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 = '5700' 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 = '5700' 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 RRXA10892Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE L/H L/E WING CENTER AT STA XFS 422.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAAW DC-8 SRM 57-2-0, FIG AND 51-1-20D.SDR DHL2001806577Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 785.250. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUSSDR DKAA01009Structure · damagedFOUND THREE ELONGATED HOLES AT LEFT XFS206, RIGHT XFS184, XFS184. REPAIRED PER DER DRAWING NR 57-01590-1, DATED 02/07/2001. AIRCRAFT RETURNED TO SERVICE. (M)SDR DKAA01001Skin · damagedRIGHT WING TIP ASSEMBLY BOTTOM SKIN DAMAGED. REPLACED AFFECTED SKIN PANELS PER DER DOCUMENT 01-02 REV A, DATED 1/18/2001. AIRCRAFT RETURNED TO SEVICE. (M)SDR UPS01235218Structure · corrodedINSPECTION TYPE:C+SI, X-RAY REPORT - SUSPECT CORROSION ON WING CENTER SECTION AT WBL 70.5 UPPER LT AREA AT BS 870. REPAIR CARRIED OUT IAW SRM 51-30-2 BOEING DWG 69-13965 & SMRO EO 200 1-006-015, UPS ENGINEERING FILE NR 727-57-20009.SDR ABXA010415Skin · gougedLEFT WING LEADING EDGE STAB WING ABOVE #2 ENGINE, OUTBOARD END OF VANE HAD SEVERAL HOLES WITH VERY DEEP GOUGES CAUSED BY DIMPLE WASHERS, APPROXIMATELY W/STA. 225.0 REMOVED SEAL ASSEMBLY, FABRICATED REPAIR DOUBLER IAW REA D857-39765MR. ALODINED AND PRIMED IAW SDR R3R2001201Screw · incorrectTHE OUTBOARD ATTACH SCREW IN THE HEATED LEADING EDGE IS TOO LONG AND CAN DAMAGE THE WING SKIN BELOW IT. THE IPC CALLS OUT A MS24694-C48 SCREW IT IS TOO LONG. (X)SDR CA010108015Bolt · leaking(CAN) MAINTENANCE INVESTIGATION OF A FUEL LEAK FROM THE LT WING NR 3 FLAP TRACK ATTACH POINT AT THE REAR WING SPAR REVEALED THAT THE ATTACH BOLTS WERE BELOW RECOMMENDED TORQUE. BOLT TORQUE WAS BROUGHT UP TO SPECS AND HEADS RESEALED INSIDE THE FUEL TANK. THE AISDR G60A053Skin · damagedLOWER SURFACE OF INBOARD AILERON, STATION XW 060 HAS 24 INCHES CORDWISE TEAR IN SKIN DUE TO ENGINE FAILURE. REMOVED AND REPLACED LEFT INBOARD AILERON IAW 27-10-01. (M)SDR UPS00433709Web · crackedINSPECTION TYPE:N/A, NR 1, 2 AND 3 PYLON WEB CRACKED. *S/D* REPAIRED PER SRM 51-10-01 PYLON NR 1 LOG PAGE 460751 NR 2 LP 460759, NR 3 LP 460752.SDR QXEA0001566Bulkhead · chafedYYC- RIGHT HAND STUB WING LATERAL BULKHEAD HAS HOLE CHAFED THROUGH DUE TO CONTACT WITH 7TH STAGE PNEUMATIC DUCT. REPAIRED IAW HORIZON AIR EA 4-54-103, FOKKER SRM 54-02-01 FIGURE 4 AND 51-31-01.SDR QXEA0001565Bulkhead · damagedYYC- LEFT HAND STUB WING LATERAL BULKHEAD HAS HOLE CHAFED THROUGH, DUE TO CONTACT WITH 7TH STAGE PNEUMATIC DUCT. REPAIRED IAW HORIZON AIR EA 4-54-103 AND FOKKER SRM 54-02-01 FIGURE 4.SDR 20000524SH018Rivet · misinstalledAIRCRAFT REPAIRED IN 1980 AFTER GEAR UP LANDING. REPAIRS FOUND TO BE UNACCEPTABLE IN 2000 ANNUAL. RIVETS WERE INSTALLED WITH NO SHOP HEAD, AND RIVET HEADS NOT AGAINST STRUCTURE. LOCATION OF REPAIR IS UPPER FORWARD WING SPAR JUST OUTBOARD OF WING BELT FITTINSDR DL72L000527Spar · crackedCRACKS IN AFT SPAR RAIL AT 21 AND 35 FROM I/B END OF FLAP. ALSO DOUBLER SHORT AT 30 FROM O/B END OF FLAP. CORRECTED ON SHOP ORDER NR 957610.SDR 20000510AP004Web · crackedFOUND 1.75 INCH CRACK AT LEFT WING OUTBOARD MID FLAP INBOARD MOST RIB AT LOWER AFT END. STOP DRILLED CRACK IAW SRM 51-10-1. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. HFEC INSPECTION CONFIRMED CRACK WAS CONTAINED. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. SDR DL72S992542Rib · crackedFOUND ON D1 LETTER CK, 1 INCH CRACK NR 2 SLAT NOSE RIB I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0.SDR DL72L991498Skin · crackedDURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE CRACK WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 809.SDR AU990491Structure · misrepaired(AUS) STEEL SCREWS USED IN THE LEADING EDGE ADJACENT TO THE COMPASS SYSTEM FLUX VALVE. A STEEL SCRIBER WAS ALSO FOUND IN THE CHANNEL ADJACENT TO THE FLUX VALVE. THE STEEL ITEMS PREVENTED THE NR 2 COMPASS SYSTEM FROM CORRECT OPERATION. UNAPPROVED PART. FODSDR AU990489Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE IN THE FOLLOWING LOCATIONS: 1. LT AILERON AND LT AND RT AILERON TAB. 2. LT AND RT ELEVATOR. 3. SPOILERS. 4. RUDDER.SDR AU990485Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT OUTBOARD AILERON, RT INBOARD AND OUTBOARD AILERONS. 2. LT AND RT ELEVATORS. 3. NR 1, NR 2, NR 3, NR 4, NR 5, NR 7, NR 8, NR 9, NR 10, NR 11, NR 12 LEADING EDGE SLATS. 4. NR 2, NR 3, NR 4SDR RAIA990221Doubler · crackedSTL - RIGHT WING AFT SPAR CRACKED NEAR RIB NR 67. MAINTENANCE REPAIRED RIGHT WING SPR IAW NR J3200-57-012-1. (M)SDR ABXA9900193Clip · crackedFITTING CRACKED INSIDE NR 2 TANK AT STATION XRS 22.750 FORWARD OF AFT SPAR LOWER STRUCTURE. REPAIRED IAW DC8 SRM 51-1-20 AND 51-1-21.SDR CA990203002Flying Wire · broken(CAN) IN CRUISE ,THE PILOT FELT THE NOW FAMILIAR THUMP OF A FLYING BREAKING. THIS IS THIRD TIME. HOWEVER, THIS TIME IT WAS THE UPPER RIGHT HAND WIRE. PILOT REPORTED THAT THE WIRE SEEMED A LITTLE TIGHTER DUE, HE THOUGHT, TO CONTRACTION OF STEEL IN COLD TEMPESDR 98ZZZX4254Lift Strut · corrodedTHIS WAS THE FRONT WING LIFT STRUT. WHILE C/W AD 98-10-06 IAW SB 528D, SKETCH 'A', CORROSION WAS FOUND AT 5 INCH-7 INCH, AND 10 INCH-12 INCH FROM THE END OF THE STRUT. AT 12 INCHES, THIS IS 1 INCH OUTSIDE THE INSPECTION AREA PER SKETCH 'A'. THE STRUT WAS RESDR 98ZZZX4324Lift · corrodedUNAIRWORTHY DUE TO CORROSION IN LEFT REAR LIFT STRUT AS INDICATED IN PARAGRAPH 'A'. AD NOTE 93-10-06.SDR DLM88991649Rib · damagedDURING CONDITION ACCEPT INSPECTION OF FLAP-A TEMP TYPE REPAIR WAS FOUND ON I/B AFT CLOSEOUT RIB, LOWER AFT CORNER. THE RIB WAS REPAIRED PER MM 57-52-0, FIG 808 BY INSTALLING A DIFFERENT DOUBLER.SDR 98ZZZX3880Struts · crackedPARA 'A' OF AD NOTE 93-10-06 C/W USING AN FAA APPROVED X-RAY METHOD. LT FRONT STRUT AIRWORTHY. LT REAR STRUT UNAIRWORTHY. RT FRONT STRUT AIRWORTHY. RT REAR STRUT UNAIRWORTHY. X-RAYS ARE ON FILE AT THIS REP STA UNDER W/O NR A-2831. SUBMITTER STATED UNAIRWSDR CA980916042Flying Wire · broken(CAN) IN CRUISE, AIRCRAFT ON FLOATS, IN CALM AIR, THE PILOT FELT A THUMP IN THE CONTROL STICK AND A SUBSEQUENT VIBRATION. FLIGHT CONTINUED TO AN UNEVENTFUL LANDING. THE UPPER LEFT FLYING WIRE WAS FOUND TO HAVE SEPARATED 6 INCHES FROM THE LOWER END. NO CORROSDR 98ZZZX1145Nacelle · corrodedFUEL LEAKING FROM RT WING FND COMING FROM RT NACELLE FUEL CELL. REMOVED NACELLE ACCESS COVER, FUEL CELL LINER, HEAT SHIELD, AND FUEL CELL. SEVERE CORROSION FND ON UPPER WING SKIN AND STRS. FUEL CELL LINER CORRODED (EXFOLIATED). ALSO, LT NACELLE INSPECTED SDR 98ZZZX1144Nacelle · corrodedFUEL LEAKING FROM RT WING FND COMING FROM RT NACELLE FUEL CELL. REMOVED NACELLE ACCESS COVER, FUEL CELL LINER, HEAT SHIELD, AND FUEL CELL. SEVERE CORROSION FND ON UPPER WING SKIN AND STRS. FUEL CELL LINER CORRODED (EXFOLIATED). ALSO, LT NACELLE INSPECTED SDR 98ZZZX760Strut · rustedWING STRUTS WERE INSPECTED IAW AD 93-10-06 AND SB 528D IN DEC '96 AND FOUND OK. DURING '97 ANNUAL, OWNER HAD ALL FOUR STRUTS INSPECTED AND MODIFIED. STC SA 4635NM WAS DONE TO STRUTS. OLD FORK BARREL WAS CUT OFF BY TECHNICIANS. FOUND 2 STRUTS RUSTED SEVERELSDR ABXA9701884Rib · crackedLEFT WING, LEADING EDGE UPPER RIB CRACKED AT XFS 341. REPAIRED IAW SRM 57-2-0 AND 51-1-20D.SDR 97ZZZX2062Structure · crackedAD 75-27-09 PERFORMED ON OUTBOARD WING AT WS 111 AND WS 102. X-RAYS REVEALED LINEAR INDICATIONS AT WS 111 AND CORROSION AT WS 102. FILMS SENT TO BEECHCRAFT FOR FURTHER EVALUATION. THIS WING NOT YET ATTACHED TO AN AIRCRAFT. IT WAS PURCHASED AS A SERVICEABLESDR 97ZZZX1247Strut · corrodedREMOVED WING LIFT STRUT VERTICAL BRACES TO FACILITATE REPAINT OF STRUTS AND BRACES. FOUND CORROSION ON STRUT AT BRACE CLAMP AREA. PTTING HAD OCCURRED CIRCUMFERENTIALLY AROUND THE LIFT STRUT. ALTHOUGH PITTING WAS NOT EXCESSIVE IN THIS CASE, FURTHER DAMAGE COSDR 97ZZZX846Strut · corrodedWING SUPPORT STRUTS (P/N C6W1005-7 LEFT, C6W1005-8 RIGHT). FOUND EXFOLIATON CORROSION ON BEAM FLANGES 12 TO 18 INCHES FROM LOWER ATTACH POINTS WHILE PERFORMING INTERNAL STRUT BEAM INSPECTION IAW FAA AD 87-04-23. SUBMITTER SUGGESTS CORROSION CAUSED BY ELECTROSDR 97ZZZX845Strut · corrodedWING SUPPORT STRUTS (P/N C6W1005-7 LEFT, C6W1005-8 RIGHT). FOUND EXFOLIATON CORROSION ON BEAM FLANGES 12 TO 18 INCHES FROM LOWER ATTACH POINTS WHILE PERFORMING INTERNAL STRUT BEAM INSPECTION IAW FAA AD 87-04-23. SUBMITTER SUGGESTS CORROSION CAUSED BY ELECTROSDR CA961218013Wing · contaminated(CAN) AFTER REMOVAL OF ACCESS PANEL 612BB UNDER THE RIGHT HAND WING, AN ACCUMULATION OF WATER 1 1/2" TO 2" DEEP WAS FOUND. THE AILERON CABLE IS ROUTED IN THIS AREA. ALL THIS OPERATORS 1900S HAD THE SAME PROBLEM.SDR CA961218012Wing · contaminated(CAN) AFTER REMOVAL OF ACCESS PANEL 612BB UNDER THE RIGHT HAND WING, AN ACCUMULATION OF WATER 1 1/2" TO 2" DEEP WAS FOUND. THE AILERON CABLE IS ROUTED IN THIS AREA. ALL THIS COMPANIES 1900S HAD THE SAME PROBLEM.SDR CA961218010Wing · contaminated(CAN) AFTER REMOVAL OF ACCESS PANEL 612BB UNDER THE RIGHT HAND WING, AN ACCUMULATION OF WATER 1 1/2" TO 2" DEEP WAS FOUND. THE AILERON CABLE IS ROUTED IN THIS AREA. ALL THIS COMPANIES 1900S HAD THE SAME PROBLEM.SDR 96ZZZX5241Flying Wire · brokeWIRE BROKE 10 INCHES FROM WING ATTACH (BROKE FROM TOP TO BOTTOM). PART APPEARS TO HAVE BEEN CRACKED ONE-HALF THROUGH FOR SOME TIME PRIOR TO FAILURE.SDR 96ZZZX4318Nut · fracturedLIFT STRUT HAS 5 BOLTS, AN5, THROUGH TOP AND BOTTOM. TOTAL OF '5' NUTS HAD FAILED (FIFTY PERCENT). RIGHT LIFT STRUT ALL NORMAL. CAUSE UNKNOWN, NUT P/N NAS679AW.SDR 96ZZZX3796Lift Strut · corrodedINSPECTION FOUND RIGHT REAR STRUT WITH LARGE AMOUNT OF CORROSION, LOWER 15 INCHES OF STRUT. DENSITY CHECK: COMPARITOR SHIM = 3.69 H.D., CORROSION = 4.23 H.D.SDR 96ZZZX2373Lift Strut · defectivePARAGRAPH 'A' OF AD NOTE 93-10-06 HAS BEEN ACCOMPLISHED USING AN FAA APPROVED X-RAY METHOD. REMARKS: LT FRONT STRUT AIRWORTHY, LT REAR STRUT UNAIRWORTHY, RT FRONT STRUT AIRWORTHY, RT REAR STRUT AIRWORTHY. X-RAYS ARE ON FILE AT THIS REPAIR STATION.SDR 96ZZZX2043Lift Strut · corrodedINSPECTION OF LIFT STRUTS PER AD 93-10-06 FOUND NR 1 STRUT UNAIRWORTHY DUE TO LOWER 8 INCH OF STRUT DEFECTIVE DUE TO CORROSION.SDR DL72L960405Bracket · crackedFOUND ON D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-0-21 PG 811.SDR 96ZZZX874Lift Strut · corrodedWHILE PERFORMING MAULE SB NR 11 (WING LIFT STRUT ASSY INSP/REPL), THREE OF THE FOUR LIFT STRUTS FAILED THE INSPECTION, BOTH FRONT AND RIGHT REAR FAILED. THERE WAS NO EXTERNAL VISIBILITY OF THIS PROBLEM. THE AIRCRAFT HAS ALSO BEEN HANGARED SINCE NEW. THE TOTSDR 96ZZZX673Strut · corrodedDURING ANNUAL INSPECTION, A RIVET HEAD FOUND MISSING FROM LOWER FITTING ON THE LT 'N' STRUT. DURING ATTEMPT TO REPAIR, STRUT WAS REMOVED AND SEVERE CORROSION WAS FOUND WHICH CAUSED REDUCTION OF WALL THICKNESS BY 40 PERCENT.SDR 96ZZZX20Wing · fodBIRD STRIKE TO LEFT OUTBOARD WING. OUTBOARD LEADING EDGE DAMAGE.SDR 95ZZZX3321Nut · brokenON ANNUAL INSPECTION WHEN LOWER LIFT STRUT FAIRINGS WERE REMOVED, SEVERAL PIECES OF BROKEN NAS679 NUTS FELL OUT. INSPECTION OF REMAINING NUTS REVEALED SEVERAL CRACKED NUTS. WHEN NUTS WERE REMOVED FOR REPLACEMENT, SOME BOLTS FELL OUT. SUSPECT CAUSE IS BAD BASDR 95ZZZX2416Lift Strut · corrodedREPLACE STRUT. X-RAY SHOWS NUMEROUS AREAS THAT ARE CORRODED COMPLETELY THROUGH STRUT WALL. A PIN WAS PUSHED THROUGH THE PAINT AND SHOWED THROUGH THE STRUT WALL IN SEVERAL LOCATIONS.
Back to JASC 5700