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 AUS20020450Rib · damaged(AUS) RT WING ROOT RIB FAULTY DUE TO MOISTURE INGRESS. FOUND DURING INSPECTION IAW AD/CA25/7-1.SDR DHL2002807535Fitting · crackedITEM REF.: N/R 2507 RT WING- CENTER L/E INTERIOR - FITTING WITH 2.5 INCH CRACK IN IT , STA. XW456.250CORR: R&R FITTING IAW SRM 51-1-20D PG. 9SDR 2002FA0000493Rib · crackedLOCATED AND MARKED END OF CRACKS AT WS 81.174 ON RIGHT AND LEFT WINGS IN THE LOWER RADIOUS OF THE WING RIBS. BOTH CRACKS WERE APPROX. 6 INCHES LONG AND FOLLOWED THE RADIUS FORWARD AND AFT.SDR ASOA02200Rib · crackedDURING HANGAR MAINTENANCE IN TXK, THE RIGHT WING INBOARD FLAP INBOARD TRACK SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR. (M)SDR EIA2002026Bulkhead · crackedFOUND RIGHT WING TRAILING EDGE CAVITY, LOWER BULKHEAD CHORD CRACKED AT APPROXIMATELY WBL 245, BELOW INTERSECTION OF NR 7 AND NR 8 SPOILERS. REMOVED DAMAGE AND REPAIRED PER ECRA 479-57-160-2. (M)SDR DHL2002807529Rib · crackedITEM: REF.: N/R 2045 RT. WING L/E UPPER SKIN INNER SECTION - RIB CRACKED .250 @ STA XFS 672.500CORR.: STOP DRILLED CRACK IAW SRM 57-2-0 FIG. 2 FABRICATED DOUBLER (2024T3 AL .060) IAW SRM 57-2-0 FIG.2 , CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B , INSTALLED SDR DHL2002807521Former · crackedITEM: REF.; N/R 1897 LT. WING L/E FORMER CRACKED .250 @ STA. XFS695.000CORR: STOP DRILLED CRACK I/A/W SRM 57-2-0 FIG.2 - FABRICATED REINFORCING ANGLE( 2024 T3 .063)I/A/W SRM 57-2-0 FIG. 2 - CLEANED TREATED , AND PRIMED ANGLE I/A/W SRM 51-1-8B - INSTALLED REINFSDR DHL2002807520Former · crackedRIGHT WING L/E FORMER CRACKED .500 AT STA XFS835.000. STOP DRILLED FORMER IAW 57-2-0 FIG 2. FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.SDR DHL2002807522Rib · crackedITEM: REF.; N/R 2042 RT. WING L/E UPPER INNER SKIN - RIB CRACKED .250 @ SAT. XFS628.75OCORR: STOP DRILLED CRACK I/A/W SRM 57-2-0 , FIG. 2 - FABRICATED REINFORCING ANGL ( 2024 T3 AL .063) I/A/W 57-2-0 FIG. 2 CLEANED , TREATED ,A ND PRIMED I/A/W SRM 51-1-8B . SDR DHL2002807517Rib · crackedRIGHT WING OUTBOARD L/E UPPER INNER SURFACE - RIB CRACKED .250 AT STA 660.000. STOP DRILLED CRACK IAW SRM 57-2-0 FIG 2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.SDR DHL2002807516Rib · crackedITEM: REF.: N/R 2041 RT. WING OUTBD. L/EINNER SURFACE - RIB CRACKED .250 @ SAT. XFS 622.500CORR.; STOPPED DRILLED CRACK I/A/W SRM 57-2-0 FIG.2 FABRICATED RE-INFORCING ANGLE ( 2024-T3 AL , .063 ) I/A/W/ SRM57-2-0 FIG.2 CLEANED , TREATED AND PRIMED REINFORCING ASDR ASOA02203Rib · crackedDURING HANGAR MAINTENANCE IN TXK, THE RIGHT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW ASA EO120-57-0123. THIS EO REFERENCES SST-3404/00 AND SRM 57-20-07. (M)SDR ASOA02203SRib · crackedDURING HANGER MAINTENANCE, THE RIGHT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW EO. THIS EO SETS THE FLIGHT LIMIT NOT TO EXCEED 400 FLIGHT HOURS BEFORE THE PERMANENT REPAIRSDR ASO2002F00016Rib · crackedDURING HANGER MAINTENANCE, THE RT INBOARD FLAP INBOARD FIXED TRACK SUPPORT WAS CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR TO THE FLAP TRACK SUPPORT RIB IAW THIS EO SETS THE FLIGHT LIMIT NOT TO EXCEED 400 FLIGHT HOURS BEFORE THE PERMANENT REPAIR IS DONSDR DHL2002807509Track · crackedITEM: REF.: 1347 AFT CARGO COMPT. AFT DOOR -TRACK SUPPORT FITTING BROKENCORR: REPLACED TRACK SUPPORT FITTING OF "D" BELLY DOOR / TIGHTENED BOLTS I/A/W 51-1-3 PG. 2A REFER TO N/R 2386 FOR OPS CK.NOTE: RII ITEMSDR DHL2002807508Former · crackedRIGHT WING L/E - FORMER WITH .250 CRACK IN IT AT STA XFS822.000. STOP DRILLED CRACK IAW 57-2-0 FIG 2, FABRICATED AND INSTALLED DOUBLER IAW 57-2-0 FIG 2.SDR DHL2002807507Rib · crackedITEM: REF.: N/R 2050 RT. WING L/E UPPER INNER RIB .250 CRACK @ STA.XFS760.000 CORR: STOP DRILLED I/A/W 57-2-0 FIG. 2 FABRICATED DOUBLER I/A/W 57-2-0 FIG 2 ( 2024T3 AL .063)CLEANED , TEATED , AND PRIMED DOUBLER I/A/W SRM 51-1-8B . INSTALLED DOUBLER ARM @RT. WINSDR DHL2002807506Rib · crackedITEM: REF.; N/R 2049 RT. WING L/E UPPER INNER SECTION - RIB CRACKED .250 @ STA. XFS 735.000CORR: STOP DRILLED CRACK I/A/W SRM 57-2-0 FIG. 2 FABRICATED DOUBLER( 2024 T3 AL .063) I/A/W57-2-0 FIG 2. CLEANED , TREATED AND PRIMED I/A/W 51-1-8B . INSTALLED DOUBLER SDR DHL2002807505Rib · crackedITEM: REF.; N/R 2048 RT. WING L/E UPPER INNER SECTION - RIB CRACKED .250 @ STA. XFS 741.250CORR: PERFORMED STOP DRILL I/A/W 57-2-0 - FABRICATED DOUBLER (2024T3 AL .063) I/A/W 57-2-0 FIG 2 - CLEANED , TREATED AND PRIMED I/A/W 51-1-8B - INSTALLED NEW DOUBLER SDR DHL2002807504Rib · crackedITEM: REF.: N/R 2047 RT. WING L/E UPPER INNER SECTION - RIB .250 CRACKED @ STA. XFS 722.500CORR: PERFORMED STOP DRILL I/A/W SRM57-2-0 FIG. 2 - FABRICATED DOUBLER (2024T3 AL .063) I/A/W SRM57-2-0 - CLEANED, TREATED AND PRIMED I/A/W 51-1-8B - INSTALLED DOUBLERSDR DHL2002807503Rib · crackedRT WING L/E UPPER INNER SKIN RIB CRACKED .250 AT STA. XFS 860.00. PERFORMED STOP DRILL, FABRICATED DOUBLERS, CLEANED , TREATED AND PRIMED.SDR GTIA020344Rib · crackedFTW - FOUND RIGHT LOWER CENTER WING CRACKED AT THE NR 1 RIB, FROM DOOR JAMB. REMOVED NR 1 RIB CRACKED. FORMED INNER DOUBLER. LOCATED AND DRILLED. INSTALLED REPAIR PARTS. INSTALLED NR 1 RIB RIGHT LOWER CENTER WING. (M)SDR GTIA020381Former · corrodedFTW - FOUND RIGHT WING CORRODED AT NOSE CAP SECTION ATTACH, FORMERS VORTILON. FORMED FORMER. DRILLED AND LOCATED. INSTALLED ATTACHED FORMED ANGLE. (M)SDR GTIA020380Rib · corrodedFTW - FOUND RIGHT LOWER CENTER WING CORRODED AT RIB NR 8, FROM MLG DOOR JAMB. REMOVED CORROSION. RIB SPLICE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF THE RIB SPLICE. FABRICATED NEW SECTION OF RIB SPLICE AND REPAIR. INSTALLED RIB SPLICE AND DOUSDR AWXA200200313Rib · crackedYWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON LT WING GEAR SUPPORT RIB 5, HOLE NR 82. MAINTENANCE OVERSIZED HOLE TO AND INSTALLED NEW FASTENER IAW AWA ER 26-5721-02093-TB2.SDR ASOA02202Rib · crackedDURING A HANGAR INSPECTION IN TXK, THE RIGHT INBOARD FLAP SUPPORT RIB WAS FOUND TO BE CRACKED. MAINTENANCE INSTALLED A TEMPORARY REPAIR IAW ASA EO120-57-0122. THIS EO REF SST-3404/00 AND SRM 57-20-07. (M)SDR UPS02837909Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-2-0 FIG 2.SDR UPS02837901Rib · crackedINSPECTION TYPE:C1 LT WING T/E UPPER RIB IS CRACKED AT XRS 247. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2.SDR 2002FA0000346Rib · crackedNR 8 RIB, LT WING SIDE BRACE LOCATION HAD CRACK THAT PROPAGATED THE FULL UPPER AREA OF THE SIDE BRACE. THE FORWARD ATTACH BOLT WAS MISSING AND EVIDENCE OF SPINNING ON THE SURFACE OF THE RIB. AFT BOLT WAS HELD BY 2 THREADS. INSPECTED AREA AT ANNUAL.SDR 02FDEA00129Rib · crackedRIGHT WING L/E COMPT RIB FOUND CRACKED AT STA XORS 694 APPROX 3 INCHES. REMOVED AND REPLACED RIB PER DWG ARB 2922.SDR MWEA020108Rib · corrodedLEFT WING FUEL TANK STATION XRS 164, RIB HAS LIGHT CORROSION IN AREA ON OUTBOARD SIDE FROM AFT SPAR TO STRINGER. COMPLIED WITH PER BOEING TELEX MWX-ORD-02-00056H.SDR MWEA020106Rib · corrodedRIGHT WING TANK -XRS 189 WING RIB LOWER CAP HAS LIGHT CORROSION ON LOWER SURFACE FROM STRINGER 17 TO 13. BLENDED OUT AREA TO 1.0 INCH RADIUS IAW DAC TELEX MWX-ORD-02-00051H.SDR MWEA020105Rib · corrodedRIGHT WING TANK -XRS 189 WING RIB LOWER CAP HAS LIGHT CORROSION ON UPPER INBOARD SURFACE FROM FORWARD SPAR TO STRINGER 19. BLENDED OUT AREA TO 1.0 INCH RADIUS IAW BAC TELEX MWX-ORD-02-00051H.SDR ABXA010718Bulkhead · crackedRIGHT WING LEADING EDGE BULKHEAD CRACKED AT LOWER FASTENER ON INBOARD SIDE OF NR 2 SLAT TRACK. REPAIRED AREA IAW DC-9 REA D957-43261.SDR UPS02837604Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR 2002FA0000129Rib · crackedDURING A SHCEDULED INSPECTION, IT WAS NOTED THAT THE RIGHT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-2 (RCWS 26.85) HAD A CRACK ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45) AND EXTENDING APPROXIMATELY 1.5 INCH AFT OF THE SPAR. AFTERSDR 2002FA0000128Rib · crackedDURING A SHCEDULED INSPECTION, IT WAS NOTED THAT THE LEFT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-1 (LCWS 26.85) HAD A CRACK ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45) AND EXTENDING APPROXIMATELY 1.5 INCH AFT OF THE SPAR. AFTER SDR 2002F00157Rib · crackedFOUND LEFT WING STATION 453 HAS A CRACKED RIB AT THE FORWARD VENT STRINGER FORWARD ATTACH BOLT. (M)SDR 2002FA0000127Rib · crackedDURING A SHCEDULED INSPECTION, IT WAS NOTED THAT THE RIGHT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-2 (RCWS 26.85) HAD A CRACK ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45) AND EXTENDING APPROXIMATELY 1 INCH AFT OF THE SPAR. AFTER RSDR 2002FA0000126Rib · crackedDURING A SHCEDULED INSPECTION, IT WAS NOTED THAT THE LEFT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-1 (LCWS 26.85 INCHES) HAD A CRACK ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45 ) AND EXTENDING APPROXIMATELY 1 INCH AFT OF THE SPAR. SDR AWXA200200031Rib · damagedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK MAINTENANCE DISCOVERD A HOLE DRILLED THROUGH INBOARD L/H MIDFLAP LOWER SURFACE INTO THE FLAP TRACK SUPPORT RIB AT APPROXIMATELY WBL 116. DAMAGE APPEARED TO BE FROM A DRILLED OUT GREASE FITTING. MAINTENANCE REMOVED ISDR DHL2002805010Rib · crackedN/R 2396LT. WING , CTR. LEADING EDGE, UPPER SKIN RIB (FORMER) TRAILING EDGE CRACKED 1" @ STA. XFS416.500SDR DHL2002805006Rib · crackedN/R 2299LT. WING CTR. L/E LOWER SKIN RIB T/E CRACKED BTWN XFS329.000 & 347.750SDR DHL2002805005Rib · crackedN/R 2297LT. WING CTR. LEADING EDGE LOWER SKIN RIB T/E CRACKED 1" BTW. XFS404.000 & XFS422.750SDR DHL2002805004Rib · crackedN/R2301LT. WING CTR. L/E UPPER SKIN RIB T/E CRACKED 1" BTWN. 291.500 AND 250SDR DHL2002805003Rib · crackedN/R # 2300 LT. WING CTR. L/E LOWER SKIN RIB T/E 1" CRACK BTWN XFS 291.500-310.250SDR DHL2002805002Rib · crackedLT. WING CENTER LEADING EDGE UPPER SKIN RIB TRAILING EDGE CRACKED 2" BETWEEN STA. XFS416 AND XFS435.789SDR DHL2002805001Rib · crackedLT. WING CENTER LEADING EDGE UPPER SKIN RIB TRAILING EDGE CRARACKED @ XFS 329.000SDR DHL2002805024Rib · crackedN/R 1992RT. WING LEADING EDGE INNER RIB (FORMER) CRACKED 1" @ STA. XFS601.000SDR DHL2002805012Rib · crackedN/R 1991RT. WING L/E UPPER RIB (FORMER) CRACKED .500 @ XFS 701.000
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