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 UPS00831980Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E AT STA XS520.168, THE UPPER RIB/END CAP IS CRACKED. REMOVED AND REPLACED END CAP IAW DWG 5769857 AND SRM 51-1-20D.Feb 26, 2000 · N706UP · Doug DC871FSDR RRXA000670Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT RIGHT WING L/E RIB AT AFT UPPER END AT XFS 810, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIG 1B.Feb 24, 2000 · N831AL · Doug DC873FSDR RRXA000669Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT RT WING L/E RIB AT XFS 785.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIG 1B.Feb 24, 2000 · N831AL · Doug DC873FSDR RRXA000667Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RT WING L/E RIB AT XFS 753.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIRED DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 1B.Feb 24, 2000 · N831AL · Doug DC873FSDR RRXA000666Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE LEFT WING L/E RIB AT STA XFS 397.79, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AFeb 24, 2000 · N831AL · Doug DC873FSDR RAIA0002020Rib · crackedMX - STL - DURING LEFT WING AILERON PCA MODIFICATION, FOUND LEFT WING RIB 21 CRACKED AT UPPER CENTER RIB FLANGE. MAINTENANCE REPAIRED LEFT WING UPPER CENTER RIB FLANGE IAW MANUFACTURERS REPAIR INSTRUCTIONS.Feb 22, 2000 · N802HK · Emb EMB145SDR RRXA000719Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/E RIB AFT UPPER END STA XFS 741.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED CRACK IAW DC-8 SRM 57-2-0 FIG 2.Feb 19, 2000 · N831AL · Doug DC873FSDR RRXA000656Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LEFT WING L/E RIBS AFT FASTENERS AT STA XFS 741.250, 747.500. 753.750 AND 760.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLFeb 19, 2000 · N831AL · Doug DC873FSDR RRXA000690Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E RIBS AT STA'S XFS 366.500, 360.250, 354.000, 347.750, 341.500 AND 322.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AFeb 18, 2000 · N831AL · Doug DC873FSDR RRXA000647Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE LT WING L/E RIBS AT STA XFS 722.5, 728.75 AND 735.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2Feb 18, 2000 · N831AL · Doug DC873FSDR QXEA0000545Rib · corrodedPDX - RIGHT WING RIB 2230 LOWER STRUT BOX CHANNEL HAS CORROSION AND BUBBLED POINT, LOCATED AT 3 STRINGERS AFT OF 72A APERATURE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, ITEM 4C.Feb 18, 2000 · N488US · Fokker F28MK4000SDR RRXA000689Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E UPPER RIBS AT STA'S XFS 422.750, 416.500, 379, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIBS, REPAIRED AND INSTALLED IAW DC-8 SFeb 17, 2000 · N831AL · Doug DC873FSDR UPS00831681Rib · crackedINSPECTION TYPE:C123 LEFT WING CENTER L/E.. RIB CRACKED AT XFS 335.25. REPAIRED IAW SRM 57-2-0 FIG 2.Feb 16, 2000 · N707UP · Doug DC871FSDR TWAA0003009Rib · crackedDURING CHECK-C MAINT, ON RT WING LE RIB STA XRS 418 WAS CRACKED AT AFT END. THE CRACKED ATTACH ANGLE WAS REMOVED FROM LE FORMER. NEW ANGLE AND DOUBLER WERE FABRICATED FROM 7075-0 AND HEAT TREATED TO 7075-T6. PARTS INSTALLED PER SRM 57-06A, PAGE 17 FIG 5 SHEFeb 16, 2000 · N953U · Doug DC982SDR RRXA000688Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT O/B L/E UPPER RIBS, AT STA'S XFS 603.750, 610.000, 616.250 AND 622.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DFeb 15, 2000 · N831AL · Doug DC873FSDR RRXA000687Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE LT O/B CENTER L/E UPPER RIB AT FASTENER END AT STA'S XFS 635.000, 641.250, 653.750, 660.000 AND 672.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, RFeb 15, 2000 · N831AL · Doug DC873FSDR RRXA000662Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT FASTENER ON THE LT O/B LEADING EDGE UPPER RIB AT STA XFS 572.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS, STOP DRILLED TO THE CRACKS AND INSTAFeb 10, 2000 · N831AL · Doug DC873FSDR LR7A0010Rib · crackedDURING SCHEDULED C2 INSPECTION PER JOB CARD HSP53161, FOUND CWS 20.5 CENTER WING RT RIB CRACKED AT FS 579.5 BRACE. REPLACED IAW LAC MEA 382-57-00-017, SRM SMP 583-51-60 & 51-70.Feb 6, 2000 · N401LC · Lkheed 382GSDR RRXA002394Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 760.000, 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-8Feb 4, 2000 · N995CF · Doug DC862SDR RRXA002393Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 772.500, 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-8Feb 4, 2000 · N995CF · Doug DC862SDR RRXA002392Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 822.500, 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-8Feb 4, 2000 · N995CF · Doug DC862SDR RRXA002391Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 828.750, 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-8Feb 4, 2000 · N995CF · Doug DC862SDR RRXA002390Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 847.500, 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 Feb 3, 2000 · N995CF · Doug DC862SDR RRXA000641Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT LOWER AFT FASTENER AT STA XFS 653.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0Feb 1, 2000 · N831AL · Doug DC873FSDR RRXA000638Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB AT THE AFT LOWER FASTENER AT STA XFS 616.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAAW DC-8 SRM 5Feb 1, 2000 · N831AL · Doug DC873FSDR RRXA000637Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT THE AFT LOWER FASTENERS AT STA XFS 660.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-Feb 1, 2000 · N831AL · Doug DC873FSDR RRXA000636Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT THE AFT LOWER FASTENER AT STA XFS 622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2Feb 1, 2000 · N831AL · Doug DC873FSDR UPS00831725Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL RIB WAS CRACKED AT XS 250. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 31, 2000 · N707UP · Doug DC871FSDR UPS00831527Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB WAS CRACKED AT XS240. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 31, 2000 · N707UP · Doug DC871FSDR TWAA0002304Rib · crackedDURING CHECK-C MAINTENANCE, THE RT WING LE RIB SRA XR5269 WAS CRACKED AT AFT END. REPLACED CRACKED CLIP PER SRM 51-01.Jan 31, 2000 · N953U · Doug DC982SDR ABXA000094Rib · crackedDURING C CHECK, FOUND A RIGHT WING TRAILING EDGE RIB ABOVE THE INBOARD FIXED VANE CRACKED. REPAIRED RIB IAW ABX REA D957-35354.Jan 31, 2000 · N929AX · Doug DC931SDR ABXA000093Rib · crackedDURING C CHECK, FOUND A RIGHT WING TRAILING EDGE RIB ABOVE THE INBOARD FIXED VANE CRACKED. REPLACED RIB IAW DC9 SRM 51-30-2 AND 51-30-5.Jan 31, 2000 · N929AX · Doug DC931SDR UPS00831550Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E RIB WAS CRACKED AT XS256.25. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 28, 2000 · N707UP · Doug DC871FSDR UPS00831722Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB WAS CRACKED AT XFS 772.5. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769471 AND SRM 51-1-20D, 51-1-21.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831682Rib · crackedINSPECTION TYPE:C123 LEFT WING L/E UPPER RIB IS CRACKED AT XS250.089. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831518Rib · crackedINSPECTION TYPE:C123, LT WING L/E HAD RIBS CRACKED AT XFS 628.75 UPPER AND LOWER, AND XFS 616.25 LOWER. REPAIRED PER SRM 57-2-0 FIG 2.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831452Rib · crackedINSPECTION TYPE:C1, RT WING L/E NR 3 STUB WING UPPER WAS CRACKED AT XS 256.339. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2, 51-1-20D, 51-1-21.Jan 26, 2000 · N703UP · Doug DC871FSDR UPS00831448Rib · crackedINSPECTION TYPE:C1, RT WING L/E NR 3 STUB WING UPPER RIB CRACKED AT XS227.335. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2, 51-1-21, 51-1- 20D.Jan 26, 2000 · N703UP · Doug DC871FSDR UPS00831447Rib · crackedINSPECTION TYPE:C1, RT WING L/E NR 3 STUB WING UPPER RIB CRACKED AT XILD .7095. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-3-1 FIG 3, 51-1-21, 51-1-20D.Jan 26, 2000 · N703UP · Doug DC871FSDR UPS00831446Rib · crackedINSPECTION TYPE:C1, RIGHT WING NR 3 STUB WING UPPER WAS CRACKED AT XFS207.5. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-3-0 FIG 3, 51-1-21, 51-1-20D.Jan 26, 2000 · N703UP · Doug DC871FSDR DHL200080309CRib · crackedAT C-CHECK, RT WING L/E NR 522B ACCESS PANEL SHOWS RIB CRACKED 3 INCHES AT STA XFS 347.730. FABRICATED DOUBLER IAW SRM 57-2-0 (2024730.63A6). TREATED AND PRIMED IAW SRM 51-1-2B/P6 344. INSTALLED DOUBLER WITH FASTENERS IAW SRM 51-1-200 PG 69. WORK DONE ON NJan 25, 2000 · N803DH · Doug DC873FSDR UPS00831538Rib · crackedINSPECTION TYPE:C123, LEFT WING CENTER L/E UPPER RIB CRACKED AT XS484.895. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 25, 2000 · N707UP · Doug DC871FSDR UPS00831520Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E HAD RIBS CRACKED AT XFS 285.25 AND XFS 341.5. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 25, 2000 · N707UP · Doug DC871FSDR UPS00831526Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIB CRACKED AT XILD.7095. REPAIRED IAW SRM 57-2-0 FIG 2.Jan 24, 2000 · N707UP · Doug DC871FSDR UPS00831525Rib · crackedINSPECTION TYPE:C123 LEFT WING L/E. UPPER RIB CRACKED AT XS227.335 REPAIRED I.A.W. SRM 57-2-0 FIG. 2Jan 24, 2000 · N707UP · Doug DC871FSDR UPS00831524Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E AT STA XS 250.089 UPPER RIB WAS CRACKED. REPAIRED PER SRM 57-2-0 FIG 2.Jan 24, 2000 · N707UP · Doug DC871FSDR RRXA000632Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RT WING L/E RIB UPPER ARM AT STA XFS 697.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000631Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 678.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000630Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 660.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873FSDR RRXA000629Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB UPPER ARM AT STA XFS 653.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Jan 23, 2000 · N831AL · Doug DC873F
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