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 07FDEA02756Rib · crackedRT WING L/E SLAT NR 5 INBD END PORK CHOP SEAL MOUNTING PLATE DEFORMED AND CRACKED. REMOVED CRACKED RIB, FABBED NEW RIB ON TRAVLER T/682663. INSTALLED NEW RIB.Aug 3, 2007 · N254FE · Boeing 727233SDR SWAA073898Rib · crackedDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING LOWER RIB CHORD CRACKED AT STA 135.5. REPAIRED CHORD PER ACO.Aug 2, 2007 · N345SA · Boeing 7373K2SDR UPS07M50967Rib · crackedINSPECTION TYPE:C RIGHT WING NR 16 SLAT TRACK I/B RIB FITTING SUSPECTED CRACK AS MARKED. HFEC INSP C/OUT FOUND CRACK AS MARKED. RIGHT WING NR 8 EXT & RET CABLES DISCONNECTED. RIGHT WING NR 16 SLAT TRACK DOOR, ATTACHED HARDWARES & ROLLERS & SLAT TRACK REMOVEJul 30, 2007 · N290UP · Doug MD11FSDR AWXA200700981Rib · corrodedSAL - MAJOR REPAIR - C-06 CHECK - NR 5990411, CORROSION ON RIGHT WING RIB 5 FORWARD LUG, WS 2508/RIB 5. REPAIRED THE NR 5 RIGHT WING RIB 5 FORWARD LUG, WS 2508/RIB 5 IAW A320 SRM 57-26-13.Jul 29, 2007 · N633AW · Airbus A320231SDR GLBA20060966Rib · crackedLT WING RIB OB OF POWER PACK CRACKED AT (L) BRACKET APPROX. 1 INCH BY 1 INCH IN LENGTH ORIGINATING FROM RIVET HEAD. MAINTENANCE REPAIRED THE LT WING RIB OB OF HYDRAULIC POWER PACK ONE INCH CRACK AT W.S. 79.65 IAW SRM 51-70. REPAIR DIMENSION 4 INCH BY 2.7500 IJul 20, 2007 · N201GL · Beech 1900DSDR 07FDEA02503Rib · damagedCOMPLY WITH EA 7-5710-110753, RT SIDE ONLY, WINGS- (AD 90-06-09 AND AD 94-07-08) MAIN FRAME, RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-110753 RT SIDE IAW SB 727-57-0112.Jul 17, 2007 · N241FE · Boeing 727227SDR 07FDEA02502Rib · misalignedCOMPLY WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER REPAIR DEVIATIONS.Jul 17, 2007 · N241FE · Boeing 727227SDR 07FDEA02501Rib · misalignedWING RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS EA NR 7-5710-110754. COMPLIED WITH EA NR 7-5710-110754 WING, AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS.Jul 17, 2007 · N241FE · Boeing 727227SDR DHL2007804500Rib · crackedNR 1 STUB WING RIB JOINT ANGLE CRACKED 0.750", STA XFS 529.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075"0" 0.080") IAW DWG NR 9753297. HEAT TREATED FROM AL7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED Jul 16, 2007 · N804DH · Doug DC873FSDR CWQR200705Closeout Panel · crackedDURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED. (3) CRACKS WERE FOUND BEGINING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STRAIGHT UP THE PANEL. AN SCR HAS BEEN SUBMITTED TO MFG AIRCRAFT UNDER NR 303303.Jul 16, 2007 · N694QS · Cessna 560XLSDR CWQR200704Closeout Panel · crackedDURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED. (3) CRACKS WERE FOUND BEGINNING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STRAIGHT UP THE PANEL. AN SDR HAS BEEN SUBMITTED TO AIRCRAFT UNDER NR 303303.Jul 16, 2007 · N694QS · Cessna 560XLSDR UPS07M50467Rib · crackedINSPECTION TYPE:C RIGHT WING FIXED WING L/E INTERIOR AREA APPROX STA XOS 667 FOUND RIB CRACKED. CRACKED RIB REMOVED (REF C/N: MD072549, STEP FOR WORK DETAILS). NEW RIB FAB PER DWG ARB2930-20. RIB HEAT - TREATED PER DPS 7.00-1 & HARDNESS VALUE HRB 81.7 PER DJul 14, 2007 · N289UP · Doug MD11FSDR EIA2007146Rib · looseLEFT WING LEADING EDGE HAS RIVETS LOOSE AT FORMER RIB INBOARD OF NR 3 KREUGER FLAP. REPAIRED LEFT WING LEADING EDGE AT FORMER RIB INBOARD OF NR 3 KREUGER FLAP PER ECRA 488-57-020-2.Jul 13, 2007 · N488EV · Boeing 747230BSDR 2007FA0000929Bulkhead · misalignedCONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A. THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE. IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGJul 12, 2007 · N373ES · Cessna 172RSDR DL76S070849Rib · crackedRT WING LES 688 AREA RIB SUPPORT FWD END CRACKED. RT WING LES 688 AREA RIB SUPPORT REPAIRED PER SRM 57-41-01 FIGURE 201 REPAIR 4.Jul 3, 2007 · N127DL · Boeing 767332SDR 07FDEA02354Rib · crackedRT WING INBD L/E FORMER WEB CRACKED AT AFT UPPER AREA INBD SIDE. FORMER LOCATED AT O/B END OF NR 6 FLAP. FABRICATED REPAIR DOUBLER, ON RT WING INBD L/E FORMED WEB TREATED AND PRIMED, AND INSTALLED IAW B727 SRM 51-40-2 FIG 1, 51-10-2, 51-30-2, CLASSIFIED MIJul 2, 2007 · N481FE · Boeing 727227SDR UPS07850053Rib · crackedINSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE AT STA XFS 641 IS CRACKED. STOP DRILLED CRACK AT STA XFS 641 L/WING LEADING EDGE IAW SRM 57-2- 0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LEADING EDGE STA XFS 641 IAW SRM 57-03-01 FIG 006.Jun 23, 2007 · N705UP · Doug DC871FSDR UPS07850052Rib · crackedINSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE RIB CRACKED AT STA XFS 672. STOP DRILLED CRACK AT STA XFS 672 L/WING LEADING EDGE IAW SRM 57-2- 0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 672 L/WING LEADING EDGE IAW SRM 57-03-01 FIG 006.Jun 23, 2007 · N705UP · Doug DC871FSDR UPS07850051Rib · crackedINSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE UPPER RIB CRACKED AT XFS 678. STOP DRILLED CRACK AT STA XFS 678 L/WING LEADING EDGE IAW SRM 57-02-00-0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 678 L/WING LEADING EDGE IAW SRM 57-03-01-0 FIG 006Jun 23, 2007 · N705UP · Doug DC871FSDR UPS07850050Rib · crackedC3 L/WING LEADING EDGE OUTBD LWR RIB CRACKED AT STA XFS 772. STOP DRILLED CRACK ON RIB AT STA XFS 772 L/WING LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 772 L/WING LEADING EDGE IAW SRM 57-03-01-0 FIG 007.Jun 23, 2007 · N705UP · Doug DC871FSDR UPS07850195Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 697. STOP DRILLED CRACK AT XFS 697 RIGHT WING IAW SRM 51-1-21. INSTALLED DOUBLER IAW SRM 57-03-01 AND 57-02-00.Jun 22, 2007 · N705UP · Doug DC871FSDR DL76S070778Rib · crackedDURING ACCOMPLISHMENT OF SIP EO, THE LHS WING FRONT SPAR AT RIB NR 8 WAS FOUND CRACKED AT A FASTENER HOLE. THE CRACK WAS APPROXIMATELY 0.030 INCH IN LENGTH. THE SUBJECT HOLE FROM WHICH THE CRACK EMANATED WAS ALREADY BEYOND THE EA ALLOWABLES. BOEING APPROVEDJun 22, 2007 · N127DL · Boeing 767332SDR UPS07850079Rib · crackedINSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 360. STOPPED DRILLED CRACKED RIB AT R/WING L/E STA XFS 360 IAW SRM 57-03 -03-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING STA XFS360 IAW SRM 57-03-03-0 FIG 2.Jun 22, 2007 · N705UP · Doug DC871FSDR UPS07850078Rib · crackedINSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 461 STOPPED DRILLED CRACK RIB AT STA XFS 461 IAW SRM 57-03-03-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 461 IAW SRM 57-03-0 3-0 FIG 7.Jun 22, 2007 · N705UP · Doug DC871FSDR UPS07850077Rib · crackedINSPECTION TYPE:C3 L/WING OUTBD L/E LWR RIB CRACKED AT STA XFS 734. STOPPED DRILLED CRACKED RIB AT L/WING LE STA XFS 734 IAW SRM 57-02- 0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LE STA XFS 734 IAW SRM 57-03-03-0 FIG 7.Jun 22, 2007 · N705UP · Doug DC871FSDR UPS07850076Rib · crackedINSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 816. STOPPED DRILLED CRACK AT R/WING L/E STA XFS 816 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING L/E STA XFS 816 IAW SRM 57-03-03-0 FIG 7, AND SRM 57-02-00-0 FIG 2.Jun 22, 2007 · N705UP · Doug DC871FSDR UPS07850075Rib · crackedINSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 734. STOP DRILLED CRACK ON R/WING UPPER OUTBD L/E AT STA XFS 734 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 734 R/WING L/E IAW SRM 57-03-03-0 FIG 7.Jun 22, 2007 · N705UP · Doug DC871FSDR USAA070477Rib · crackedLEFT WING RIB STA 135.5 AFT END JUST BEFORE REAR SPAR HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PER EA 98713, DEFECT SIZE: .625 INCH.Jun 22, 2007 · N418US · Boeing 737401SDR SWAA073114Rib · crackedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING RIB CRACKED AT STA 135.5, BETWEEN S2 AND S3. REPAIRED RIB PER ACO.Jun 21, 2007 · N653SW · Boeing 7373H4SDR DLM88070788Rib · crackedCRACKED RIB ON LT WING OUTBD REMOVABLE TRAILING EDGE. REPAIRED PER SRM 57-01 FIG 3 ON N/R T0058787 HMV/GDL.Jun 20, 2007 · N947DL · Doug MD88SDR 07FDEA02229Rib · crackedLT WING FIXED LEADING EDGE CAVITY AT XORS = 492 RIB STIFFENER FOUND CRACKED. [07-09-07] REMOVED CRACKED RIB STIFFENER AND FABRICATED NEW RIB STIFFENER AS PER DOUGLAS DRAWING ARB2931. INSTALLED NEW RIB STIFFENER AT LT WING FIXED LEADING EDGE CAVITY AT XORS 4Jun 20, 2007 · N575FE · Doug MD11FSDR 07FDEA02219Rib · crackedRIGHT WING FIXED LEADING EDGE RIB FOUND CRACKED AT XOS 911. [07-06-07] CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW RIB FABRICATED PER DOUGLAS DRAWING ARB2921. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11FSDR DLM88070789Rib · crackedCRACKED RT WING OUTBD REMOVABLE TRAILING EDGE RIB. REPAIRED PER SRM 57-01 FIG 3 ON N/R T0058792 HMV/GDL.Jun 19, 2007 · N947DL · Doug MD88SDR NOCA13007Rib · crackedRIB CRACKED AFT OF NR 6 SLAT AT REAR SPAR. REPLACED RIB SEALED AND PAINTED AS PER 57-11-00-1.Jun 17, 2007 · N765NA · Boeing 767306SDR NOCA12907Rib · crackedFIXED L/E RIB CRACKED AT REAR SPAR. REPLACED AIR LOAD RIB AND SUPPORT CLIP PER SRM 51-10-02.Jun 17, 2007 · N765NA · Boeing 767306SDR 2007FA0000924Bulkhead · mislocatedCONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A. THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE. IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGJun 16, 2007 · N2630U · Cessna 172RSDR A6WA200740318Rib · crackedLT WING STR 53.60 BATTERY RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K)Jun 16, 2007 · N434AW · Cndair CL6002B19SDR A6WA200740317Rib · crackedRT WING STR 53.60 BATT RIB IS CRACKED 1.0 INCH ON UPPER AFT CORNER. MAINTENANCE REPAIRED IAW REO 601R-57-51-046. (K)Jun 16, 2007 · N434AW · Cndair CL6002B19SDR 07FDEA02161Rib · crackedLT WING LEADING EDGE RIB AT XOS 584 FOUND CRACKED. [06-29-07] REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. NEW FORMER FABRICATED AS PER DOUGLAS DWG ARB2931. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jun 16, 2007 · N607FE · Doug MD11FSDR 07FDEA02152Rib · crackedRT WING LEADING EDGE RIB NEAR XOS 762 FOUND CRACKED. [06-29-07] REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. RIB FABRICATED AS PER DOUGLAS DRAWING NR ARB2923. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jun 15, 2007 · N607FE · Doug MD11SDR 07FDEA02138Rib · crackedLT WING STATION XORS 346 STRINGERS 42-43 AND 43-44 LWR RIB CHORD CRACKED IN TWO PLACES IN THE VERTICAL LEG REPAIRED IAW SRM 57-20-00 FIG 27 SHEET 3 VOL 1.Jun 15, 2007 · N387FE · Doug DC1010SDR AMWA7026DRib · corrodedBIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R.Jun 12, 2007 · N126YV · Beech 1900DSDR AMWA7026ARib · corrodedBIO CORROSION RT WING RIB AT WS125.00; AREA NEAR THE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW A REPORT 6702-4 REV 1R.Jun 12, 2007 · N126YV · Beech 1900DSDR UPS07849961Rib · crackedINSPECTION TYPE:C3 LEFT WING CENTER LEADING EDGE LOWER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-3-3 FIG 007, 51-1-20D.Jun 10, 2007 · N810UP · Doug DC873FSDR UPS07849975Rib · crackedINSPECTION TYPE:C3 LEFT WING CENTER L/E RIB PUNCTURED AND CRACKED AT STA SX515. REMOVED AND REPLACED CRACKED RIB AT LEFT WING STA XS515 IAW SRM 57-2-0 FIG 2, AND SRM 57-3-03 FIG 4.Jun 9, 2007 · N810UP · Doug DC873FSDR UPS07849960Rib · crackedINSPECTION TYPE:C3 LEFT WING CENTER LEADING UPPER RIB CRACKED XS497. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 57-03-03 FIG 004, 51-1-20D.Jun 9, 2007 · N810UP · Doug DC873FSDR UPS07849959Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE STA XFS 597 INTERNAL RIB IS CRACKED AT LWR END. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D.Jun 9, 2007 · N810UP · Doug DC873FSDR UPS07849962Rib · crackedINSPECTION TYPE:C3 LEFT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 796. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-00 FIG 2, 51-1-20D.Jun 8, 2007 · N810UP · Doug DC873FSDR UPS07849945Rib · crackedINSPECTION TYPE:C3 RIGHT WING CENTER LEADING EDGE UPPER RIB CRACKED AT STA XS 497. STOP DRILLED CRACKED RIB AT STA XS 497 IAW SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XS 497 IAW 57-2-0 FIG 2.Jun 8, 2007 · N810UP · Doug DC873FSDR UPS07450010Rib · corrodedINSPECTION TYPE:C LEFT WING L/E UPPER PANEL AT WS 970 FOUND BULGED UP. CORROSION BLEND OUT 0.030 X 1 X 2 INCHES LT WING L/E UPPER WS 970 UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Jun 7, 2007 · N520UP · Boeing 747212B
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