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 UPS98825756Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER STA XFS- 772.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825755Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 810.000. REPAIRED IAW SRM 57-2-0.SDR UPS98825754Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XFS 766.250. REPAIRED IAW SRM 57-2-0.SDR UPS98825753Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 728.750. REPAIRED IAW SRM 57-2-0.SDR UPS98825752Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER AT STA XFS 822.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825751Rib · crackedINSPECTION TYPE:C, LT WING LE RIB UPPER AND LWR ARM CRACKED BY AFT FASTENER AT STA XFS 797.500, REPAIRED IAW SRM ADDN DC8-5720-4087.SDR UPS98825749Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA, XFS 760.000, REPAIRED IAW DC8 SRM 57-2-0.SDR UPS98825748Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XF S747.500. REPAIRED IAW DC-8 SRM 57-2-0.SDR UPS98825747Rib · crackedINSPECTION TYPE:C, RT WING L/E AT STA XOLDI 6.225, THE UPPER L/E RIB HAS A 9 INCH CRACK. REPAIRED CRACKED L/E RIB AT STA XOLDI 6.225 IAW DC-8 SRM 57-2-0 FIG 2.SDR DHL9872404CRib · crackedAT C-CHECK, RT WING RIB CHORD AT BL 70.5 HAS HFEC CRACK INDICATION, HFEC HOLE, OVERSIZED. HFEC INSTALLED ATTACH TEE PER SRM 51-20-2, N/R 2288.SDR CALA9800171Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT LOWER OUTBOARD FLANGE AFT END, OF LT WING LEADING EGDE RIB, XORS 885. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-00-01 AND 51-31-01.SDR MZZA98077Rib · crackedKUL - Q-CHECK - RIGHT WING OUTBOARD F/FLAP CENTER STABILIZING TRACK - SUPPORT FITTING INBOARD AND OUTBOARD TRACK RIBS - OUTBOARD RIB HAS .50 INCH CRACK AT FORWARD RIVET HOLE AND INBOARD RIB HAS EXCESSIVE WEAR IN LUG RADIUS. BOTH FITTINGS REPLACED IAW SRM 51-3SDR 98ZZZX1074Rib · crackedKUL - Q-CHECK - RIGHT WING OUTBOARD F/FLAP CENTER STABILIZING TRACK - SUPPORT FITTING INBOARD AND OUTBOARD TRACK RIBS - OUTBOARD RIB HAS .50 INCH CRACK AT FORWARD RIVET HOLE AND INBOARD RIB HAS EXCESSIVE WEAR IN LUG RADIUS. BOTH FITTINGS REPLACED IAW SRM 51-3SDR UPS98825990Rib · crackedINSPECTION TYPE:D/CK LEFT WING MIDDLE LEADING EDGE RIB CRACKED AT FUEL DOOR. RECEIVED REO FABRICATED PARTS HEAT TREATED IAW REO 04277. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW REO 04277 AND DC8 SRM 51 1 20D.SDR UPS98825692Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED LWR ARM STA 385.250. REPAIRED IAW SRM 57-3-1.SDR CALA9800128Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT FASTENER OF RT WING LEADING EDGE RIB, INBOARD OF NR 4 LEADING EDGE FLAP, AT L/E STA 130. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR ABXA9800123Rib · crackedLT WING L/E RIB AT STA XOLDI 6225, ABOVE THE PNEUMATIC DUCT IS CRACKED, APPROXIMATELY 2.75. REPAIRED IAW DC8 SRM 57-2-0.SDR ABXA9800121Rib · crackedRIGHT WING LEADING EDGE, INBOARD OF NR 3 PYLON, LEADING EDGE PANEL, UPPER RIB CRACKED AT STA XFS 192. REPAIRED IAW DC8 SRM 51-1-20D AND ABX DWG K0-5056-7007.SDR ABXA9800120Rib · crackedLEFT WING LEADING EDGE RIB, STA XFS 741.25 CRACKED AT UPPER END. REPAIRED IAW DWG K05056-7008 AND DC8 SRM 51-18 AND 51-1-20D.SDR ABXA9800115Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XS 497.491 IS CRACKED AT AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0.SDR ABXA9800114Rib · crackedRIGHT WING LEADING EDGE, OUTBOARD OF NR 4 PYLON INBOARD LWR RIB CRACKED AT XFS 585. REPAIRED IAW DC8 SRM 57-2-0.SDR CALA9800105Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT FASTENER IN RT WING RIB INBOARD OF NR 4 LEADING EDGE FLAP AT L/E STA 130. THE CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR P5CA9800122Rib · crackedNR 2 MAIN TANK LOWER REP STIFFENER CRACKED RIB. ALSO, WEB UNDER STIFFENER CRACKED. REPLACED STIFFENER AND REPAIRED WEB PER SRM 51-10-01 AND 57-10-05 FIG 2.SDR UPS98825594Rib · crackedINSPECTION TYPE-C, LT WING L/E AT STA XFS 728.750 UPPER ARM CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98825690Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 UPPER RIB CRACKED 4. REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS98825642Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 772.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98825598Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 778.750 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98825646Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED ON LWR ARM BY AFT FASTENER STA 616.250. REPAIRED IAW SRM 57-2-0.SDR UPS98825597Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 297.50. REPAIRED IAW SRM 57-2-0.SDR UPS98825596Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 622.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825595Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA XFS 647.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825593Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 653.750. REPAIRED IAW SRM 57-2-0.SDR UPS98825592Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 635.000. REPAIRED IAW SRM 57-2-0.SDR UPS98825591Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER STA XFS 778.750. REPAIRED IAW SRM 57-2-0.SDR UPS98825590Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XS 484.395. REPAIRED IAW SRM 57-2-0.SDR UPS98825589Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XS 466.651. REPAIRED IAW SRM 57-2-0.SDR UPS98825588Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 597.5. REPAIRED IAW SRM 57-2-0.SDR UPS98825587Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 747.500. REPAIRED IAW SRM 57-2-0.SDR MWEA98070Rib · crackedDURING C-CHECK, FOUND LEFT WING LEADING EDGE RIB AT STA XRS 394 CRACKED ON AFT LOWER LEG APPROX 2 .625 IN. MTC INSTALLED ANGLE REPAIR IAW TELEX MISC DG 28/GLP.SDR F3LA97175Rib · crackedPAE - FIXED L/E NR 3 SLAT TRACK INBOARD MAIN TRACK, INBOARD ROLLER SUPPORT RIB HAS CRACK, FSS 271, SS 31.42. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-30-02. (M)SDR DHL9880658CRib · crackedAT C-CHECK, RT WING FILLET FAIRING RIB CRACKED. REMOVED DAMAGED RIB, FABRICATED REPAIR AND INSTALLED PER SRM 51-1-21, 1 X 1 X 9.SDR DHL9872454CRib · crackedAT C-CHECK, CRACK IN UPPER FLANGE OF RIB 13, R/W. STOP DRILL CRACK, HFEC, INSTALLED RIB REPAIR PER SRM 57-10-5. REPAIR 16 X 2 X 1. N/R 2257.SDR DHL9872440CRib · crackedAT C-CHECK, 1 CRACK NOTED AT UPPER FLANGE AT RIB 13. STOP DRILLED CRACK, HFEC STOP DRILL, INSTALLED RIB REPAIR AT WS 601.5 PER SRM 57-10-5, 16 X 2 X 1. N/R 2257.SDR CALA9800073Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF NR 6 LEADING EDGE SLAT STA 234. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800072Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN ABOVE PNEUMATIC DUCT FORWARD SUPPORT BRACKET AT FSS 106.8. A REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR DHL9872459CRib · crackedAT C-CHECK, LEFT WING RIB CHORD BL 70.5 HAS CRACK INDICATION AT FWD UPPER AND FWD LOWER HOLES. HFEC, CRACK VERIFIED. STOP DRILLED CRACK, HFEC, INSTALLED REPAIR PER S/B 57-0211. N/R 1030/1143.SDR CALA9800062Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN LOWER EDGE AT FSS 106.8. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800061Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2.SDR CALA9800059Rib · crackedINSPECTION FOUND A .5 INCH CRACK INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STA 130 ABOVE HOT AIR DUCT PLENUM. ALSO, A .5 INCH CRACK WAS FOUND INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STATION 130 BELOW LIGHTENING HOLE AREA. DOUBLER REPAIRS WERE FSDR 98ZZZX720Rib · crackedFOLLOWING A WINDSTORM THAT BROKE THE GUSTLOCK, AN INVESTIGATION OF THE FLIGHT CONTROLS REVEALED CRACKS ON BOTH THE INBD AND OTBD WING RIBS AT THE AILERON BRACKET RIVETS.
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