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 2005FA0000557Rib · crackedDURING VISUAL INSPECTION, A SMALL CRACK WAS FOUND IN THE RT NOSE RIB P/N-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCHES LONG), WAS FOUND ON THE RIB P/N-78475-009 AND -008. THESE RIBS ARE INCLUDED IMar 21, 2005 · N701ER · Piper PA28R201SDR 2005FA0000579Rib · crackedDURING A 100HR. INSPECTION, A SMALL CRACK WAS FOUND IN THE RT. NOSE RIB PN-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCES LONG), WAS FOUND ON THE RIB PN-78475-009 AND -008. THESE RIBS ARE INCLUDED IMar 20, 2005 · N705ER · Piper PA28R201SDR UPS05844249Rib · crackedINSPECTION TYPE: C2, LEFT L/E UPPER RIB CRACKED .5 INCH LONG AT STA 811. REPAIRED LT L/E UPPER RIB IAW DC-8 SRM 57-2-0 FIG 2 AND SRM 51-1 20D.Mar 19, 2005 · N819UP · Doug DC873FSDR UPS05844248Rib · crackedINSPECTION TYPE: C2, LT L/E UPPER RIB CRACKED .25 INCH LONG AT STA 782. REPAIRED LEFT L/E UPPER RIB IAW DC-8 SRM 57-2-0 FIG 2 AND SRM 51-1-20D.Mar 19, 2005 · N819UP · Doug DC873FSDR UPS05844252Rib · crackedINSPECTION TYPE: C2, RIGHT WING L/E UPPER RIB CRACKED .5 INCH LONG AT STA XRS 727, VIEW FROM PANEL 518A. REPAIRED RIGHT WING L/E UPPER RIB AT STA XRS 727 IAW DC-8 SRM 57-2-0.Mar 18, 2005 · N819UP · Doug DC873FSDR A6WA200540111Rib · crackedRIGHT MLG WHEEL WELL AT WS 48.3O FS 523.8 BATTERY RIB IS CRACKED APPROX 1 INCH. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW BOMBARDIER INC REO 601R-57-57-046 REV B. (M)Mar 16, 2005 · N415AW · Cndair CL6002B19SDR A6WA200540112Rib · crackedLT MLG WHEEL WELL AT WS 48.30 FS 523.8 BATT RIB IS CRACKED APPROX 1 INCH.Mar 16, 2005 · N415AW · Cndair CL6002B19SDR A6WA200540122Rib · crackedLT HAND MLG WHEEL WELL AT SS 48.30, FS 523.8, BATT RIB IS CRACKED 1.2500 INCH LONG. REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19SDR USAA050411Rib · crackedCLT - Q6 - RIB, (2 EA- 1.5 INCH AND .3750 INCH) CRACK. LT WING RIB AT WS 505 UPPER FLANGE RADIUS 20 INCHES FROM L/E OF RIB. FABRICATED REPAIR DOUBLER IAW EA. (K)Mar 10, 2005 · N442US · Boeing 7374B7SDR DHL2005782522Rib · crackedRIB CRACKED ON FWD BOTTOM EDGE, RT WING LE WS 130. REMOVED NR 4 K-FLAP FOR ACCESS IAW B727 MM 27-81-01. STOP DRILLED CRACK IAW 727 SRM 51-10-1 AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO NR 900861 DIM. 6" BY 1 3/4" IAW 727 SRM 57-20-2 FIG 1 AND 51-40-3 FIG 1Mar 10, 2005 · N782DH · Boeing 727227SDR 05FDEA00464Rib · gougedCOMPLY WITH EA 8-5710-55459, REWORK OF GOUGES IN WING LEADING EDGE RIB PN NRD6037-1. CLOSING ACTION ON 03/09/05. ON NR S00019. COMPLIED WITH EA 8-5710-55459.Mar 9, 2005 · N369FE · Doug DC1010SDR 05FDEA00425Rib · crackedRT WING 4 IN IB OF RIB 30 L/E AREA AFT PANEL LANDING IS CRACKED REF N00636. REMOVED AND REPLACED LANDING IAW SRM 51-40-21 AND 51-72-10 AND DRW A57243955.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00426Rib · crackedRT WING L/E UPPER SIDE OF PANEL LANDING, LANDING FOR PANEL HAS 2 EA CRACKS AT 11 IN I/B OF RIB 14 AND 11 IN O/B OF RIB 14 REF N00631. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A57244165.Mar 8, 2005 · N446FE · Airbus A310SDR GTIA050094Frame · crackedFROM C/O 0155770 RT WING L/E 2 EA FORMERS ST APPROX STA 351 CRACKED. FABRICATED DOUBLER IAW SRM. HEAT TREATED 2 EA DOUBLER IAW SRM. TREATED AND PRIMED INSTALLED REPAIR DOUBLER IAW SRM. LP NR 01476783. (K)Mar 7, 2005 · N821NK · Doug DC982SDR ASOA05203Rib · crackedDURING A C-CHECK IN MCN, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)Mar 5, 2005 · N904EV · Cndair CL6002B19SDR IXXA0500139SRib · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBOARD PYLON STUB WING N 4 RIB EXTENDED LEADING EDGE CRACK DAMAGE AT STA XOLDO 67.750. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGE. FABRICATED NEW RIB. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREMar 4, 2005 · N821BX · Doug DC871FSDR SWIA200515654Rib · crackedLEFT BATTERY RIB IN MLG BAY CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 601R-57-51-046.Mar 3, 2005 · N417SW · Cndair CL6002B19SDR SWIA200515653Rib · crackedRIGHT BATTERY RIB IN MLG BAY CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-57-51-046.Mar 3, 2005 · N417SW · Cndair CL6002B19SDR DHL2005781562Rib · crackedDURING A C-CHECK, RT WING NR 6 SLAT I/B RIB AT ACTUATOR ROD ATTACH POINT IS CRACKED. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MATERIAL USED 2024 T3, .040 PO 9002012 DIM15 X 5.5 INCH IAW B727 SRM 57-50-2 FIG 2 AND 51-20-1 FIG 7. ALODINE AMar 3, 2005 · N781DH · Boeing 727227SDR UPS05644029Rib · crackedINSPECTION TYPE: C LEFT WING I/B AILERON I/B HINGE RIB IS CRACKED AT UPPER TRAILING EDGE ON CHORD ATTACH FASTENERS. REPAIRED I/B AILERON I/B HINGE RIB IAW UPS ER05-1834.Mar 3, 2005 · N301UP · Boeing 76734AFSDR 050606392Rib · crackedLEFT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS.Mar 1, 2005 · N639BR · Cndair CL6002B19SDR 050606391Rib · crackedRIGHT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS.Mar 1, 2005 · N639BR · Cndair CL6002B19SDR 2005FA0000397Bulkhead · crackedDURING AN ANNUAL INSPECTION, FOUND AFT BULKHEAD OF THE LT WING TIP TANK ASSY. CRACKED THROUGH FROM APPROXIMATE CENTER OF THE IB LIGHTENING HOLE HORIZONTALLY TO THE BULKHEAD IB EDGE. CRACKED AREA IS ADJACENT TO AFT ATTACH POINT FOR THE TIP TANK ASSY. AIRCRAFFeb 25, 2005 · N421CT · Cessna 421BSDR 2005FA0000396Rib · crackedDURING AN ANNUAL INSP, NOTED CRACKS IN LT AND RT WING T/E RIBS AT FORWARD END AFT SPAR ATTACHMENT POINT AREAS. AFFECTED RIBS ARE FIRST RIBS IB OF SPOILER SYSTEM ACTUATOR ATTACH POINTS. ALSO FOUND CRACKED AREA IN WING OB T/E SKIN PANEL AT ATTACHMENT POINT TO Feb 25, 2005 · N421CT · Cessna 421BSDR UPS05444007Rib · crackedINSPECTION TYPE:C RIGHT W ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB MULTI CRACKS FOUND DURING RIB INSTALLATION WITH RIVET (CRACK LENGTH 1 TO 3 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB TOP FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-5740-218Feb 22, 2005 · N676UP · Boeing 747123SDR SWAA050527Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND BOTH LT & RT WING LOWER T-CHORDS CRACKED AT WBL 135.5, BETWEEN STR 2 & 3. REPAIRED T-CHORDS PER SWA EA.Feb 22, 2005 · N507SW · Boeing 7375H4SDR DHL2005781542Rib · gougedDURING A C-CHECK, RT WING L/E CAVITY RIB GOUGED WSTA 734. REMOVED DAMAGED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE 20 24 T3 .040 9001634 (16 X 1.875 INCH) IAW B727 SRM 57-20-2 FIG 1 AND 51-20-1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW ANFeb 15, 2005 · N781DH · Boeing 727227SDR 2005UALA00155Rib · crackedRT WING L-E CAVITY AT FSS 512, UPPER RIB LOWER CHORD PREVIOUS REPAIR CRACKED AT AFT END-OUTBD OF NR 8 SLAT OUTBD ACTUATOR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. RIB REPAIRED WITH ANGLE DOUBLER.Feb 13, 2005 · N652UA · Boeing 767322SDR AU510001809Rib · crackedLT WING UPPER FORWARD PN 572001-3S AND AFT PN 572001-5S DRAG ANGLES CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW CQB03-1 REV 1. EDDY CURRENT INSPECTION REVEALED A TOTAL OF NINE CRACKS ALL AROUND 5MM (0.196IN) IN LENGTH.Feb 9, 2005 · Cessna 441SDR ASAA0580088Rib · crackedOKC - FOUND C-CHECK, RIGHT WING L/E HAS CRACKED RIB. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)Feb 7, 2005 · N960AS · Doug DC983SDR ASOA05107Rib · crackedDURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATTERY RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT BATTERY RIB ASSEMBLIES AT WLS 53.60 IAW ASA EO 600-57-039A. (M)Feb 6, 2005 · N846AS · Cndair CL6002B19SDR UPS05444006Rib · crackedINSPECTION TYPE:C RIGHT WING ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB FWD VERTICAL MOUNTING ATTACH FASTENER HOLES CRACKED (CRACK LENGTH 1 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-574Feb 5, 2005 · N676UP · Boeing 747123SDR UPS05443997Rib · crackedINSPECTION TYPE:C RIGHT WING 17 VC FLAP O/B ARM O/B RIB MOST FWD FASTENER HOLE CRACKED (CRACK LENGTH 1.25 INCH). RIGHT WING 17 VC FLAP O/B ARM O/B RIB FWD FLANGE FASTENER HOLES REPAIRED AS PER HX RS R57-41-35263 AND UPS EO B747-5740-21796-A.Feb 5, 2005 · N676UP · Boeing 747123SDR UPS05443994Rib · crackedINSPECTION TYPE:C RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE AT ROTARY ACTUATOR AFT AREA FOUND CRACKED, CRACK LENGTH .5 INCH. RIGHT WING 20VC FLAP I/B ARM O/B RIB I/B FACE REPAIRED AS PER HX RS R57-41-35254 WITH CRACKED AREA TRIMMED OFF & INSPECTED BY NDT.Feb 5, 2005 · N676UP · Boeing 747123SDR SWIA200514889Rib · crackedBATT RIB CRACKED AT UPPER FLANGE, AFT SIDE. LOCATED AT RT MLG BAY WS53-600. ITEM FOUND AT C-CHECK INSPECTION, INSTALLED REPAIR PARTS IAW REO 601R-57-51-046.Feb 3, 2005 · N589SW · Cndair CL6002B19SDR SWIA200514888Rib · crackedBATT RIB CRACKED AT UPPER FLANGE, AFT SIDE. LOCATED AT LT MLG BAY, WS 53-600. (ITEM FOUND AT C-CHECK INSPECTION) INSTALLED REPAIR IAW 601R-57-51-046.Feb 3, 2005 · N589SW · Cndair CL6002B19SDR ASAA0580072Rib · crackedOKC - DURING C-CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED. REPLACED DAMAGE. INSTALLED REPAIR ANGLE, SHIM, RADIUS, AND FILLER. (M)Jan 31, 2005 · N948AS · Doug DC983SDR ASAA0580071Rib · crackedOKC - DURING C-CHECK, WING LEADING EDGE RIB CRACKED, FROM WS XDS449 TO XDS499. REPLACED RIB. (M)Jan 31, 2005 · N948AS · Doug DC983SDR ASAA0580082Rib · crackedOKC - DURING C-CHECK, LT WING FIXED LEADING EDGE RIB LOWER L-ANGLE IS CRACKED. REPLACED ANGLE. (M)Jan 31, 2005 · N948AS · Doug DC983SDR A6WA20050033Rib · crackedLT WING STATION 53.6 BUTT RIB IS CRACKED, 1 INCH LONG IN UPPER AFT RADIUS. REPAIRED LT WING STATION 53.60, BATT RIB IAW MFG REPAIR EO 601R-57-51-046, REV B.Jan 25, 2005 · N412AW · Cndair CL6002B19SDR A6WA200540034Rib · crackedMWC 60. RT WING STATION 53.6 BUTT RIB IS CRACKED .5000 INCH LONG IN UPPER AFT RADIUS. REPAIRED RT WING STATION 53.60 BATT RIB IAW MFG EO 601R-57-51-046, REV B.Jan 25, 2005 · N412AW · Cndair CL6002B19SDR COMA0560086Rib · crackedCRACK FOUND TO BATT RIB ASSEMBLY AT WS 53.60 IN MLG BAY RIGHT HAND. REPAIRED IAW REO 601R-57-51-046.Jan 25, 2005 · N978CA · Cndair CL6002B19SDR COMA0560084Rib · crackedLEFT HAND PYLON LOWER RIB AT FS 605.00 CRACKED. REPAIRED IAW REO 601R-54-61-038.Jan 24, 2005 · N978CA · Cndair CL6002B19SDR CALA0500016Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN RIB AND DOUBLER AT LT WING LEADING EDGE INTERNALLY BETWEEN NR 9 AND NR 10 SLAT TRACK CUTOUTS, STA XRS 324. THE CRACKED RIB AND CLIP ANGLE WERE REMOVED AND A NEW RIB AND CLIP ANGLE WERE INSTALLED IAW SRM 51-10-03, 51-30-02,Jan 21, 2005 · N35836 · Doug DC982SDR 2005F00012Rib · damagedOUTBOARD RT WING RIBS DAMAGED.Jan 14, 2005 · N750DH · Boeing 7272M7SDR UPS05843756Rib · crackedINSPECTION TYPE:C3, RT WING CENTER L/E RIB CRACKED AT XFS 335.25. NDT VERIFIED CRACK TERMINATES AT RIVET HOLE REF SPM06-10-01.001. FAB 2 STACKED REPAIR ANGLES FROM SHT 7075T6-.040. INSTALLED REPAIR PER SRM 57-3-3 FIG 5, 57-2-0 FIG 2, 51-1-8, 51-1-21, 51-1-2Jan 8, 2005 · N868UP · Doug DC873FSDR 05FDEA00036Rib · corrodedACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, LT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FEDEX EA 6-5710-81827. PERFORMED NDT INSPJan 6, 2005 · N454FE · Airbus A310222SDR UPS05843933Rib · crackedINSPECTION TYPE: C, NR 4 STUB WING INBOARD L/E RIB CRACKED AT L/E. REMOVED, FABBED, AND INSTALLED NR 4 INBOARD STUB WING TAPERED FLANGE IAW DC8 SRM 51-1-21, DWG 9753297, SRM 51-1-8 AND DC8 SRM 51-1-21A.Jan 5, 2005 · N868UP · Doug DC873FSDR UPS05843753Rib · crackedINSPECTION TYPE:C3, LT WING ATTACHMENT RIB CRACKED AT XW454. CUT OUT DAMAGE, VERIFIED PER NDT SPM06-10-01.001. FABRICATED REPAIR DOUBLER FROM SHT7075-0-.100 & FILLER FROM SHT7075T6-.090 REF DWG 9753297. HEAT TREAT TO T6 PER DPS7.00-1. INSTALLED REPAIR PER Jan 5, 2005 · N868UP · Doug DC873FSDR UPS05843935Rib · crackedINSPECTION TYPE: C, RT WING O/B LEADING EDGE HAS CRACKED UPPER RIB AT STA 776. REMOVED FASTENERS, STOP DRILLED, FABBED AND INSTALLED FILLER IAW DC8 SRM 51-1-21, 57-2-0, 57-3-3 FIG 7, 57-2-0 FIG 2, 51-1-8, AND 51-1-20D.Jan 4, 2005 · N868UP · Doug DC873F
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