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 ZW0A0210804Skin · dentedDURING CHECK-C MAINT THE LT WING FIXED LE 15 INCHES AND 19 INCHES OTBD FROM 0 SLAT OTBD TRACK, FOUND DENT IN LE. INSTALLED REPAIR PER SRM 57-06B, FIG 14.SDR ASAA0280413Doubler · crackedOKC - FOUND DURING 30K CHECK, LEFT WING LEADING EDGE BUTT SPLICE DOUBLER IS CRACKED 1.25 INCH AT LOWER AFT EDGE. REPLACED SPLICE PER SRM 57-32-1, 51-10-4, AND 51-30-2. (M)SDR ASAA0280403Skin · crackedOKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE CRACKED .5 INCH ON RIB AT FASTENER HOLES AT WING STATION XRS 69. STOP DRILLED, REMOVED DAMAGE, AND INSTALLED DOUBLER AND SHIM PER SRM 51-10-3. (M)SDR DHL2002362509Skin · corrodedR/H WING BOTTOM SKIN BETWEEN RIB 7 AND 8 AND, FRONT AND CENTER SPAR, SEVERAL AREAS WITH CORROSION.REMOVED CORROSION JUST OUT BOARD OF CENTER SPAR FOUND NTO BE OUT OF LIMITS. REPAIRED BY BLENDING OUT CORROSION, ENSURING AREA WAS CRACK AND CORROSION FREE BY HFECSDR 02FDEA00742Skin · corrodedLT WING T/E SKIN CRACKED AT 581AB ACCESS CUTOUT AT RIB 11. R&R SKIN PER EA 6-5710-65463.SDR UPS02839817Skin · corrodedINSPECTION TYPE:C-2 LT WING LOWER WING SKIN, O/B OF FUEL VENT PANEL, FWD OF REAR SPAR, IS CORRODED ON EXTERIOR SURFACE. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER IAW REO G08852 AND DC8 SRM 57-2-0 FIG 2A, AND INSTALLED DOUBLER REPAIR IAW REO G08852 AND DC8SDR DHL2002720530Skin · corrodedDURING C CHECK, LT WING UPPER SURFACE STRAP BULGED ABOVE FRONT SPAR AFT. OF NR 3 SLAT. REPAIRED IAW SRM.SDR UPS02839831Skin · crackedINSPECTION TYPE:C2 RIGHT WING CENTER L/E LOWER SKIN IS CRACKED AT FASTENER HOLE AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B.SDR UPS02839827Skin · crackedINSPECTION TYPE:C2 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-1 FIG 10.SDR UPS02839826Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 75 AT STRINGER 9. CUTOUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 10.SDR CALA0200493Skin · crackedINSPECTION FOUND AN 8" CRACK IN R/H WING FIXED L/E SKIN PANEL ABOVE #4 SLAT ACTUATOR. THE SKIN PANEL WAS REMOVED AND REPLACED IAW ECRA 5720-01894.SDR AWXA200201076Skin · delaminatedDURING C-08 CHECK REPAIR OF DELAMINATED AREA OF LT WING LEADING EDGE REQUIRED TO TERMINATE MONITOR. WS 106 TO WS 169 LT. MAINTENANCE REMOVED PREVIOUS REPAIR AND CUTOUT A 11 X 6.5 INCH DELAMINATED AREA OF LT INBOARD FIXED WING LEADING EDGE AT WS 106 TO WS 169; SDR DHL2002362501Skin · corrodedRT WING BOTTOM SKIN BETWEEN RIB 1 & 2, CENTER AND AFT SPAR, CORROSION FOUND. REMOVED CORROSION IAW A300 SRM 51-40-11, NDT AREA IAW NTM 51-31-05, NO CRACKS FOUND, THICKNESS CHECKED AREA PER NTM 51-20-00, 5 PERCENT LOSS OF MATERIAL, AREA FOUND TO BE IN LIMITS ISDR AUS20021138Panel · separated(AUS) LT MAIN LANDING GEAR SUPPORT AFT LOWER ACCESS PANEL MISSING.SDR QXEA0201670Skin · damagedPDX - LT WING UPPER SKIN HAS 1/2 X 1/4 INCH SCUFF DAMAGE NEXT TO FORWARD EDGE OF APERTURE FOR PANEL 522AT. REPAIRED IAW DHC-8 SRM 57-10-11 AMD SR, 51-20-11.SDR F3LA200200346Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED LT WING FIXED LE CRACKED ON INBD SIDE OF NR 2 SLAT, INBD AUX TRACK CUTOUT. REPAIRED CRACK PER SRM 57-20-L1 AND MM 51-21-021.SDR UPS02839621Skin · crackedLT WING DOUBLER SKIN CRACKED, FERRIED TO VENDOR AQUAMISED, NR 2 MAIN TANK 5788, INSTALLED DOUBLER & TRIPLER PER EO DC8-2810-6720I. H FEC INSPECTION PER NDT SPM 06-10-01.00 OF THE LT WING REAR SPAR LOWER ROOT DID NOT DETECT ANY CRACKS. VISUALLY INSPECTED SDR 02FDEA00697Skin · damagedAFT PYLON HYD TUBES FITTING HOLES ON RIGHT WING UNDER SURFACE SKIN FOUND ELONGATED AFT OF PYLON RIB 21. R&R WING LWR SKIN PER EA 6-5710-65098.SDR 02FDEA00694Skin Panel · crackedLEFT WING LWR SKIN PANEL NR 2 FOUND WITH EDGE CRACK JUST OUTBOARD OF RIB 11, CRACKED 1 INCH. R&R WING LWR SKIN PANEL NR 2 PER EA 6-5710-65099.SDR CA021001008Panel · corroded(CAN) FWD OUTBOARD CORNER OF BONDED DOUBLER. PANEL WAS BEING REPLACED DO TO OIL CANNING FROM DATE OF MANUFACTURE WHEN THE CORROSION WAS FOUND AT THE FWD OUTBOARD CORNER WHERE THE PANEL CONTACTS A MONEL DOUBLER SPLICE PLATE. THIS IS NOT AN AREA THAT CAN BE INSSDR SWIA200211277Skin · dentedRIGHT WING LEADING EDGE BETWEEN WS 85.5 AND WS 96.13 IS DENTED AND OIL CANNING ON LOWER SIDE OF LEADING EDGE. REPLACED INBOARD RIGHT LEADING EDGE IAW MM 57-41-01.SDR F3LA200200273Skin · gougedDURING C-4 CHECK, INSPECTION REPORTED RT WING LEADING EDGE AT INBD END OF NR 5 SLAT GOUGED. REPAIRED DAMAGE PER SRM 51-70-17, FIGURE 19.SDR QXEA0201700Panel · gougedPDX - LT WING TOP PANEL 532AT APERTURE FLANGE GOUGED. REPAIRED IAW DHC-8 SRM 51-20-36.SDR UPS02839793Skin · crackedINSPECTION TYPE: C2, LT WING UPPER SKIN IS CRACKED AT XRS AT STRINGER 9 CUTOUT CRACKED AREA,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM. 57-2-1 FIG. 10SDR AALA20021400Skin · crackedTUL - FOUND NR 8 SLAT TRACK AREA, TOP OF LEADING EDGE HAS CRACK TO SKIN, XRS 256. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 57-30-00-8. (M)SDR AALA20021351Skin · corrodedFOUND BOTTOM SKIN (WING) CORRODED TOP SURFACE JUST INBOARD OF NR 5 JACKSCREW. FLAP PEENED BLENDED AREA PER SRM 51-29-00-2 ALODINED AND PRIMED PER ESO 30595 DATED 9-23-2002. (M)SDR UPS02439728Skin · corrodedINSPECTION TYPE:C LHW LWR SKIN SURFACE CORROSION IS FOUND AT FUEL TANK ACCESS DR 522BB CUTOUT. CORROSION BLEND OUT 0.06"X0.5"X8"EXCEED SRM LIMIT 57-30-03. CORROSION REMOVED REFER SOPM 20-20-02.SDR 16138CSkin · crackedLOWER CENTER WING SKIN CRACKED AT FASTINER HOLES.SDR 200200279Skin Panel · corrodedRIGHT WING - CORROSION REPAIR AT FORWARD EDGE OF LOWER FORWARD SKIN PANEL, WS 1390-1498. THE CORROSION WAS IN THE UPPER SURFACE OF THE SUBJECT SKIN, AND IN THE LOWER SURFACE OF THE RT WING FORWARD SPAR LOWER CHORD. THE CORROSION WAS REMOVED BY BLENDING PER BSDR AUS20021045Skin · corroded(AUS) RT WING UPPER SURFACE CORRODED IN AREA LOCATED FORWARD OF THE FILLER CAP AT APPROXIMATELY WING STN 440. AN AREA OF 6.35MM (0.250IN) BY 25.4MM (1IN) WAS REMOVED AT THE FORWARD EDGE OF THE FILLER CAP HOUSING.SDR CALA0200463Doubler · crackedINSPECTION FOUND A 2" CRACK IN R/H WING UPPER I/B T/E PANEL DOUBLER, WBL 80. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-70-11.SDR 2002F00931Panel · looseVIBRATION FELT AND AIRSPEED STARTED TO DECREASE. FLIGHT RETURNED TO THE AIRPORT. UPON ARRIVAL A WALK-AROUND INSPECTION REVEALED THAT THE FORWARD WING BOX PANEL WAS LOOSE, NOT FLUSH. REPLACED FORWARD WING BOX PANEL. (M)SDR DHL2002873502Skin · crackedLT WING L/E LOWER OUTER SKIN CRACKED .500, STA XW761. PERFORMED MAJOR REPAIR IAW EO DHL 020904, ED-3124, EO SEMAN 2002737. TRIMMED OUT DAMAGED OUTER SKIN IAW EO DHL020904, ED-3214, EO SEMAN 2002737. FABRICATED A REPAIR DOUBLER AND FILLER IAW ED DHL 020904, SDR 02FDEA00640Skin · crackedRIGHT WING OUTER LWR SKIN PANEL NR 2 AT TRAILING EDGE OF RIB 2 CRACK. R&R WING LWR SKIN PANEL NR 2 PER EA 6-5710-65100.SDR AUS20020997Doubler · cracked(AUS) WING WALK SKIN CORRUGATED DOUBLER CRACKED IN AREA NEAR RIB AT STN36.9.SDR AUS20020996Skin · corroded(AUS) RH WING LOWER SKIN CONTAINED THREE CORROSION HOLES INTO THE TANK. AFT STRINGER CONTAINED EXFOLIATION CORROSION IN THE SAME LOCATION AS ONE OF THE HOLES.SDR C2XA02TY136Skin · gougedTYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND LEADING EDGE NR 2. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 2649/02 AND EMB145 AMM 57-41-00. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ISDR C2XA02TY135Skin · gougedTYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND NR 1 LEADING EDGE. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB GST 2512/02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELEASED UPON COMPLETION OF INSPECTION.SDR UPS02839359Tripler · crackedINSPECTION TYPE:C1 LEFT WING CENTER L/E LOWER INTERNAL TRIPLER IS CRACKED AT STA XOLDI 6.225. REMOVED INTERNAL DOUBLER AND TRIPLER AT WING STA XOLDI 6.225 IAW SRM 51-1-21, FABRICATED REPAIR DOUBLER AND TRIPLER IAW DC8 DRAWING 5769589. INSTALLED REPAIR DOUBLESDR GAIA02087STPlenum · corrodedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT PLENUM LOWER SKIN HAS CORROSION IN TWO PLACES. FOUND CORROSION OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW B727 SRM 57-30-3 FIGURE 8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR AUS20020973Seal · leaking(AUS) RT WING ACCESS PANEL LOCATED INBOARD OF THE NR 3 NACELLE LEAKING FUEL DUE TO A FAULTY SEALING RING.SDR UPS02839515Doubler · crackedINSPECTION TYPE:C1 LEFT WING CENTER L/E INTERNAL CIRCUMFERENCE DOUBLER IS CRACKED ON LOWER SECTION AT XFS 348. CUTOUT CRACKED SECTION OF INTERNAL DOUBLER, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER SECTION AND SPLICE IAW UPS ENGINEERINSDR QXEA0201306Skin · deterioratedPDX - LEFT HAND WING TOP WING BOX SKIN AFT SURFACE COMPOSITE IS SOFT AND HAS PAINT MISSING AT STATION YW410.000. REPAIRED IAW HORIZON AIR EA 2-57-187.SDR 2002FA0001104Panel · delaminatedHONEYCOMB SIDEPANELS HAVE BECOME DELAMINATED IN NUMEROUS AREAS, EVEN IN THE AREA THAT THE CARRY THROUGH SPAR IS BOLTED TO. THE DELAMINATION OF THE HONEYCOMB PANELS IN THIS AREA REDUCE THE STRUCTURAL INTEGRITY AND MAY ALLOW POSSIBLE SPAR SLIPPAGE AFFECTING THESDR QXEA0201319Skin · scratchedPDX - SCRATCHES ON MATTING UPPER SURFACE FOR LEADING EDGE AT STATION YW178.00 ON RIGHT HAND WING. REPAIRED IAW DHC-8-200 SRM 51-20-36.SDR CA021002013Skin · cracked(CAN) ON INSPECTION IT WAS NOTICED THAT WHERE THE RT MAIN GEAR PUSHES TO THE UP POSITION, THE RIB HOLDING THE WHEEL STOP WAS CRACKED AND THE WING SKIN HOLDING THE RIB WAS ALSO CRACKED FROM THE MANY CYCLES.SDR UPS02839325Skin · crackedINSPECTION TYPE:C1 LT WING L/E LOWER SKIN IS CRACKED AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087 APPROX C.SDR AALA20021607Skin · crackedTUL - FOUND 5 INCH CRACK IN LEFT WING LOWER FIXED LEADING EDGE AT WING STATION 214. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER/ AND STRAP AARD 80559, CHECK OK. (M)SDR UPS02839362Doubler · crackedINSPECTION TYPE:C1 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.SDR CA020904010Skin · cracked(CAN) WINGS REMOVED FOR INSPECTION AFTER HARD LANDING WITH RT WING REMOVED FORWARD AND AFT WING WALKS UNDER UPPER WING SKINS INSPECTED AND CRACKS FOUND AT END RADIUS OF STAMPED STIFFENER SECTIONS.
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