JASC 5712

Service difficulty reports · 6,970

Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712'
  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.

SDR UPS00832558Rib · crackedINSPECTION TYPE:C-2, LEFT WING CENTER L/E RIB CRACKED STA XOLDI 6.225. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED DOUBLER IAW 57-2-0 FIG-2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832434Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 647. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832433Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 785. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832432Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832426Rib · crackedINSPECTION TYPE:C2, RT WING L/E AT STA XFS 792.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR TWAA0006421Rib · crackedDURING CHECK-C MAINT, TIE CLIP WAS CRACKED AT LT WING FRONT SPAR TO RIB AT UPPER T/E, 9 INCHES I/B OF NUMBER 7 TRACK, AFT OF NR 2 L/E SLAT. REPLACED CLIP. RIB FOUND TO BE CRACKED UNDER THE CLIP. STOP DRILLED THE UPPER CRACK AND ROUTED OUT THE LOWER CRACK.Apr 18, 2000 · N9306T · Doug DC983SDR MALA000294Rib · crackedDURING C-CHECK, FOUND 3 & 4 RIBS CRACKED AT ENDS OF LEADING EDGE STA 611 BR. MX FABRICATED NEW ANGLES AND SHIMS IAW 57-10-30, HOLES TRANSFERRED FROM EXISTING HOLES AND IAW SRM 57-10-30. CUT BACK 3 SUPPORT RIBS WITH CRACKS IN REF TO SRM 57-10-30, FNDT REQUIREApr 14, 2000 · N406XJ · Saab 340BSDR RRXA002279Rib · crackedDURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK TO THE UPPER RIB ON THE NR 2 STUB WING AT STA XFS 250.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 5Apr 7, 2000 · N995CF · Doug DC862SDR TWAA0005608Rib · crackedDURING OP 16 MAINT CHECK, FOUND LT WING L/E RIB APPROX 7 INCHES I/B OF NUMBER 11 SLAT TRACK WAS CRACKED AT LOWER AFT FASTENER, AND ANOTHER CRACK 19 INCHES /B OF NUMBER 11 SLAT TRACK AT LOWER AFT FASTENER. REPAIRED PER SRM 57-02 FIG 6.Apr 5, 2000 · N989Z · Doug DC931SDR RRXA002278Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING NR 2 STUB WING UPPER RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW EO NR 00-047 WITH APPROVED 8110-3 DATEApr 4, 2000 · N995CF · Doug DC862SDR UPS00832215Rib · crackedINSPECTION TYPE: C, LT WING LE UPPER RIB CRACKED AT XILD .7095 REPAIRED I.A.W. SRM. 57-2-0 FIG. 2Apr 4, 2000 · N709UP · Doug DC871FSDR UPS00832342Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 360.25 AND XS 442.185. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 3, 2000 · N709UP · Doug DC871FSDR UPS00832227Rib · crackedINSPECTION TYPE: C1, RT WING LE RIB IS CRACKED AT XS 535. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2Apr 3, 2000 · N709UP · Doug DC871FSDR UPS00832223Rib · crackedINSPECTION TYPE: C1, LT WING LE, VERTICLE RIB IS CRACKED AT XW 240. REMOVED, FABRICATED, AND REPLACED RIB I.A.W. DWG. 9753294, AND SRM. 51- 1-21,51-1-20DApr 3, 2000 · N709UP · Doug DC871FSDR UPS00832222Rib · crackedINSPECTION TYPE: C1, RT WING LE, UPPER RIB IS CRACKED AT XFS 328.750. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2Apr 3, 2000 · N709UP · Doug DC871FSDR UPS00832389Rib · crackedINSPECTION TYPE:C123 LEFT WING L/E RIB IS CRACKED AT XFS 691.25. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 2, 2000 · N709UP · Doug DC871FSDR UPS00832289Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XW 454. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 30, 2000 · N812UP · Doug DC873FSDR UPS00832285Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 304. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 30, 2000 · N812UP · Doug DC873FSDR TWAA0005303Rib · crackedDURING CHECK-C MAINT, THE RT WING LEADING EDGE RIB WAS CRACKED INSIDE PANEL 1211R BEHIND NUMBER 5 SLAT. REMOVED AND REPLACED RIB PER SPM 6-70-02. INSTALLED FASTENERS PER SRM 51-30-02.Mar 30, 2000 · N902TW · Doug DC982SDR UPS00832305Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XS461.372. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 29, 2000 · N812UP · Doug DC873FSDR UPS00832303Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 716.25 AND XFS 722.5. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 29, 2000 · N812UP · Doug DC873FSDR UPS00832298Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 635. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 29, 2000 · N812UP · Doug DC873FSDR UPS00832292Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 379 AND XS 461. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 29, 2000 · N812UP · Doug DC873FSDR UPS00832290Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E HAS CRACKED RIBS UPPER SIDE AT XFS 735, 741.25, 778.75, 803.75, 828.75 AND LOWER SIDE AT XFS 785. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 29, 2000 · N812UP · Doug DC873FSDR UPS00832283Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 797.5. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 29, 2000 · N812UP · Doug DC873FSDR UPS00832269Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 610. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 28, 2000 · N812UP · Doug DC873FSDR UPS00832293Rib · crackedINSPECTION TYPE:C1 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 635.75 AND XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 27, 2000 · N812UP · Doug DC873FSDR UPS00832274Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 285.25. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 27, 2000 · N812UP · Doug DC873FSDR UPS00832267Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 672.5. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 27, 2000 · N812UP · Doug DC873FSDR RRXA002072Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT CENTER L/E UPPER RIB AT STA XFS 497.491, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20DMar 22, 2000 · N961R · Doug DC873FSDR RRXA002071Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E UPPER RIB AT STA XFS 461.372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20DMar 22, 2000 · N961R · Doug DC873FSDR 20000802SH008Rib · crackedDURING 100-HOUR INSPECTION, DISCOVERED THE RT WING LEADING EDGE NOSE RIB LOCATED AT STA 136.00 CRACKED AT THE LIGHTENING HOLE. SUBMITTER SUSPECTED PART WAS DAMAGED DURING INITIAL INSTALL AT THE FACTORY ASSY LINE. (X)Mar 22, 2000 · N2312V · Cessna 206HSDR UPS00832037Rib · crackedINSPECTION TYPE:C123 RIGHT WING L/E UPPER RIB IS CRACKED AT XS250.089. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 11, 2000 · N706UP · Doug DC871FSDR UPS00832059Rib · crackedINSPECTION TYPE: C1, RT WING LE UPPER RIB IS CRACKED AT STA. XS240.126. STOP DRILLED CRACK AND REPAIRED I.A.W. SRM 57-2-0 FIG.2.Mar 7, 2000 · N748UP · Doug DC871FSDR UPS00832025Rib · crackedINSPECTION TYPE:C1 RT L/E UPPER RIBS ARE CRACKED AT THE FOLLOWING LOCATIONS, XFS797.5, XFS766.25, XFS753.75 AND XFS785.0. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2.Mar 7, 2000 · N748UP · Doug DC871FSDR UPS00832021Rib · crackedINSPECTION TYPE:C1 RT WING L/E UPPER RIB IS CRACKED AT STA XFS828.75. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Mar 7, 2000 · N748UP · Doug DC871FSDR UPS00832016Rib · crackedINSPECTION TYPE:C1 RT WING L/E LOWER RIB IS CRACKED AT STA XFS635.0. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Mar 7, 2000 · N748UP · Doug DC871FSDR UPS00831991Rib · crackedINSPECTION TYPE:C1, LT WING L/E UPPER RIBS ARE CRACKED AT STA XFS 410.25 AND XFS 416.5. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2.Mar 7, 2000 · N748UP · Doug DC871FSDR RRXA000684Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE RT WING L/E RIB AT THE AFT LOWER FASTENER AT XF 722.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION/////REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-8-1. RECEIVED REPAIRED DOUBLER AND INSTALMar 5, 2000 · N831AL · Doug DC873FSDR UPS00432193Rib · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE, CORROSION ON LE RIB AT OLES 1543 RT O/B SIDE. NEW RIB FABRICATED AND INSTALLED I.A.W SRM 51-30-02.REF WORK SHOP OR DER E0098342.Mar 4, 2000 · N522UP · Boeing 747212BSDR QXEA0000722Rib · damagedPDX- RIGHT HAND WING FORGED RIB AT WS 2635 TOP FLANGE INBOARD EDGE HAS TOOL DAMAGE BETWEEN TOP SKIN STRINGERS 2.37 AND 2.38 AND BELOW STRINGER 2.36. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 5.Mar 4, 2000 · N478US · Fokker F28MK4000SDR UPS00832069Rib · crackedINSPECTION TYPE: C1, RT WING LE AT STA. XS250.089, THE UPPER LE RIB HAS A 10 INCH CRACK. REPAIRED AREA I.A.W. SRM 57-2-0 FIG.2.Mar 3, 2000 · N748UP · Doug DC871FSDR UPS00832048Rib · crackedINSPECTION TYPE: C1, RT WING LE AT STA. XFS397.750, LOWER LE RIB IS CRACKED AT MID SPAN. REPAIRED AREA I.A.W. SRM 57-2-0 FIG.2.Mar 3, 2000 · N748UP · Doug DC871FSDR TWAA0003906Rib · crackedDURING 0P 16 MAINT CHECK, THE RT WING LE INTERNAL RIB AT XRS 468 HAD A CRACK AT LOWER AFT MOUNT HOLE. REMOVED AND REPLACED LE INTERNAL RIB WITH MFG PN 9919330-8 PER 51-30.Mar 3, 2000 · N984Z · Doug DC931SDR UPS00832019Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB AT STA XFS366.5 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-02-0 FIG 2.Mar 3, 2000 · N748UP · Doug DC871FSDR UPS00832110Rib · crackedINSPECTION TYPE: C 1 RT WING LE. UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2Mar 2, 2000 · N748UP · Doug DC871FSDR UPS00832010Rib · crackedINSPECTION TYPE:C1, RT WING L/E LWR RIB FWD OF ACCESS PANEL OPENING IS CRACKED AT STA XFS810.0. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769471 AND SRM 51-1 -20D.Mar 2, 2000 · N748UP · Doug DC871FSDR RRXA000674Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT WING L/E RIB AT STA 822.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIGFeb 28, 2000 · N831AL · Doug DC873FSDR RRXA000673Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LT WING CENTER L/E UPPER RIB AT STA 448.581, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMBED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-Feb 28, 2000 · N831AL · Doug DC873FSDR UPS00831985Rib · crackedINSPECTION TYPE:C123, RT WING L/E AT STA XS250.089, THE RIB/END CAP IS CRACKED. REMOVED AND REPLACED END CAP IAW DWG 5769859 AND SRM 51-1-20D.Feb 26, 2000 · N706UP · Doug DC871F
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