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 IPXA11M64583Doubler · crackedINSPECTION TYPE:1C, LT WING L/E COMPARTMENT CEILING HAS CRACKS AT FASTNER, 22" OTBD OF NR11 SLAT TRACK XOS 679. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-10-02, REPAIR 9, FIG. 203SDR IPXA11M64582Doubler · crackedINSPECTION TYPE:1C, LT WING L/E COMP CEILING HAS CRACKS AT 2 EA FASTNERS 17" INBD OF NR11 SLAT TRACK, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR IPXA11M64581Doubler · crackedINSP TYPE:1C, LT WING L/E COMP CEILING HAS CRACKS AT FASTENERS 43" OTBD OF NR11 SLAT TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR IPXA1M64476Doubler · crackedINSPECTION TYPE:1C, LT WING L/E COMP CEILING HAS CRACKS ON DOUBLER, 10" OTBD OF NR9 SLAT TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02 REPAIR 9, FIG 203.SDR IPXA1M64475Doubler · crackedINSPECTION TYPE:1C, LT WING L/E COMP CEILING HAS CRACKS ON DOUBLER, 23" OTBD OF NR9 SLAT TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02 REPAIR 9, FIG 203.SDR IXXA11SMN008SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 385.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPSDR IXXA11SMN007SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 347.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPSDR IXXA11SMN006SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 341.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPSDR IXXA11SMN004SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING UPPER SKIN CORRODED AT STATION XRS 811.000 STRINGER 3 TO STRINGER 4. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRSDR IXXA11SMN002SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING UPPER SKIN CORRODED AT STATION XRS 763.000 STRINGER 2-4. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SDR IXXA11SMN003SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING UPPER SKIN CORRODED AT STATION XRS 795.000 STRINGER 3-5. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SDR IXXA11SMN010SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING CTR L/E UPPER PANEL CORRODED AT STA XW 408.000. REMOVED CORRION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND RSDR IXXA11SMN009SDoubler · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING CTR L/E UPPER SURFACE DOUBLER CORRODED AT STA XFS 423.000 - XFS 400.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED DOUBLER. FABRICATED DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALSDR IXXA11SMN005SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING UPPER SKIN CRACKED AND CORRODED AT STA XRS -17.000 STR-9. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FSDR A6WA201140051Skin · damagedLT WING CTR L/E HAS 1 EA UNSERVICEABLE COUNTERSINK ON LWR SIDE BETWEEN WS 203.23 & WS 212.81. REPAIRED IAW REO 601R-57-41-740.SDR IXXA11009SSkin · crackedDURING ROUTINE B-CHECK INSP FOR ACCOMPLISHING AD 2008-26-07 FOUND LT WING LOWER SKIN CRACKED AT STA XW408.343, STRINGER 60. MX PERFORMED FERRY FLIGHT INSP IAW GMM 3.117, FOR THE REPAIR.SDR REXA201100045Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB AND NR 11 FOR 550CB HAVE CORROSION AT INBOARD AND OUTBOARD ENDS NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB AND NR 11 FOR 550CB AT INBOARD RADII IN THE NONCRITICAL REGIONSSDR IXXA110003SSkin · crackedDURING SKIN INSP FOR AD 2008-26-07, FOUND A .5 INCH CRACK ON LT WING LOWER SKIN AT STRINGER 58. MX PERFORMED INSP FOR FERRY FLIGHT FOR PERMANENT STORAGE IAW GMM 3.117.SDR R61A20110009Skin Panel · crackedWHILE THE AIRCRAFT WAS IN FOR HEAVY CHECK LOWER LEFT WING HAS 1/32 INCH CRACK AFT EDGE INBOARD OF RIB 25. LOWER SKIN HAS 2MM GOUGE DEPTH, MEASURING 1.0 X .75 INCH AND DENTED SKIN AFT OF PANEL 541DB 3 TO 4 MM DEEP MEASURING 4.0 X 1.5 INCH. CUTOUT DAMAGED AREASDR FDEA201101140173Skin · crackedDURING HFEC OPEN HOLE INSP, CRACK INDICATION FOUND AT LT WING LOWER SKIN PANEL INBD OF RIB 9, AFT OF REAR SPAR HOLE (G) 1 EA ON LOWER SKIN SIDE. REPAIR CARRIED OUT PER EA NR 6-5710-143824. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR GLBA20110113FSkin · leakingMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE LT WING L/E PATCH AT WS 194.85 TO WS 214.35 LEAKING FUEL AT SEVERAL RIVETS AND SEEMS (UPPER & LWR). SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERSDR FDEA201101130129Skin · crackedRT WING LOWER SKIN PANEL INBD OF RIB 9 JUST INBD OF STIFFENER, FOUND WITH SUPPORT CRACK. REPAIR CARRIED OUT AS PER EA NR 6-5710-143821. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR C2XA11SH020Skin · crackedSHV - DURING C-CHECK LT WING SKIN HAS CRACK JUST FWD OF GROUND SPOILER CTR HINGE POINT. REPAIRED SKIN IAW EC5740-01276. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA201101120106Skin · crackedCRACK FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON RT WING LOWER BOTTOM SKIN PANEL INBD OF RIB NR 9. REPAIR CARRIED OUT PER EA NR 6-5710-143821. THIS REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 111.SDR R61A20110001Skin · crackedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED RT WING SPAR 2 RIB 10 SKIN CRACKED AT I/B MOST SCREW HOLE. MAINTENANCE PERFORMED MAJOR REPAIR OF SPAR 2 RIB 10 SKIN CRACK IAW ETD 2011-170-00322. PARTS FABRICATED REF PO 220470 MATERIAL USED 2024-T3SDR IPXA11M64395Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPARTMENT, THRU ACCESS PANEL 619EB, BEADED DOUBLER FOUND CRACKED AT 2 LOCATIONS AS MARKED XOS 643.5-647. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR UALA2011011000147Skin · crackedLARGE CRACK IN RIGHT WING FIXED LEADING EDGE UPPER SKIN PANEL JUST INBOARD OF NR 3 ENG. ACCOMPLISHED 250 DEG. PREP REG REPAIR AND APPLIED NON CHROMATED COMPOSITE PRIMER. NEEDS TOP COATED.SDR UALA2011011000145Skin · damagedEVIDENCE OF LEFT WING TIP SCRAPE ON UPPER TOP SURFACE AFTER TOW INTO GATE ON AIRCRAFT ARRIVAL. WINGLET TIP SCRAPE LENGTH 34 INCH. MAIN GOUGE AREA IS 2 INCH LONG, STARTING 3'5 INCH FROM AFT TIP EDGE, DEEPEST GOUGE DEPTH IS 0'118 INCH. AFT TIP CURL IS 0'551 ISDR FDEA201101070070Skin · crackedLT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, FOUND 03 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6SDR FDEA201101070069Skin · crackedRT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, FASTENER HOLES 12 EA. FOUND CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2SDR REXA201100029Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB HAS CORROSION AT INBOARD AND OUTBOARD END NOT IN CRITICAL REGION. REPAIRED LEFT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB AT INBOARD AND OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 RSDR REXA201100028Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE NR 3 FOR 510BB HAS CORROSION AT OUTBOARD END NOT IN CRITICAL REGION. REPAIRED LEFT WING LOWER PLANK ACCESS HOLE NR 3 FOR 510BB AT OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR REXA201100027Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE NR 2 FOR 510AB HAS CORROSION AT FORWARD SIDE AND OUTBOARD END IN AND OUT OF CRITICAL REGION. REPAIRED LEFT WING LOWER PLANK ACCESS HOLE NR 2 FOR 510AB AT FORWARD SIDE AND OUTBOARD END IN AND OUT OF CRITICAL REGION IAW BOMBARDSDR REXA201100026Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE NR 2 FOR 610AB HAS CORROSION AT INBOARD END NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 640BB AT OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR REXA201100025Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 640BB HAS CORROSION AT OUTBOARD END NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 640BB AT OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR REXA201100024Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE NR 4 FOR 640AB HAS CORROSION AT INBOARD AND OUTBOARD ENDS NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 4 FOR 640AB AT INBOARD AND OUTBOARD ENDS NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-0SDR REXA201100023Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLE NR 6 FOR 640DB HAS CORROSION AT INBOARD END NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 6 FOR 640DB AT INBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.SDR IPXA12M71091Doubler · crackedINSPECTION TYPE:3C, RT WING FIXED L/E COMPT INBD OF SLAT TRACK NR 10 BEADED DOUBLER CRACKED. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS648-653 IAW EO MD11-5730-42916-B AND SRM 57-40-02 REPAIR 9, FIG 203.SDR IPXA12M71090Doubler · crackedINSPECTION TYPE:3C, RT WING FIXED L/E COMPT INBD OF SLAT TRACK NR 11 BEADED DOUBLER CRACKED 3 PLACES. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS692-708 IAW EO MD11-5730-42916-B AND SRM 57-40-02, REPAIR 9, FIG 203.SDR U2RA449SPIM001Skin · wornLT WING, T/E UPPER SURFACE, XRS 272 EXISTING REPAIR WITH WEAR.SDR DALA1112929222Rub Strip · corrodedHMV2 UPPER FUEL PANEL CUT OUT NR 520 FT HAS SURFACE CORROSION ON EXTERIOR RIM. REPLACED RUB STRIP PER 57-10-05.SDR GUUA95657010311ASkin · damagedDURING SCHEDULE ROUTINE INSP, DISCOVERED A HOLE APPROX 0.032 IN IN DIAMETER ON THE RT WING UPPER SKIN T/E. INSTALLED CR3213-4-1 RIVET IN THE HOLE.SDR GUUA95257010311ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STA 138.00 AND 160.25. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR USAA2011010390008Skin · corrodedCLT - RON - MAJOR REPAIR - SEVERAL AREAS OF CORROSION ON RIGHT WING SKIN UPPER SURFACE INBOARD OF WBL 114, S2. REPAIRED RIGHT WING SKIN UPPER SURFACE INBOARD OF WBL 114, S2 IAW EA 102499.SDR ASAA1148984Skin · gougedRT WING L/E GOUGED AT APPROX WS 178. REPAIRED LEADING EDGE IAW B737 400 SRM 57 41 01 FIG 101.SDR VNAA2010123100021Skin · damagedDURING SCHEDULED MAINTENANCE A LEFT WING LOWER PLANK HOLE HAD LEVEL 1 CORROSION. REPAIRS WERE MADE USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR QXEA2011010400963Access Panel · damagedC2 CHECK - LT WING FUEL ACCESS PANEL, 524AT HAS AREAS OF FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-442.SDR QXEA2011010400962Access Panel · corrodedC2 CHECK - LT WING FUEL ACCESS PANEL 524BT HAS AREAS OF CORROSION AND MINOR FRETTING. REMOVED DAMAGE IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-44SDR QXEA2011010300954Access Panel · damagedC2 CHECK - LT WING FUEL ACCESS MOUNT FLANGE HAS AREAS OF FRETTING. REMOVED DAMAGE FROM MOUNT FLANGE IAW RD 8/4-57-445. FOUND FLANGE TO BE WITHIN LIMITS. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-02-01. COMPLIED WITH RD 8/4-57-445.SDR QXEA2011010300953Access Panel · corrodedC2 CHECK - LT WING FUEL ACCESS PANEL 524BT MOUNT FLANGE HAS AREAS OF CORROSION AND MINOR FRETTING. REMOVED DAMAGE FROM ACCESS PANEL 524BT IAW RD 8/4-57-445. FOUND DAMAGE TO BE WITHIN LIMITS. RESTORED SURFACE PROTECTION IAW SRM 51-21-10-02-01 AND 51-25-40-0
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