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 DHL2007806595Doubler · crackedLT WING ACCESS DOOR NR 505F INTERNAL DOUBLER CRACKED 0.250" STA XRS 135.000 X-5 TO S-6 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 04-18-07, BOEING MESSAGE NR 1-306853011 DATED 04-18-07, NR 1-306853011-2 DATED 03-27-07. REMOVED FASTENERSSDR QXEA200700696Skin Panel · chafedC4 OKC - FOUND PANEL 632CB INNER SKIN CHAFED. REPAIRED IAW SRM 57-41-01 AND 51-21-11.SDR 07FDEA01526Skin · corrodedLEFT WING TRAILING EDGE UPPER SURFACE AT STA XORS 405-415 CLOSEOUT STRAP AND REAR SPAR ARE CORRODED. . [SUP 05-06-07] REMOVED AND REPLACED CLOSE-OUT STRAP IAW DAC DRAWING ARC0771,DC10 SRM 51-31-01 VOL II AND 51-33-01 VOL II.REMOVED CORROSION IAW DC10 SRM 5SDR 07FDEA01525Skin · corrodedLEFT WING TRAILING EDGE UPPER SURFACE CLOSEOUT PANEL IS BULGED AT THE NR 3 SPOILER AREA. INSTALLED L/W T/EDGE PANELS BETWEEN NR 2 AND 5 SPOILERS. CORROSION REMOVAL TO BE ACCOMPLISHED ON FEDEX N/R N000828-SDR 07-1740.SDR QXEA200700697Skin · damagedC4 OKC - FOUND PANEL 632CB OUTER SKIN DAMAGED TWO PLACES. REPAIRED IAW SRM 57-41-01 AND 57-42-32.SDR UPS07M50144Skin · dentedINSPECTION TYPE:C RIGHT WING UPPER SURFACE FIXED L/E STRUCTURE FOUND DEEP DENT AT STA XORS 593 AREA. RIGHT WING L/E COMPT RIBS 4EA REMOVED. RIGHT WING L/E DAMAGED SKIN TRIMMED PER EN12 63-07. HFEC INSP CUT OUT ON TRIMMED OFF AREA, FOUND NO CRACK. REPAIR SKSDR DHL2007806573Skin · damagedLT WING CTR L/E LWR SKIN HAS ELONGATED HOLES STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00004 DATED 03-27-07 REV IR. FABRICATED REPAIR DOUBLER (AL7075T6 0.071") IAW ASDR QXEA200700711Skin · chafedC4 OKC - LEFT WING FIXED LEADING EDGE CHAFED AFT OF THE MATING POINT OF SLAT NR 1 AND NR 2. REPAIRED IAW SRM 51-12-00, 57-41-01, 51-21-11.SDR DHL2007806580Skin · crackedRT WING UPPER EXT SKIN CRACKED 0.250" STA XRS 74.000 S-11 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHEET 1, PG 59-60. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (AL7075T6 0.125") AND FILLER PLUG (AL7075T6 0.280") IAW SRM 57-2-1 FIG 10SDR VNAA0704006Winglet · lightning strikeCREW REPORTED A LIGHTNING STRIKE UPON POST FLIGHT INSPECTION. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND WINGLET. MAINTENANCE REPAIRED ALL DAMAGE. OPERATIONAL CHECKS WERE PERFORMESDR DU4R2007104Plate · corrodedFOUND LT WING TANK PLATE 541EB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 112N6101-1 IAW DELTA JOB CARD OPN 3512.SDR DU4R2007103Plate · corrodedFOUND RT WING TANK PLATE 641EB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612.SDR 07FDEA01456Skin · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).SDR 07FDEA01449Doubler · damagedFOUND DOUBLER ON CENTER WING STA 1216 TO STA 1257 RT SIDE B/T XCW 47 TO XCW 81. DOUBLER INSTALLED PER P TO F MOD, EF DWG S110570002 AND VSP0022 SEE FAA FORM 337, DATED 26 JUNE 1998, SEE ENGINEERING RECOMMENDED ACTION.SDR UPS07849826Skin · crackedINSPECTION TYPE:C1 LEFT WING UPPER REAR SPAR SKIN CRACKED 5 INCHES AT STA XCW 69. REPAIRED LEFT WING UPPER AFT SPAR AT STA XCW 69.5 IAW SAA EA 008- 5710-01-A0835, UPS EO DC8-5730-26787-A, AND FAA FORM 8100-9.SDR 07FDEA01441Skin · corrodedCORROSION FOUND IN CWB UPPER SURFACE BETWEEN FR46/47 AND FR48 BETWEEN Y1555 AND Y1850. PERFORM NDT INSPECTION NTM 51-10-08, 51-10-01 AND 51-10-04. REPAIRED PER SRM 57-10-12 PG. 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.SDR 07FDEA01440Skin · corrodedLT WING OUTER SKIN SURFACE WITH CORROSION ON T/E AREA 591 RIB 27 REPAIRED PER FEDEX EA 6-5710-106708. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS " MAJOR.SDR 07FDEA01446Skin · tool damageRT WING REAR SPAR, MISDRILLED HOLE ON BOTTOM SKIN DURING EMBODIMENT OF SB 57-2081. REPAIR WAS PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5710-103285 AND RAS/BAE/1003241/2006 ISSUE "A".SDR 07FDEA01434Skin · misalignedAT LT WING REAR SPAR, FOUR MISDRILLED HOLES WHILE INSTALLING REINFORCING PLATE R573-49237-202, -203 IAW SB A310-57-2081. REPAIR PERFORMED BY OVERSIZING THE HOLES IAW EA 6-5710-103264 AND RAS/BAE/1003170/2006 ISSUE "A".SDR 07FDEA01430Skin · corrodedCORROSION FINDINGS ON BOTTOM SKIN PANEL NR 1 AND NR 2, RT WING, RIB 17-27. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING FASTENER HOLE RIB 28A-29 IAW EA 6-5720-103284 AND RAS/BAE/1003245/2006 ISSUE "A".SDR 07FDEA01429Skin · corrodedCORROSION FINDINGS ON BOTTOM SKIN PANEL NR 1 AND NR 2, RIB 17-19 AND RIB 21-24. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-103322 AND RAS/BAE/1003249/2006 ISSUE "A".SDR 07FDEA01428Skin · crackedCRACK FINDING ON PYLON REINFORCEMENT PLATE, RIB 8-9, RT WING (HOLE 1, CRACK LENGTH 14MM; HOLE 4 CRACK LENGTH 20MM). REPAIR PERFORMED BY REAM UP HOLES IAW EA 6-5720-101271 AND RAS/BAE/1003147/2006 ISSUE "A".SDR 07FDEA01427Panel · corrodedCORROSION FINDINGS ON CENTER WING BOX LOWER PANEL LT AT C47 IN SEVERAL HOLES (NR 1- NR 21). REPAIR PERFORMED BY BLEND OUT AND REAM UP HOLES IAW EA 6-5710-103305 AND RAS 046071/006/2006 ISSUE "A".SDR 07FDEA01425Skin · corrodedCORROSION ON PYLON REINFORCING PLATE ON THE LT WING, UNDERNEATH THE SPIGOT FITTING. REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5720-103303 AND RAS/BAE/1002985/2006 ISSUE "A".SDR 07FDEA01419Skin · corrodedCORROSION AROUND THE INBOARD (RIB 13-14) AND OUTBOARD (RIB 27-28) OVERWING REFUELING PORTS OF THE LT AND RT WINGS. REPAIR PERFORMED BY LOCALIZED BLENDING AND SOME SUIT LOCALLY MANUFACTURED PACKERS IAW EA 6-5720-103301 AND RAS/BAE/1002880/2006 ISSUE "A".SDR K11A2008120372203Skin · dentedSEVERAL DENTS, LEFT WING L/E BL 70.59 - 130.59.SDR K11A2008120372202Skin · dentedSEVERAL DENTS, RIGHT WING L/E BL 70.59 - 130.59.SDR K11A2008120272210Skin · dentedSEVERAL DENTS ALONG LEADING EDGE, LT WING ABOVE KRUEGER FLAPS.SDR K11A2008120272209Skin · dentedSEVERAL DENTS ALONG LEADING EDGE, RT WING ABOVE KRUEGER FLAPS.SDR 07FDEA01417Skin · crackedRIGHT WING, NR 4 LEADING EDGE SLAT O/B TRACK LOWER CUTOUT I/B CORNER FOUND CRACKED. [SUP 04-30-07] REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 07FDEA01407Panel · corrodedCORROSION ON LT BOTTOM WING PANEL NR 2, RIB 28/30. REPAIR PERFORMED BY BLEND OUT IAW 6-5720-101273 AND RAS/BAE/1002867/2006 ISSUE "A".SDR 07FDEA01400Skin · corrodedIMPACT AND CORROSION AROUND ACCESS HOLES OF LT WING BOTTOM SKIN BETWEEN RIB 22-23, RIB 28A-29 AND RIB 29-30. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-101243 ISSUE "A" AND RAS/BAE/1002786/2006 ISSUE "A".SDR 07FDEA01399Skin · corrodedCORROSION ON AN OLD REPAIR LT WING BOX FWD OF FRONT SPAR, BETWEEN RIB 28A-29. REPAIR PERFORMED BY REAM UP THE AFFECTED HOLES AND OVERSIZING IAW EA 6-5720-101242 AND RAS/BAE/1002718/2006 ISSUE "A".SDR DHL2007806546Skin · wornRT OTBD FLAP UPPER SKIN WORN STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-30-07, ASTAR DRAWING NR D857R1020 DATED 03-28-07. REMOVED EXISTING DAMAGED REPAIR SEGMENT AND INTERNAL SPLICE IAW SRM 51-1-21. FABRICATED NEW REPSDR DHL2007806555Skin · damagedRT WING CTR L/E LOWER SKIN HOLES ELONGATED STA XFS 526.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-06-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00006 REV IR DATED 03-28-07. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPASDR DHL2007806554Skin · damagedRT CTR L/E OTBD SLOT HOLES ELONGATED, STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-05-07, ENGINEERING VARIATION AUTHORIZATION NR D852-00003 DATED 03-18-07 REV IR. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTSDR DU4R2007102Plate · corrodedFOUND RT WING TANK PLATE 641MB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612.SDR DU4R2007101Plate · corrodedFOUND RT WING TANK PLATE 641AB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612.SDR DU4R2007100Plate · corrodedFOUND RT WING TANK PLATE 641DB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612.SDR DU4R2007099Plate · corrodedFOUND RT WING TANK PLATE 641FB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612.SDR 07FDEA01364Skin · crackedLEFT WING FAIRING NR 3343 VERIFIED MATERIAL AS 2024-0 .050 REF DWG 65-22555 AND SRM 51-40-2 PG 1. STOPPED DRILLED CRACK REF SRM 51-10-PG 13 ITEM 10, HFEC IAW 727NDT MAN PART 6, 51-00-00 FIG 23. TOOL NR IDM 0031 11-30-07. VERIFIED CRACK TO BE CONFINED BY STOSDR 07FDEA01353Skin · crackedLEFT WING DROOPED LEADING EDGE UPPER SURFACE FOUND CRACKED. [SUP 4-19-07] REMOVED AND REPLACED AS PER AMM 27-80-10. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR DHL2007806531Doubler · crackedRT WING ACCESS DOOR NR 505F INTERNAL DOUBLER HAS TWO CRACKS OF 0.500" AND 0.250" STA XRS 18.000 S-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 36. PERFORMED NSDR DHL2007806532Doubler · crackedLT WING ACCESS DOOR NR 505F INTERNAL DOUBLER CRACKED 0.250" STA XRS 21.000 S-5 TO S-6 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 36. PERFORMED NDT INSPECTION IASDR 07FDEA01317Skin · crackedRT WING DURING INSPECTION WITH EO NR 8-5100-7-5001 P2 FOUND 1 CRACK 1" LONG ON UPPER SKIN OF O/B FLAP. REPAIRED SKIN IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1.SDR 07FDEA01316Skin · crackedRT WING L/E ON EXTERNAL SKIN FOUND 1 CRACK 1" LONG. REPAIRED CRACK ON L/E SKIN IAW SRM 57-10-00 FIG 68 SHT 1 VOL 1.SDR 07FDEA01343Skin · crackedLT WING LWR EXT SKIN L/E FOUND CRACK 0.5" LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1.SDR 07FDEA01327Skin · crackedRT WING LEADING EDGE UPPER SURFACE CUTOUT AT NR 5 SLAT INBD GUIDE IS GOUGED AND CRACKED AT AFT EDGE REMOVED SLAT SEALS AND COVER FOR ACCESS, DAMAGE REMOVED REF SRM 57-30-2. HFEC FOR CRACKS REF B727 NDT MANUAL PART 6. FABRICATED PART AND INSTALLED REPAIR REF SDR 07FDEA01323Skin · crackedLT WING L/E CRACK LONG 0.75" ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 SHT 1-3 VOL 1.SDR 07FDEA01320Skin · crackedRT WING L/E EXTERNAL SKIN FOUND 1 CRACK 1.5" LONG. REPAIRED SKIN IAW SRM 57-10-00 FIGURE 68 SHT 2 VOL 1.
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