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 ASOA05580Skin · crackedDURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 RT IAW ASA EO 600-57-0134A. (M)SDR UPS05844981Skin · crackedINSPECTION TYPE:C1 RH WING UPPER AFT SKIN PANEL AT XCW 69.500 CRACKED 1 INCH LONG. CUT OUT DAMAGE,FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-02-01 FIG. 20.SDR VNAA0507001Skin · lightning strikeAFTER LANDING MAINTENANCE DISCOVERED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WING TIP. A DETAILED LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-05-220-801. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR DHL2005746511Skin · gougedRT WING LOWER WS 770 FWD HAS EDGE OF SKIN GOUGED. CUT OUT DAMAGED SECTION OF SKIN AT WS 770 LWR SKIN DIM 3/4"X 2.5" IAW B727 SRM 57-30-4 FIG 1. FABBED REPAIR DOUBLER FROM .080 2024 T3 PO 9002255 DIM 3 1/8" X 6 3/4" IAW B727 SRM 57-30-4 FIG 1. TREATED AND PRSDR 05FDEA01760Skin · delaminatedDURING CONVERSION FOUND ON RT WING, LE UPPER SIDE, STA XW 346, WITH DELAMINATION. REPAIRED IAW SRM 57-00-01 FIG 4, SH 2. (OPEN)SDR IXXA05SMN147SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT WING INTERIOR ANGLE DEFORMED, STA XFS -17.500 TO XFS -11.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05259 DATE 06-24-05, SEMAN DWG ED 4016 DATE 06-20-05, EO SEMAN NR 2005948 DATE 06-24-05.SDR IXXA05SMN153SSkin Panel · improperDURING ROUTINE C-CHECK INSPECTION, RH. INBD. FLAP.- FWD UPPER PLATING HAS INTERIN REPAIR, XF 134.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN 20051009 DATE 06-28-05. REMOVED PLATING WITH INTERIM REPAIR IAW DC-8 SRMSDR IXXA05SMN151SSkin Panel · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING. SLANT PANEL UPPER PART CORRODED, XFS 38.750 - XFS 70.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 37, EO NR 20051004 DATE 06-16-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21. SMOOTHED AND PESDR IXXA05SMN150SSkin · dentedDURING C CHECK INSPECTION, LT IB FLAP UPPER PART WITH SEVERAL DENTS XW 2.000 - XW 20.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1, EO NR 20051013 DATE 06-29-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-3-0PAGE 1. REMOVED PLATING SEGMENT (DAMAGED)SDR IXXA05SMN149SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LH INBD FLAP UPPER PART DENTED, XW 131.000 PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN Nº 20051010 DATE 06-28-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLSDR IXXA05SMN144SSkin · improperDURING ROUTINE C CHECK INSPECTION, RT WING. CTR L/E SKIN FWD PART HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-3-1 FIG. 5 SHEET 1, EO SEMAN NR 2005910 DATE 06-18-05. REMOVED DAMAGED PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 SDR IXXA05SMN141SSkin · deformedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SURFACE DEFORMED, STA XFS -11.250 TO XFS -23.750. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 05259, SEMAN DWG ED 4016, EO SEMAN 2005948.SDR IXXA05SMN140SSkin · brokenDURING ROUTINE C CHECK INSPECTION, LT WING IB L/E UPPER SURFACE BROKEN, STA XFS 51.250 - 57.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 25, EO SEMAN NR 2005908 DATE 06-15-05. REMOVED DAMAGED AREA IAW SRM 57-2-1 FIG. 21. PERFORMED NDT INSPECTION IAW NDT SSDR IXXA05SMN138SSkin · improperDURING ROUTINE C CHECK INSP, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIR AT STA XF 415.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005914 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PAGE 1. FSDR IXXA05SMN137SSkin · wornDURING ROUTINE C CHECK INSPECTION, RT OTBD FLAP FWD UPPER PLATING WORN, STA XF 226.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05258 DATE 06-24-05, SEMAN DWG ED 4005 DATE 06-20-05, EO SEMAN 2005913 DATE 06-24-05. REMOVED FASTENERS IAW DC-8 SRSDR IXXA05SMN136SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT OB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (03 EA) AND WEAR DAMAGES BETWEEN STA XF 197.000 - XF 213.000PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4 TR NR 57-94, EO SEMAN NR 2005912 DATE 06-18-05. REMSDR IXXA05SMN135SSkin · improperDURING ROUTINE C CHECK INSPECTION, RT IB FLAP LOWER UPPER PLATING NON STANDARD REPAIRS (02 EA) STA XF 45.000 - XF 87.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1, EO NR 2005947. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SRM SDR DHL2005802505Doubler · crackedRT OUTER WING INBD L/E LWR DOUBLER CRACKED 0.250. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED DOUBLER (AL7075T6 0.050) IAW SRM 57-3-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG SDR 05FDEA01749Skin · puncturedLT WING FIXED LE FOUND PUNCTURED AT XORS 402. PUNCTUREED SKIN ON LT WING FIXED L/E AT XORS402 TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00, FIG 14, VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (OPEN)SDR IXXA05SMN134SSkin Panel · improperDURING ROUTINE C CHECK INSPECTION, RT IB FLAP FWD UPPER PLATING NON STANDARD REPAIRS (02 EA ) STA XW 84.00 -XW 91.00. PERFORMED MAJOR REPAIR IAW NR 05258 DATE 06-24-05, DWG ED 4004, EO NR 2005911 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED PLATISDR UPS05444869Skin · corrodedINSPECTION TYPE: C, AFT T/E PANEL REMOVED FOR RECTIFICATION WING UPPER SKIN LWR SURFACE FOUND CORRODED AT WS 390. CORROSION BLEND OUT 0.131 X 1.25 X 2.5 INCHES EXCEED SRM 57-30-01 FIG 1 LIMITS, LEFT WING UPPER SKIN LOWER SURFACE REPAIRED AT WS 390 AREA AS PERSDR VNAA0506014Skin · lightning strikeAFTER LANDING THE CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801 AND 05-51-05-220-801. LIGHTNING DAMAGE FOUND ON THE LEFT WING TIP WAS REPAIRED IAW BOMBARDIER REO 601R-57-30-001. NO ASDR IXXA05SMN118SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LT OB FLAP, NON STANDARD REPAIR, XF 345.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4, TR NR 57-94, EO SEMAN NR 2005856 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 51-1-21 SDR IXXA05SMN117SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LT OB FLAP NON STANDARD REPAIR, XF 304.000 -XF 309.000 (UPPER PART). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1, SRM 57-7-1 FIG. 4, TR NR 57-94, EO SEMAN NR 2005854 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW SSDR IXXA05SMN115SSkin · nickedDURING ROUTINE C CHECK INSP, LT OB FLAP L/E NICKED, XF 226.000 (UPPER PART) PERFORMED MAJOR REPAIR, DWG NR ED 3987 DATE 06-20-05, EO. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED PLATING SEGMENT IAW DWG ED 3987. PERFORMED NDT INSP IAW SPM. NO CRACK, CORROSION FSDR IXXA05SMN114SSkin Panel · dentedDURING C CHECK INSPECTION, LT OTBD FLAP L/E DENTED, XF 213.000 (UPPER PART. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PG 1, DC-8 SRM 57-7-1 FIG 4, TR NR 57-94, EO SEMAN NR 2005852 DATE 06-18-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51SDR IXXA05SMN113SSkin · improperDURING ROUTINE C CHECK INSPECTION, LT IB FLAP REPAIR IMPROPER, XF 415.000 (UPPER PART) PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG. 1. EO SEMAN NR 2005858 DATE 06-18-05. REMOVED DAMAGED PLATING IAW SRM 57-2-5 FIG. 1(SHEET 1,2). PERFORMED DETAILED VISUAL INSPECTISDR IXXA05SMN112SSkin · improperDURING C CHECK INSPECTION, LT OTBD FLAP L/E UPPER PART NON STANDARD REPAIR, XF 415.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PG 1, DC-8 SRM 57-7-1 FIG 4, TR # 57-94, EO SEMAN NR 2005857 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW DC-8 SRM 5SDR IXXA05SMN111SWing · crackedDURING ROUTINE C CHECK INSPECTION, RT WING UPPER SKIN CRACKED 1INCH, STA. XRS 74. 869, S-10. REMOVED EXISTING REPAIR DOUBLERS SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 3981. PERFORMED NDT INSPECTION IAW SPM PART 06-10-01-001. FABRICATED EXTESDR IXXA05SMN110SSkin · crackedDURING C CHECK INSPECT, RT WING UPPER SKIN HAS 2 CRACKS OF 1" EACH AT XRS 74. 869, S-15 AND S-16. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05280 DATE 07-04-05, SEMAN DWG # ED 3981 DATE 06-29-05, EO SEMAN NR 2005834 DATE 07-04-05. REMOVED EXISTING REPAIR SDR IXXA05SMN109SWing · elongatedDURING C CHECK INSPECT, LT WING, NR 2 STUB WING VANE SLOT HOLE ELONGATED, XS 247.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05270 DATE 06-29-05, SEMAN DWG # 3986 DATE 06-28-05, EO SEMAN # 2005849 DATE 06-29-05. REMOVED DAMAGED AREA IAW SEMAN DWG ED 398SDR IXXA05SMN106SSkin · wornDURING ROUTINE C CHECK INSPECTION, LH INBOARD FLAP UPPER PART SKIN WORN, XW 104.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN NR 2005850 DATE 06-18-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 51-1-21 PAGE 1. FABRICATED SDR IXXA05SMN100SPanel · corrodedDURING ROUTINE C CHECK INSPECTION, LH WING.- SLANT PANEL UPPER PART CORRODED, XW 6.000 PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG. 37, EO SEMAN Nº 2005847 DATE 06-16-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. SMOOTHED, PESDR IXXA05SMN99SSkin · crackedDURING C CHECK INSPECT, LT WING, SKIN UPPER PART WITH 02 CRACKS 1", 1/2", XRS 74.000 S-9 - S10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 10, EO SEMAN NR 2005833 DATE 06-14-05. REMOVED DAMAGED AREA IAW DC-8 SRM 57-2-1 FIG 10 (SHEET 3). PERFORMED NDT INSPSDR IXXA05SMN96SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 5 SPOILER LWR SKIN WITH 02 CRACKS 2", XRS 367.000 - XRS 421.000. REMOVED REPLACED NR 5 SPOILER PANEL ON LT WING XRS 367.000 XRS 421.000 IN ACCORDANCE WITH DC-8B MM 27-61-1 PAGES 201-205.SDR IXXA05SMN94SSkin · crackedDURING C CHECK INSPECTION, RT MLG REMOVE AND INSTALL CTR DOOR (LWR SKIN CRACKED). REMOVED AND REPLACED CTR MAIN PANEL ON RT MLG IN ACCORDANCE WITH DC-8 MM 32-12-1 PAGE 401. FOR OPS CHECK SEE J/C 74204.SDR IXXA05SMN95SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, LT LWR WING T/E NR 546 ACCESS DOOR EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED EXTERNAL PANEL IN LT LWR WING T/E NR 546 ACCESS DOOR IN ACCORDANCE WITH DPS 367-15.SDR IXXA05SMN93SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RT WING, T/E LWR PANEL EXTERNAL , INTERNAL SKIN DELAMINATED, XW 0.000 - XW 90.000. REMOVED AND REPLACED PANEL ON RT WING T/E, XW 0.000 XW 90.000 IAW DC-8 SRM 51-3-0 PAGE 1, DC-8 SRM 51-1-21 PAGE 14. TORQUED IAW DC-8 SRM 51-SDR UPS05844919Skin · crackedC1 RT WING LE LWR SKIN CRACKED 1 INCH LONG AROUND FASTENER HOLE AT XW 257. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5720 -4087-B APPENDIX C.SDR UPS05844918Skin · crackedINSPECTION TYPE: C1, LW NR 2 STUBWING UPPER OB CORNER HAS A CRACK IN SKIN. STOP DRILLED THREE CRACKS, FABRICATED, AND INSTALLED REPAIR IAW DC-8 S RM 57-2-0, 57-5-0, AND 57-2-1 FIG 18.SDR UPS05844917Skin · scratchedC1 DEEP SCRATCHS IN SKIN L/W UPPER SPAR CAP IB CORNER OF NR 2 STUB WING. SCRATCHS FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 FIG 26.SDR IXXA05SMN92SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RT WING UPPER T/E PANEL EXTERNAL SKIN DELAMINATED, XA 613.000 - XA 681.000. REMOVED AND REPLACED UPPER T/E PANEL ON RT WING XA 613.000 XA 681.000 IAW DC-8 SRM 51-3-0, DC-8 SRM 51-1-21 PAGE 1. TORQUED IAW DC-8 SRM 51-3-1.SDR IXXA05SMN77SSkin · crackedDURING C CHECK INSPECT, RT WING INBD OUTER L/E LWR SKIN CRACKED 1/2", XFS 591.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05270 DATE 06-29-05, SEMAN DWG ED 4017 DATE 06-28-05, EO SEMAN NR 2005969 DATE 06-29-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PSDR IXXA05SMN74SSkin · damagedDURING ROUTINE C CHECK INSPECTION, RT WING INBD L/E UPPER SKIN NON STANDARD REPAIR BETWEEN STA XFS 113.750 - XF 120.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG. 2J, EO SEMAN NR 2005970 DATE 06-23-05. REMOVED DAMAGED PLATING IAW DC-8 SRM 57-2-1 FIG. 2SDR 05FDEA01671Skin · bulgedRT WING TRAILING EDGE UPPER SURFACE AT XORS 826.50, OUTBOARD OF NR 5 SPOILER, FOUND BULGING. CORROSION REMOVED PER SRM 51-21-01 VOLUME II.SDR USAA050783Skin · corrodedCLT - FOUND WING UPPER SURFACE WITH CORROSION 2 INCH BY 3 INCH, 2 INCH BY 4 INCH, 2 INCH BY 2 INCH, 4 INCH BY 6 INCH, 1 INCH BY 3 INCH, BETWEEN WBL 117 AND WBL 133 AFT OF FWR SPAR, STRINGER 10 STRINGER 15. REMOVED CORROSION IAW SRM 57-20-01. (M)SDR 05FDEA01606Skin · delaminatedRIGHT WING UPPER SURFACE PANEL AT APU EXHAUST HAS DELAMINATION, CORROSION AND OLD REPAIR TORN OFF JUST AFT OF EXHAUST PORT. FABRICATED NEW PANEL AND INSTALLED NEW PANEL IAW SRM 51-30-5 & 51-30-2.SDR CHQA200500111Panel · leakingIN CRUISE AT FL310, A PASSENGER NOTIFIED F/A THAT A FLUID BUBBLE WAS COMING DOWN FLAPS ON RT WING. CAPT OBSERVED RT WING FROM FORWARD FLAP SECTION TO REAR FLAP WAS DARK GRAY COLOR & APPEARED WET. DIVERTED FOR FURTHER INSPECTION, AN EMERGENCY DECLARED. ON RUSDR GTIA050189Skin · damagedEXTERNAL REPAIR LEFT WING L/E XIS 241.081 IS DAMAGED. DOUBLER OUT OF LIMITS. REMOVED DAMAGED DOUBLER FROM LEFT WING. FABRICATED REPAIR DOUBLER TREATED, PRIMED AND INSTALLED DOUBLER. (M)SDR ASAA0540277Skin · gougedLT WING UPPER SKIN GOUGED AT WING STA 223 BETWEEN STA 12 AND 13. BLENDED AREA, TREATED AND PRIMED IAW EA. (K)
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