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 ABXA9701620Rib · crackedLT WING L/E RIB AT STA XFS 810.0 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.SDR ABXA9701616Rib · crackedLT WING L/E RIB AT STA XFS 828.75 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.SDR ABXA9701608Rib · crackedRT WING L/E AT STA XFS 728.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.SDR UPS97824747Rib · crackedINSPECTION TYPE-C, THE LT WING L/E RIB AT THE OTBD END OF THE UPPER SLOT DOOR IS CRACKED PAST THE STOP DRILL. REMOVED AND REPLACED PAN ASSY IAW SRM 51-1-21, 51-1-20D, 51-3-0, AND DWG 5769857.SDR UPS97824717Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 696.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-0.SDR UPS97824712Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 397.75 IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.SDR TWAA9711709Rib · crackedMCI - INSTALLED DOUBLER IN CRACKED RIB CHORD LEFT WING AT STATION 738.5. (M)SDR TWAA9711703Rib · crackedMCI - REPAIRED CRACKED AREA AT RIB UPPER CHORD RBL 70.2 STATION 760 FWD BOLT HOLES. (M)SDR C2XA97IA295Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING OUTBOARD LEADING EDGE SUPPORT RIB AT RIB NR 30 CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW ATR-42 SRM 51-70-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR UPS97824606Rib · crackedINSPECTION TYPE-C, L/WING UPPER L/E RIB CRACKED AT STA 828.750. REPAIRED IAW SRM 57-2-0, 51-1-21 AND 51-1-29D.SDR UPS97824597Rib · crackedINSPECTION TYPE-C, L/WING L/E UPPER RIB CRACKED AT STA 703.750. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20D.SDR UPS97824596Rib · crackedINSPECTION TYPE-C, L/WING LWR L/E RIB CRACKED AT STA 603.750. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20D.SDR UPS97824595Rib · crackedINSPECTION TYPE-C, L/WING L/E UPPER RIB CRACKED AT STA 787.500. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20.SDR UPS97824594Rib · crackedINSPECTION TYPE-C, L/WING UPPER L/E RIB CRACKED AT STA 597.500. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20D.SDR UPS97824587Rib · crackedINSPECTION TYPE-C, L/WING L/E UPPER RIB CRACKED AT STA 803.750. FABRICATED AND INSTALLED REPAIR IAW SRM 57-3-3, 57-2-0, 51-1-20D.SDR UPS97824525Rib · crackedINSPECTION TYPE-C, RT WING L/E STA XFS 748.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0, 51-1-20D, 51-1-21.SDR ABXA9701697Rib · crackedLEFT WING L/E RIB AT STA XFS 760.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC-8 SRM 57-2-0.SDR ABXA9701696Rib · crackedLEFT WING L/E RIB AT STA XFS 722.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC-8 SRM 57-2-0.SDR ABXA9701593Rib · crackedRT WING L/E AT STA XFS 660.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-20D AND 51-1-21.SDR ABXA9701595Rib · crackedRT WING L/E AT STA XFS 822.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-10, 51-1-20D AND 51-1-21.SDR ABXA9701594Rib · crackedRT WING L/E AT STA XFS 697.5 THE UPPER L/E RIB IS CRACKED AT THE AFT END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D AND 51-1-21.SDR ABXA9701592Rib · crackedRT WING L/E AT STA XFS 741.25, THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0 FIG 2, SRM 51-1-20D AND SRM 51-1-21.SDR ABXA9701578Rib · crackedLT WING L/E RIB IS CRACKED AT XFS 578.75 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701577Rib · crackedLT WING L/E RIB IS CRACKED, XFS 585.00 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701576Rib · crackedLT WING L/E RIB IS CRACKED, XFS 591.25 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701575Rib · crackedLT WING L/E RIB IS CRACKED XFS 597.5 AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701574Rib · crackedLT WING L/E RIB IS CRACKED XFS 603.75 AFT LWR END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701558Rib · crackedLT WING L/E RIB IS CRACKED AT XFS 610.00 AFT UPPER END. REPAIRED IAW SRM 52-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701557Rib · crackedLT WING L/E RIB IS CRACKED AT XFS 616.25 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701556Rib · crackedLT WING L/E RIB IS CRACKED XFS 622.50 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701555Rib · crackedLT WING L/E RIB IS CRACKED XFS 778.75 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701554Rib · crackedLT WING L/E RIB IS CRACKED XFS 785.00 AFT UPPER END. REPAIRED IAW SRM 57-2-0 FIG 2, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701553Rib · crackedLT WING L/E RIB IS CRACKED XFS 797.50 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701552Rib · crackedLT WING L/E RIB IS CRACKED AT XFS 810.00 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701551Rib · crackedLT WING L/E RIB IS CRACKED AT XFS 816.25 AFT UPPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701550Rib · crackedLT WING L/E RIB IS CRACKED AT STA XFS 828.75 AFT LWR END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701549Rib · crackedLT WING L/E RIB IS CRACKED AT STA XFS 835.00 AFT LOWER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR ABXA9701548Rib · crackedLEFT WING L/E RIB IS CRACKED AT STA XFS 628.75 AFT UPER END. REPAIRED IAW SRM 57-2-0, SRM 51-1-21, AND SRM 51-1-21.SDR TWAA9804006Rib · crackedMCI - DURING OP17 MAINTENANCE CHECK, THE LEFT WING WS 738.5 RIB CHORD WAS CRACKED ON LOWER CHORD AT STRINGER 6 AND 8, IN THE RADIUS. INSTALLED NEW RIB PER SRM 51-10-1 AND 51-30-2. (M)SDR CA970916005Rib · buckled(CAN) THE BENT RIB CONDITION PROBLEM HAS BEEN PREVIOUSLY FOUND ON OTHER INSPECTIONS. IT APPEARS THIS CONDITION OCCURS IN AREA ABOVE THE AILERON HINGE OUTBOARD SECTION AND IS ALSO THE AREA WHERE THE AILERON BALANCE WEIGHTS ARE LOCATED.SDR CA970915005Rib · cracked(CAN) WHILE CARRYING OUT A 100 HR INSPECTION THE AME, FOUND CRACKS AT THE WING RIBS AT STATION 22.87 AND STATION 36.12. THREE CRACKS WERE FOUND IN THE SECOND AND THIRD LIGHTENING HOLE IN P/N 1621401-8 AND THREE CRACKS WERE FOUND IN THE FIRST, SECOND AND THIRDSDR CA970915006Rib · cracked(CAN) WHILE PERFORMING A 100 HR INSPECTION, THE AME FOUND A CRACK AT THE WING RIB AT STATION 20.62. THE CRACK IS APPROXIMATELY .75 INCH LONG STARTING FROM THE LIGHTENING HOLE WHICH IS LOCATED 11 INCHES FORWARD OF THE REAR WING ATTACHMENT.SDR 97ZZZX4038Rib · rivet shearedRIB NR 3 AT STA 69.24 WHERE ANGLES RIVET TO FALSE SPAR RIVETS SHEAR ALLOWING STRUT TO PUSH UP THROUGH UPPER SKIN. ALSO DAMAGES RIB NR 2 AT STA 49.25 AND CRACKS BOTH UPPER AND LOWER FALSE SPAR CAPS. SUSPECT CAUSE, HARD LANDING OPERATING WITH FLAT STRUT OR OVESDR 97ZZZX4034Rib · rivet shearedRIB NR 3 AT STA 69.24 WHERE ANGLES RIVET TO FALSE SPAR RIVETS SHEAR ALLOWING STRUT TO PUSH UP THROUGH UPPER SKIN. ALSO DAMAGES RIB NR 2 AT STA 49.25 AND CRACKS BOTH UPPER AND LOWER FALSE SPAR CAPS. POSSIBLE CAUSE, HARD LANDING OPERATING WITH FLAT STRUT OR OVSDR 97ZZZX4517Rib · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR 97ZZZX4513Rib · crackedMAIN LANDING GEAR SUPPORT STRUCTURE, LT AND RT, MLG WHEELWELL - CRACKS ARE OCCURRING IN THE RIBS, PN 0822175-79, -74, CENTER RIB WEB, ORIGINATING AT UPPER AFT CORNER OF THE CUT-OUT HOLE (WHERE THE OPERATING PUSH/PULL ROD PASSES THROUGH) PROPAGATING TOWARDS TOPSDR UPS97824384Rib · crackedINSPECTION TYPE:C, RT WING L/E AT STA XFS 821.00 - THE L/E RIB IS CRACKED AT THE AFT UPPER END. REPAIRED L/E RIB IAW SRM 57-3-1 FIG 7 AND 51-1-20D.SDR UPS97824383Rib · crackedINSPECTION TYPE:C, RT WING L/E AT STA XFS 636.00 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-20D.SDR ABXA9701590Rib · crackedRT WING L/E AT STA XFS 847.50, THE UPPER L/E RIB IS CRACKED AT THE AFT END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.SDR ABXA9701589Rib · crackedLT WING L/E RIB AT STA 816.25 IS CRACKED AT THE AFT LOWER END. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0, SRM 51-1-20D AND SRM 51-1-21.
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