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 DHL2002805026Rib · crackedN/R0434RT. WING LEADING EDGE - UPPER RIB(FORMER) @ STA. XFS593.000 , CRACKED .500SDR DHL2002805025Rib · crackedN/R0433RT. WING.. UPPER RIB (FORMER) @ STA. 588.000 CRACKED .500SDR DHL2002805016Rib · crackedN/R 0438LH. WING L/E - RIB @ STA. XFS 603.750 , CRACKED .500SDR DHL2002805015Rib · crackedN/R 0436RH. WING L/E- UPPER RIB @ STA. XFS601.000 , CRACKED .500SDR DHL2002805014Rib · crackedN/R 0432RH. WING L/E- UPPER RIB (FORMER) @ STA. XFS 615.000 , CRACKED .500SDR DHL2002805013Rib · crackedN/R 0435RH WING L/E - UPPER RIB (FORMER) @ STA XFS608.000 , .500 CRACKEDSDR 01FDEA01104Rib · crackedRT WING LEAD EDGE RIB CRACKED WS 510, WBL 415. R&R RIB PER SRM 51-40-2.SDR 01FDEA01094Rib · crackedRIGHT WING L/E RIB CRACKED WS 491.5 WBL 398. REPAIRED RIB IAW FEDEX SRM 51-40-2.SDR DL72S011952Rib · crackedINSPECTIONS OF THE UPPER RIB CHORD ON THE RT WING AT RBL 70.5 PER BAC S/B 727-57-0112 AND AD 94-07-08 REVEALED A CRACK IN A FASTENER HOLE AT FS 760.95. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND THEN COLD WORKED. THE HOLE WAS BUSHED AND THE CHORD REINFORSDR CA011205001Rib · cracked(CAN) 3 RIBS RT, 2 RIBS LT WING FOUND CRACKED AT UPPER CORNER OF FLANGE WHERE RIB ATTACHES TO REAR SPAR. ALL RIBS LOCATED CLOSEST INBOARD AT WING ROOT, AND ALL RIBS CRACKED EXACTLY THE SAME.SDR UPS01837315Rib · crackedINSPECTION TYPE:N/A RT WING T/E RIB CRACKED AT FORWARD SURFACE VERTICAL CHANNEL AT XW33. THIRD OUTBOARD WAS PREVIOUSLY REPAIRED PER A/C ENGINEERING AMC HAS ASSIGNED INFORMATIONAL ITEM I226648 ASSIGNED.SDR AUS20011255Rib · cracked(AUS) WING RIB CRACKED. RIB SUPPORTS UNDERCARRIAGE DOWNLOCK.SDR AUS20011254Rib · cracked(AUS) WING RIB CRACKED. RIB SUPPORTS UNDERCARRIAGE DOWNLOCK.SDR ABXA010600Rib · corrodedEXFOLIATION CORROSION ON LEFT WING REAR SPAR RIB, ABOVE THE CENTER ATTACH POINT OF THE INBOARD BUTE DOOR. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-8.SDR GTIA012325Rib · crackedFTW - FOUND RIGHT WING FUSELAGE MOUNTED VERTICAL RIB, INBOARD OF TRAILING EDGE FLAP HAS A .250 CRACK ON ITS LOWER EDGE. REMOVED DAMAGE PART. FORMED ANGLE FOR REPAIR ON VERTICAL RIB. INSTALLED REPAIR ANGLE IAW DC9 SRM 51-30-2. (M)SDR GTIA012173Rib · crackedFTW - FOUND RIGHT SIDE, FUSELAGE AREA, INBOARD OF NR 1 SLAT HAS A VERTICAL RIB, BENT AND CRACKED. REMOVED DAMAGED RIB. FORMED NEW RIB. HEAT TREATED RIB TO T-6 CONDITION. INSTALLED FORMED RIB IAW DC9 SRM 51-30-3. (M)SDR CA011108010Rib · damaged(CAN) WHILE ATTEMPTING TO REMOVE WIRE FROM FLEXIBLE CONDUIT TECHNICIAN NOTICED THAT FLEXIBLE CONDUIT HAD BEEN BURNT. UPON CLOSER INSP FOLLOWING NOTED: 1) HOME MADE PLASTIC CABLE BLOCK (FAIR LEAD) INST 2) FRESH PRIMER WAS BRUSHED ON SEVERAL AREAS INCLUDING WINGSDR 2001FA0000544Rib · crackedDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RIGHT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-2 (RCSW 26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45). FURTHER INSPECTION USING FLUORESCENT PENETSDR 2001FA0000543Rib · crackedDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE LEFT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-1 (LCWS 26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS BETWEEN THE CENTER WING MAIN SPAR (FS 177.45) AND FS 188.95. FURTHER INSPECTION USING FLUSDR DL72S011702Rib · crackedINSPECTION OF THE RBL 70.5 UPPER RIB CHORD AT FS 760.95 ON THE RT WING PER BAC S/B 727-57-0112 AND AD 94-07-08 REVEALED CRACK INDICATIONS IN TWO FASTENER HOLES. THE HOLES WERE OVERSIZED AND BUSHED TO REMOVE THE CRACKS. THE AREA WAS REPAIRED WITH A REPAIR ANGSDR UPS01837180Rib · crackedINSPECTION TYPE:C2 RIGHT WING T/E UPPER RIB IS CRACKED AT XW 5. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.SDR DHL2001801529Rib · crackedRT WING CNTR L/E INTERIOR RIB CRACKED .5 INCH (LWR) AT XFS 385.000. STOP DRILLED CRACK PER SRM 57-2-1 PAR 7. FABRICATED REINFORCING ANGLE PER SRM 57-2-1 PAR 7. INSTALLED REINFORCING ANGLE PER SRM 57-2-1 PAR 7.SDR LR7A01100Fitting · crackedDURING SCHEDULED C3 INSPECTION PER JOB CARD HSP57165 FOUND LH WING OWS 293 LOWER RIB FORMER FITTING CRACKED.REPLACED FITTING PER DWG 371285, SRM SMP 583-51-70 & SB 382-57-75. NR 0470.SDR LR7A01093Fitting · crackedDURING SCHEDULED C3 INSPECTION PER JOB CARD HSP57165 FOUND RH WING OWS 293 LOWER RIB FORMER FITTING CRACKED.REPLACED FITTING PER DWG 371285, SRM SMP 583-51-70 & SB 382-57-75. NR 0381.SDR DHL2001801519Rib · crackedRIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 304. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2.SDR UPS01837134Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837120Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 404. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837118Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837117Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 491.193. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837116Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837115Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 366.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837114Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837113Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 515.72. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837112Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 335.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837011Rib · crackedINSPECTION TYPE: C23, LEFT WING L/E. UPPER RIBS ARE CRACKED AT XFS 354 AND XFS 379 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837010Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 297.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837139Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 822.5, XFS 828.75, XFS 835. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01837137Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 628.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837136Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 578.75, XFS 585. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR DHL2001801520Rib · crackedRIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 310. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2.SDR UPS01837100Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 660. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837099Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 747.5, XFS 753.75, XFS 760. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01837098Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 847.5. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR UPS01837019Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837020Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS01837018Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIB IS CRACKED AT XFS 672.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837017Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 747.5 TO XFS 760 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837016Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 635 AND XFS 647.5. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837015Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 722.5,XFS 728.75, XFS 735. REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2SDR UPS01837014Rib · crackedINSPECTION TYPE: C23, RIGHT WING L/E. LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2
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