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 UPS05845451Skin · corrodedLEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 785.000. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8,51-1-21 AND EO DC8-5720-7767-A.SDR UPS05845449Doubler · crackedINSPECTION TYPE:C3 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.250. REMOVED INTERNAL DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-3-0, 51-1-20D AND 51-1-21.SDR UPS05845418Skin · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN HAS A DAMAGED FASTENER HOLE AT XFS 347.750. FABRICATED AND INSTALLED DOUBLER IAW 57-03-03 FIG 005 PG 1,EO DC8-572 0-7767-A AND SRM 51-1-21.SDR MALA050703Skin · gougedWHILE ACCOMPLISHING F1.E INSPECTION FOUND A GOUGE ON THE RIGHT WING LOWER SKIN AFT OF THE AFT SPAR AT RIB 1. IT APPEARS THAT THE DAMAGE WAS CAUSED BY PANEL 284BR.SDR UPS05845498Skin · crackedINSPECTION TYPE:C3 LT UPPER WING NR 2 MAIN TANK ACCESS PANEL 505F UNDER LANDING HAS 1" LONG POSSIBLE CRACK. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 36.SDR A6WA200540296Skin · corrodedLEFT WING LOWER WING FUEL TANK ACCESS DOOR CUTOUT FOR 510AB HAS CORROSION LESS THAN .004 INC DEEP IN SEVERAL AREAS. MAINTENANCE REMOVED CORROSION, PERFORMED NDT ROTO-PEENED AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV D. (M)SDR A6WA200540295Skin · corrodedRIGHT WING LOWER WING FUEL TANK ACCESS DOOR CUTOUT FOR 650 OUTBOARD HAS PITTING CORROSION LESS THAN .003. MAINTENANCE REMOVED CORROSION, PERFORMED NDT, ROTO-PEENED AND APPLIED SURFACE TREATMENT IAW REO 601R-57-27-030 REV D. (M)SDR UPS05845497Skin · crackedINSPECTION TYPE: C3, RT UPPER WING SKIN CRACKED AT XCW 69.500 REAR SPAR SKIN, (4 INCHES LONG CRACK). REMOVED DAMAGED SECTION OF SKIN, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 20.SDR UPS05845398Skin · corrodedINSPECTION TYPE:C3 LT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION UNDER REPAIR DOUBLER AT XFS 410.250. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.SDR UPS05845348Skin · corrodedLT WING LE HAS INTERGRANULAR CORROSION IN SKIN AT XW 257. SKIN IS SPLIT T ALONG EDGE. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.SDR YENA200558Access Panel · looseON CLIMBOUT THRU FL220 FELT SIGNIFICANT VIBRATION IN FRONT PART OF AIRCRAFT IN BOTH PILOTS SEATS AND RUDDER PEDALS, REDUCED POWER AND LEVELED OFF AND STILL FELT SAME VIBRATION. ALL ENGINE INDICATIONS NORMAL. PERFORMED PROCESS OF TSM TASK 05-50-00-810-801. NSDR UPS05845412Skin · crackedINSPECTION TYPE: C3, RT WING L/E UPPER SKIN IS CRACKED O/B OF XFS 710.000. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845396Skin · crackedINSPECTION TYPE:C3 RIGHT WING L/E UPPER SKIN IS CRACKED IN THREE LOCATIONS (1ST XFS 310.250 ) (2ND 316.250) (3RD 322.750). CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845395Skin · crackedINSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN IS CRACKED AT XW 485. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845364Skin · corrodedINSPECTION TYPE:C3 RIGHT WING L/E SKIN UPPER I/B OF XFS 710.000 HAS INTERGRANULAR CORROSION AND IS CRACKED. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845351Skin · crackedRT WING LE SKIN IS CRACKED AT TWO LOCATIONS XW 257. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.SDR UPS05845342Skin · corrodedRT WING LE UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 622.500. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845340Skin · crackedRT WING LE UPPER SKIN IS CRACKED AT XFS 580.000. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 33.SDR UPS05845339Skin · corrodedLT WING LE UPPER SKIN IS CRACKED IB OF XFS 710.000. NO CRACK NOTED, FOUND TO BE CORROSION, CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845335Skin · corrodedRT WING LE UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 766.250. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 38.SDR UPS05845334Skin · crackedRT WING LE SKIN IS CRACKED AT FASTENER HOLE XFS 666.250. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1.SDR VNAA0508027Skin · crackedDURING THE INTERMEDIATE INSPECTION THE CREW DISCOVERED A CRACK AND DELAMINATION DAMAGE ON THE LEFT WINGLET TRAILING EDGE FAIRING. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-31-668SDR UPS05845324Doubler · crackedC3 RT LE LWR INNER DOUBLER CRACKED AROUND DRAIN HOLE (2 EA CRACKS). REMOVED, FABRICATED, AND INSTALLED INNER DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769600.SDR GTIA050243Skin · crackedFTW - FOUND RIGHT WING REFUELING STATION DOOR CUTOUT INBOARD CORNER DOUBLER CRACKED. REMOVED CRACKED SECTION AND FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER. (M)SDR 05FDEA02686Access Panel · wornLEFT WING ACCESS PANEL FOUND HARDWARE ON EXTERNAL SKIN WITH HOLE WORN. REPAIR WITH DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2 VOL I.SDR 05FDEA02685Access Panel · wornLT WING ACCESS PANEL FOUND HARDWARE ON EXTERNAL SKIN WITH HOLE WORN. REPAIR WITH DOUBLER IAW SRM 57-10-00 FIG 10A VOL I.SDR UPS05845542Skin · crackedINSPECTION TYPE: C3, LT WING UPPER SURFACE CRACKED AT XRS 22.750. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 801-804078 A.SDR UPS05845492Doubler · crackedRT WING LWR SURFACE DOUBLER CORRODED AND POSSIBLE CRACK AT XW 408.343 AFT SIDE AROUND FASTENER HOLE. NDT DETECTED A 1/2" CRACK EXTENDING FROM FASTENER HOLE TO EDGE OF PART. CUT OUT DAMAGE, TREAT, AND PRIMED IAW SAA SK 801-804073.SDR 05FDEA02660Skin · corrodedCOMPLY WITH EA 7-5710-82121, WINGS-STRUCTURE- REPAIR OF CENTER SECTION LOWER SKIN CORROSION. COMPLIED WITH EA 7-5710-82121 WINGS STRUCTURE REPAIR OF CENTER SECTION LOWER SKIN CORROSION THIS IS A MAJOR REPAIR RII:497236.SDR USAA051054Skin · crackedCLT - FOUND SKIN CRACKED 12 INCHES, IMMEDIATELY AFT OF SLAT ACTUATOR. REMOVED DAMAGE AND INSTALLED SPACER AND DOUBLER IAW SRM 57-43-01. (M)SDR AWXA200501057Skin · corrodedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON TOP LEFT WING INTERSPAR SKIN AT BS 616, STR 9L, WS 78L. MAINTENANCE BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS PER BOEING 737-300 SRM 57-20-01 FIG 101. FABRICATED REPAIR ANGLE IAW AMERICASDR 1050617008AMWPanel · failedLEFT WING UPPER BIN EVIDENCE OF DEFORMATION AT TURTLE BACK MOUNT FLANGE AREA. REPAIRED IAW SR-CO-00024. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.SDR 05FDEA02574Skin · damagedLT WING TIP FOUND 1EA EXTERNAL DOUBLER REPAIR ON EXTERNAL SKIN. REPAIRED IAW SB 57-27SDR 05FDEA02568Skin · damagedLT WING INB'D L/E FOUND 1EA EXTERNAL DOUBLER REPAIR ON SKIN AT XORS 87. REPAIRED IAW SRM 57-10-00 FIGURE 40 VOL.1.SDR 05FDEA02567Skin · damagedLT WING OUT'B L/E FOUND 1EA DOUBLER REPAIR ON SKIN AT XORS 506. FABRICATED DOUBLER REPAIR IAW SRM 57-10-00 FIGURE 68 VOL.1.SDR 05FDEA02550Skin · dentedLT WING LE PANEL 516EB , FOUND DENT EXTERIOR SURFACE AT STICKER. REPAIR CARRIED OUT AS PER EA1-5710-90127.SDR DHL2005748522Skin · dentedDENT ON LWR SURFACE OF RT WING INBD AFT FLAP 70" FROM OTBD END. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA 8.0 BY 2.25 AND FAB DOUBLER .050 7075 T6 PO 9002507 5.25 BY 11.25 IAW B727 SRM 57-50-4 FIG 5. TREATED AND PRIMED REPAIR PART AND AREA IAW B727 SRSDR DHL2005748517Skin · crackedRT WING UPPER TE PANEL CRACK NOTED FWD OF NR 11 SPOILER HINGE CUT OUT WS 464 AND REAR SPAR. STOP DRILLED CRACK .250 DIA IAW B727 SRM 51-10-1 FAB FROM 7075 T6 .071 6 3/4" BY 4" PO 900989 IAW B727 SRM 57-30-04 FIG10 DETAIL III. TREATED AND PRIMED DOUBLER IAW BSDR MALA050662Skin · scratchedDURING 4Y/2Y INSPECTION, FOUND LT WING LOWER SKIN AT WS71.5 IS SCRATCHED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$57101. REF: EAMS WORK ORDER 212631 TASK 5509.SDR MALA050648Skin · damagedWHILE ACCOMPLISHING C3 INSPECTION, FOUND A CRACK ON THE PANEL BETWEEN THE RIGHT WING AND AILERON HORN JUST AFT OF THE WING TIP, PANEL 691AR.SDR IXXA05SMN177SAccess Door · crackedDURING ROUTINE C-CHECK INSPECTION, RIGHT WING SLOT DOOR CRACKED 1, STA XILD 7095 XS 250.089. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR (NEW CONDITION) ON RIGHT WING IAW DC-8 MM 27-80-02 PAGES 201-204.SDR IXXA05SMN176SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, RIGHT WING UPPER SKIN CRACKED 1, STA XW 74 STR 9. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPSDR 05FDEA02396Skin · damagedLT WING UPPER SIDE INTERNAL L/E XORS=778 EXISTING REPAIR DOUBLER ON EXT SKIN. REMOVED AND REPLACE EXISTING REPAIR WITH NEW ONE IAW SRM 57-10-00 FIGURE 68 VOL 1.SDR 05FDEA02395Skin · damagedRT WING DROP L/E XW=332 EXISTING FLUSH REPAIR DOUBLER ON EXT SKIN. REMOVED OLD REPAIR AND INSTALL NEW REPAIR IAW SRM 57-10-00 FIG 39 VOL 1.SDR UPS05845367Skin · crackedINSPECTION TYPE:C1 RIGHT WING UPPER SKIN .25 INCH CRACK AT STA XCW 69 REAR SPAR AREA. CUT OUT CRACKED SECTION OF RIGHT WING AT XCW 69, NDT VERIFIED CRACK TERMINATION IAW HFEC INSP PER NDTSPM 06-10-01.001. FABRICATED -4 FILLER, -6 FILLER AND -8 DOUBLER IAW SRSDR VNAA0508009Skin · lightning strikeAFTER LANDING THE CREW REPORTED POSSIBLE LIGHTNING DAMAGE ON THE LEFT WINGLET TRAILING EDGE. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801, AMM 05-51-05-220-801, AND AMM 05-51-05-220-803. THE LT WISDR IXXA05SMN162SSkin · crackedDURING C CHECK INSPECTION, LT WING, UPPER SKIN HAS 03 CRACKS, XRS 74.000 S-9 S-10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 17, EO SEMAN NR 20051135 DATE 08-10-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SR, 57-2SDR IXXA05SMN163SAccess Door · crackedDURING ROUTINE C CHECK INSPECTION, LT WING, SLOT ACCESS DOOR CRACKED 1, XILD 7095 XS 250.089. REMOVED AND REPLACED INBD SLOT UPPER DOOR ON LT WING IAW DC-8 MM 27-80-02 PAGES 201-204.SDR IXXA05SMN159SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, LT WING.- T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, XW 0.000 XW 47.000. REMOVED DELAMINATED PANEL AND REPLACED ON LH WING T/E UPPER PANEL EXTERNAL SKIN, XW 0.000 – XW 47.000 IAW DC8 SRM 51-3-0SDR UPS05845238Skin · corrodedSEVERE CORROSION BETWEEN OUTER SKIN AND FRAME LOWER SURFACE AT SKIN SEAM IN FRONT OF THE LEFT SIDE FUEL DUMP MANIFOLD. REMOVED EXISTING DOUBLER, REMOVED DAMAGE, FAB`D FILLER AND DOUBLER AND INSTALLED IAW SRM 57-02-00-0, DWG 5649654.
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