLASS HAS HOLE AND DENT. REPAIRED PER XEO 57-102607 TRANS TO NON MEL N07-126. REINSPECTED IN ORD AND ACCOMPLISHED XEO 57-102607 PART 3 IAW SRM 51-40-16. REPAIRED AND TO BE INSPECTED EVERY 10 FLIGHT CYCLES SDR DHL2007801504Doubler · crackedLT WING L/E LWR INTERNAL DOUBLER CRACKED 1" STA XFS 335.250. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21. FABRICATED NEW DOUBLER (AL7075T6 0.090") IAW SRM 57-3-3 FIG 5. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IASDR TRAX200701706Panel · damagedPANEL 623GT UPPER SURFACE SCRATCHED AND FLANGE CORRODED. CORROSION REMOVED. FUEL PANEL REPLACED BY NEW.SDR 07FDEA04669Skin · damagedLT WING L/E SKIN LOWER SLAT TRACK CUT OUT NR 8 AT STA XOS 549 EXISTING REPAIR. REPLACED REPAIR PER SRM 57-10-00 VOL.1 FIG 68.SDR DHL2007801506Skin · misrepairedLT WING NR 1 STUB WING EXTERNAL PART SHOWS REPAIR NOT IAW SRM 57-2-1A AT STA XFS 533-375. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.080") AND INTERSDR UIEA200700456Panel · delaminatedRT WING UPPER SURFACE L/E FIXED PANEL AT WING STA 526.0 HAS A 3.0 INCH BY 4.0 INCH AREA OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A400.SDR HNAA0700243Panel · corrodedTHE LEFT HAND WING PANEL 522AT WAS FOUND TO HAVE PITTING DAMAGE FROM CORROSION. REPLACED THE PANEL WITH A NEW PART FROM STORES.SDR 07FDEA04617Skin · crackedRT WING OUTBOARD FLAP CRACK ON EXT SKIN UPPER SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 7 VOL I.SDR 07FDEA04614Skin Panel · corrodedFOUND CORROSION ON TOP SKIN LT WING RIB 25-29 AROUND FASTENER HOLES REPAIR PERFORMED BY BLEND OUT CORROSION, OVERSIZING THE HOLES, FLAP PEENING AND NDT FOR CRACK FREE IAW EA 6-5720-112521 AND RAS/BAE/1005138/2007 ISS A.SDR 07FDEA04613Skin Panel · corrodedFOUND CORROSION ON LT WING TOP SKIN OVER THE WHOLE WING AREA IN AREA OF FASTENER HOLES REPAIR PERFORMED BLEND OUT THE CORROSION, FLAP PEENING AND NDT FOR CRACK FREE IAW EA 6-5720-112521 AND RAS/BAE/1005138/2007 ISS A.SDR S9BA200700022Skin · corrodedRT WING BOTTOM SKIN CORRODED AT BOTTOM IB WING ROOT STATION 47.5. REMOVED AND REPLACED BOTTOM SKIN IB WING ROOT FROM RIB 2 TO RIB 1 IAW RD6-57-164.SDR A6WA200740590Skin · corrodedRIGHT WING LOWER PLANK FUEL ACCESS DOOR CUTOUT 650BB, WS 54.897, HOLE NR 1, HAS PITTING CORROSION ON INBOARD AND OUTBOARD ENDS IN NON-CRITICAL AREA MEASURES APPROX 10.5 INCH LONG BY .25 INCH WIDE BY .009 INCH DEEP AND 5.5 INCH LONG BY .25 INCH WIDED BY .006 INSDR DHL2007801502Skin · corrodedRT WING CTR L/E UPPER SKIN CORRODED, STA XFS 429.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED SSDR 07FDEA04599Skin Panel · corrodedFOUND CORROSION ON RT WING LEADING EDGE BOTTOM SKIN UPPER SURFACE AND RIB NEAR TRACK NR 7. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND OVERSIZING THE HOLES IAW EA 6-5741-106528 AND RAS BAE/1005113/2007 ISS A.SDR 07FDEA04598Skin Panel · corrodedFOUND CORROSION ON RT WING LEADING EDGE BOTTOM SKIN UPPER SURFACE AND RIB NEAR TRACK NR 5-7 REPAIR PERFORMED BY BLEND OUT THE CORROSION AND OVERSIZING THE HOLES IAW EA 6-5741-106528 AND RAS BAE/1005113/2007 ISS A.SDR 07FDEA04597Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 4-5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04596Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04595Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 5, AROUND SEVERAL HOLES. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04594Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 11 REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04593Skin Panel · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 8. REPAIR PERFORMED BY BLEND OUT CORROSION, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04592Skin · corrodedFOUND CORROSION ON LT WING BOTTOM SKIN LOWER SURFACE RIB 1-2, P4-6 REPAIR PERFORMED BY BLEND OUT CORROSION, REPAIR IAW SB 57-6047, APPROVED BY EA 6-5720-112530 AND RAS/BAE/1005161/2007 ISS A.SDR 07FDEA04587Skin · misrepairedFOUND OLD REPAIR ON RT INNER DEFLECTOR DOOR 672CB NOT CONFORM TO SRM REPAIR RENEWED IAW SRM 51-77-12 PARA 3C WITH DEVIATIONS, APPROVED BY EA 6-5755-114909 AND RAS/BAE/1005629/2007.SDR UALA2008111304215Skin · damagedFUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LT MAIN GEAR, FROM UPPER REAR SPAR CORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES IN UPPER SKIN. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES IN UPPER SKIN. EG APPROVAL TO USE LG DSDR A6WA200740588Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT 510AB, WS 12.245, HOLE NR 2 HAS PITTING CORROSION AT INBOARD AND OUTBOARD ENDS IN NON-CRITICAL AREA MEASURES APPROX 9.5 INCH LONG BY .25 INCH WIDE BY .005 INCH DEEP AND 3.5 INCH LONG BY .20 INCH WIDE BY .007 INCSDR A6WA200740587Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT 540BB, WS 54.897, HOLE NR 1, HAS PITTING CORROSION AT INBOARD AND OUTBOARD ENDS IN NON-CRITICAL AREA. MEASURES APPROX .3 INCH LONG BY .20 INCH WIDE BY .005 INCH DEEP EACH. MAINTENANCE REPAIRED IAW AWAC EO E06/SDR UIEA200700442Skin · crackedDURING LEFT WING LIGHT REPLACEMENT THE PLATFORM SUDDENLY LOWERED AND HIT THE LEADING EDGE SKIN. THE PLATFORM MOVEMENT CAUSED A 15 INCH VERTICAL CRACK. A TIME LIMITED REPAIR WAS ACCOMPLISHED AS PER XEO 57-101007 PART 1 AND SRM 57-41-01 REPAIR 4. PERMANENT REPSDR S9BA200700019Skin · corroded"OPEN" LT WING IB PLANK DOUBLER (STATION 30) CORRODED AT LEADING EDGE.SDR S9BA200700020Skin · corroded"OPEN" RT WING BOTTOM SKIN CORRODED OB OF NACELLE AT STATION 147.SDR WRLA2007106Skin · corrodedDURING 4C+12A CHECK, SEVERAL CORROSION AREAS WERE FOUND ON CENTER WING TANK UPPER SKIN AT XCW=-110 TO XCW=-106 BETWEEN S-15 TO S-22 AND STA XCW=107 BETWEEN S-18 TO S-15. 10-29-07 REPAIRED PER EGAT ENGINEERING INSTRUCTION W2007A57B-638 REV.00.SDR UIEA200700434Panel · damagedDAMAGE TO THE RT FIXED UPPER WING TRAILING EDGE PANEL WBL 235 ALONG THE TRAILING EDGE 7" FROM THE OUTBD END 1"IN LENGTH BY 1/4" WIDE .SDR 07FDEA04532Skin · crackedRIGHT WING LEADING EDGE SLAT NR 6 OUTBOARD SLAT TRACK CUTOUT, SLAT TRACK NR 14, FOUND CRACK AT CORNER EDGE. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA04531Skin · crackedRIGHT WING LEADING EDGE SLAT NR 6 INBOARD SLAT TRACK CUTOUT (SLAT TRACK NR 12), FOUND CRACK AT CORNER EDGE. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 .SDR 07FDEA04530Skin · crackedCRACK INDICATIONS REVEALED FASTENER HOLES AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT EDGE. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115214, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA04529Skin · crackedCRACK INDICATIONS REVEALED FASTENER HOLES AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT EDGE. 10-24-07 REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-115213. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA04526Skin · crackedLEFT WING, NR 5 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT LOWER EDGE FOUND CRACK. 10-24-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR UPS07851069Doubler · puncturedINSPECTION TYPE:C2 REPAIR DOUBLER PUNCTURED ON WING SKIN PANEL BOTTOM SURFACE, IN LT WHEEL WELL NEAR UPLATCH. REMOVED AND REPLACED REPAIR DOUBLER ON WING SKIN PANEL IN LT WHEEL WELL IAW SRM 51-3-00, AND SRM 57-03-00-0.SDR 07FDEA04517Skin Panel · corrodedFOUND ON LT OUTER WING ON MANHOLE FLANGE RIB 23-24 CORROSION. REPAIR PERFORMED BLEND OUT CORROSION IAW SRM 57-20-12 PARA 4 A, NDT FOR CRACK FREE IAW EA 6-5720-106525 AND RAS//BAE/1005053/2007 ISS A.SDR 07FDEA04516Skin Panel · damagedFOUND OLD REPAIR ON RT OUTER WING AT FASTENER HOLE 939, RIB 9-10 IN BAD CONDITION. REPAIR PERFORMED BY OVERSIZING THE HOLE AND INSTALLING NEW TAPER OK IAW EA 6-5720-106520 AND RAS/BAE/0564/2003 ISS B.SDR 07FDEA04515Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 20-21. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005302/2007 ISS A.SDR 07FDEA04514Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 13-14. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005302/2007 ISS A.SDR 07FDEA04513Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 10-12, FWD OF FRONT SPAR. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005247/2007 ISS A.SDR 07FDEA04510Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 11-12, P15-16. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005301/2007 ISS A.SDR 07FDEA04503Skin Panel · corrodedFOUND CORROSION AT RT WING BOTTOM SKIN IN THE AREA OF RIB 5. REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING AND INSTALLATION OF NEW FASTENER IAW EA 6-5720-112520 AND RAS/BAE/1005222/2007 ISS A.SDR 07FDEA04502Skin Panel · corrodedFOUND CORROSION AT RT WING BOTTOM SKIN IN THE AREA OF RIB 5 REPAIR PERFORMED BY BLEND OUT CORROSION, FLAP PEENING AND INSTALLATION OF NEW FASTENER IAW EA 6-5720-112520 AND RAS/BAE/1005222/2007 ISS A.SDR 07FDEA04501Skin · corrodedFOUND CORROSION ON AFT RUN OUT OF TOP SKIN PANEL NR 2, RT WING WITH ADDITIONAL CRACK FINDING AFTER CORROSION REMOVAL REPAIR PERFORMED BY CUT OUT THE DAMAGE AND INSTALLING A REPAIR DOUBLER IAW EA 6-5720-106529 AND RAS/BAE/1005083/2007 ISS A.SDR 07FDEA04495Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 8-9 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007.SDR 07FDEA04494Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 18-19 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007.SDR 07FDEA04493Skin · corrodedFOUND CORROSION AT LT WING BOTTOM SKIN BETWEEN 8-10 AND 18-19 FWD OF FRONT SPAR REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTING IAW EA 6-5720-112535 AND RAS/BAE/1005212/2007.SDR WRLA2007102Skin · crackedDURING 4C + 12A CHECK FOUND RIGHT WING FIXED L/E SKIN CRACK AT CORNERS OF CUTOUT L=0.3 INCH, AT STA XOS 464 L=0.5 INCH STA XOS 470. 10-25-07 REPAIRED THE RT WING FIXED LEADING EDGE SKIN CRACK AT CORNERS OF CUTOUT AT STA XOS=464,470 PER MD11 SRM VOL.I 57-
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