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.
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
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 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.SDR SWAA073898Rib · crackedDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING LOWER RIB CHORD CRACKED AT STA 135.5. REPAIRED CHORD PER ACO.SDR 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 REMOVESDR 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.SDR 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 ISDR 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.SDR 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.SDR 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.SDR 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 SDR 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.SDR 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.SDR 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 DSDR 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.SDR 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 MISALIGSDR 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.SDR 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 MISDR 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.SDR 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.SDR 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 006SDR 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.SDR 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.SDR 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 APPROVEDSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR SWAA073114Rib · crackedDURING SCHEDULED 10Y CHECK, FOUND RIGHT WING RIB CRACKED AT STA 135.5, BETWEEN S2 AND S3. REPAIRED RIB PER ACO.SDR DLM88070788Rib · crackedCRACKED RIB ON LT WING OUTBD REMOVABLE TRAILING EDGE. REPAIRED PER SRM 57-01 FIG 3 ON N/R T0058787 HMV/GDL.SDR 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 4SDR 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.SDR DLM88070789Rib · crackedCRACKED RT WING OUTBD REMOVABLE TRAILING EDGE RIB. REPAIRED PER SRM 57-01 FIG 3 ON N/R T0058792 HMV/GDL.SDR NOCA13007Rib · crackedRIB CRACKED AFT OF NR 6 SLAT AT REAR SPAR. REPLACED RIB SEALED AND PAINTED AS PER 57-11-00-1.SDR NOCA12907Rib · crackedFIXED L/E RIB CRACKED AT REAR SPAR. REPLACED AIR LOAD RIB AND SUPPORT CLIP PER SRM 51-10-02.SDR 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 MISALIGSDR 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)SDR 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)SDR 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.SDR 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.SDR 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.SDR AMWA7026DRib · corrodedBIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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