Douglas DC-9-32
Service difficulty reports · 12,755
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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 aircraft_model_key = 'DC932' 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 aircraft_model_key = 'DC932' 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 MWEA95360Slide · failed testDURING ROUTINE TIME CHANGE OF FWD GALLEY SERVICE DOOR EVACUATION SLIDE, THE DEPLOYMENT TEST FAILED. MAINTENANCE FOUND RELEASE LANYARD ROUTED INCORRECTLY INSIDE SLIDE AT BOTTLE REGULATOR. MAINTENANCE REPLACED GALLEY SERVICE DOOR EVACUATION SLIDE AND RETURNED SDR MWEA95359Eel · inopMAINT REPORTED, THE FWD EMERGENCY ENTRANCE LIGHT WILL NOT ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AND AIRCRAFT RETURNED TO SERVICE.SDR CAL951055Bulkhead · corrodedHOU - INSPECTION FOUND CORROSION NEAR T-CAP ON RIGHT SIDE OF AFT PRESSURE BULKHEAD. THE CORRODED SECTION WAS CUTOUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 22. (M)SDR 96ZZZM29Door · not closedON FLT 530 - ATL - AIRCRAFT EXPERIENCED A VIBRATION ON THE LEFT SIDE OF THE AIRCRAFT BY THE COCKPIT. AIRCRAFT RETURNED. CHECKED AROUND THE NOSE GEAR AREA AND FOUND THE EXTERNAL POWER DOOR PANEL LEFT OPEN AND CLOSED DOOR.SDR ABXA9600137Door · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT BUTE DOOR NR 1502 BROKEN AND DELAMINATED. REPLACED LEFT BUTE DOOR NR 1502 IAW DC-9 SRM 51-30-5.SDR ABXA9600135Door · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT BUTE DOOR NR 1053 DELAMINATED. REPLACED LEFT BUTE DOOR NR 1503 IAW DC-9 SRM 51-30-5.SDR ABXA9500989Skin · corrodedDURING CARGO MOD, OFF WING INSPECTION, FOUND LEVEL 2 CORROSION ON THE INBOARD LOWER SKIN. REPLACED SKIN IAW DC-9 DRAWING 5910039 AND SRM 51-10-3.SDR ABXA9500988Spar · corrodedDURING CARGO MOD, OFF WING FLAP INSPECTION, FOUND LEVEL 2 CORROSION ON THE AFT LOWER SPAR. REPLACED LOWER AFT SPAR IAW DC-9 DRAWING 5910039 AND SRM 57-50-1.SDR 9516589926Release Cable · frayedDURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR HANDLE FROM THE CLIPS AND TO DROP THE TAILCONE. ALSO, FOUND A FRAYED RELEASE CABLE AND A WORN UPPER LEFT SLIDER BLOCK. REPLACED THE CABLE AND SLIDER BLOCK AND RERIGGED THE RELEASSDR MWEA95358Eel Socket · inopDURING INSPECTION, FOUND ONE EMERGENCY LIGHT ON FLOOR TRACK INOP. MAINTENANCE REPLACED LIGHT SOCKET AT ROW 17, OPS CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.SDR CAL951023Doubler · corrodedHOU - INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 218, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)SDR CAL951022Bracket · corrodedHOU - INSPECTION FOUND CABIN FLOOR SUPPORT BRACKET AT STA 160, AND 8 INCHES - 10 INCHES, LEFT OF CENTERLINE CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-0. (X)SDR CAL951021Belt Frame · crackedHOU - INSPECTION FOUND A .25 INCH CRACK COMING FROM HI-LOCK HOLE ON BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED SECTION OF BELT FRAME WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-03, FIGURE 32. (X)SDR CAL950993Frame · crackedHOU - INSPECTION FOUND A 2 INCH CRACK EXTENDING FROM FASTENER HOLE ABOVE FLOOR ON FRAME AT STATION 813. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-03. (M)SDR CAL950992Floor Supports · corrodedHOU - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STATION 200. THE CORROSION EXTENDED THE FULL LENGTH FROM LEFT TO RIGHT SIDE OF FUSELAGE. FOUR FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. (M)SDR CAL950988Frame · crackedHOU - INSPECTION FOUND A 3 INCH CRACK EXTENDING FROM FASTENER IN FRAME AT STATION 794, STRINGER 18L. THE FRAME WAS REPAIRED IAW SRM 53-11-3, FIGURE 1. (M)SDR ABXA9600144Skin · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT FUSELAGE SKIN DENTED AFT OF FS 965 ABOVE LONGERON 22R. REPAIRED SKIN IAW ABX REA D953-12800-MR.SDR ABXA9500885Seat · defectiveFIRST OFFICER'S SEAT LOOSE AND ROCKS ON SEAT RAILS. ALSO, SEAT BACK ROCKS AND SEAT CUSHION WORN OUT. REPLACED FIRST OFFICER'S SEAT ASSEMBLY IAW DC-9 MM.SDR 97ZZZX4197Steering Piston · pin shearedONE EACH OF TWO STEERING PISTON PINS THAT GO THROUGH COLLAR, PN 5920605-503, WAS SHEARED INSIDE THE COLLAR. THE BREAK WAS IN THE BOTTOM THIRD OF THE SHANK. THERE WAS A HEAVY COATING OF RUST ACROSS THE SHEARED SURFACE. THIS DEFECT WAS DISCOVERED DURING THE PSDR 95ZZZM679Bearing · failedSTL - DURING CLIMB, SHUT DOWN NR 1 ENGINE, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES IN OIL FILTER. REPLACED ENGINE. GROUND OPERATION CHECKED NORMAL. INVESTIGATION OF OIL FILTER BYPASS LIGHT ILLUMINATION AND METAL PARTICLES FOUND ISDR 9522059601Blkhd Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WHEEL WELL BULKHEAD KEEL WEB FS 756. REPAIRED WEB (P/N 9910164-3), PER EA 12-5310-9-C0614.SDR 9516319603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH FITTING AT FS 237, LBL 54. REPLACED FITTING PER SRM 51-10-3, 51-30 AND 53-01.SDR CAL951057Skin · crackedHOU - INSPECTION FOUND TWO .75 INCH CRACKS AT RIVETS IN SKIN LAP AT STA 1038 ABOVE RIGHT PYLON. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M)SDR CAL951056Skin · crackedHOOU - INSPECTION FOUND A .75 INCH CRACK IN SKIN LAP AT STATION 1038 ABOVE LEFT PYLON. THE SKIN CRACK WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M)SDR CAL951024Longeron · corrodedHOU - INSPECTION FOUND LONGERON 30 AT STA 218 CORRODED IN TWO. A LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02. (X)SDR CAL950995Longeron · crackedHOU - INSPECTION FOUND A .25 INCH CRACK IN LONGERON 8L AT STATION 446. THE LONGERON WAS REPAIRED IAW SRM 53-02. (M)SDR CAL950939Actuator Pin · shearedDHN - INSPECTION FOUND THE NLG RIGHT NOSE STEERING ACTUATOR PIN SHEARED. THE STEERING CONTROL LEVER ASSEMBLY AND RIGHT NOSE STEERING CYLINDER ASSEMBLY WERE REMOVED AND REPLACED. (M)SDR CA951129519Wheel Assembly · seized(CAN)A LOUD RATTLING NOISE WAS HEARD COMING FROM NOSE WHEEL WELL AREA ON TAKEOFF. REJECTED TAKEOFF AT 80 KNOTS. A 180 DEGREE TURN WAS EXECUTED, AIRCRAFT TAXIED 100 FEET AND STOPPED. A LOUD WINDING DOWN NOI SE WAS HEARD IN NOSE WHEEL WELL AREA AS BRAKE SET. UNASDR ABXA9600184Panel · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT LOWER TRAILING EDGE PANEL INBOARD OF THE MAIN LANDING GEAR DELAMINATED. REPLACED PANEL ASSEMBLY IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9600156Blkhd Web · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE APB WEB CORRODED JUST BELOW FLOOR LEVEL AT FS 996 AND BETWEEN LBL 10 AND LBL 20. REPAIRED WEB IAW ABX REA D953-13041-MR.SDR 95ZZZM645Door · not latchedFLT NR 547 - PHL - AIR RETURN, AFT AIRSTAIR DOOR LIGHT ILLUMINATED. RECYCLED AFT STAIRS, SYSTEM CHECK NORMAL. (M)SDR 9518599926Angle · corrodedDURING H-CHECK, FOUND CORROSION IN THE UPPER CUSP ANGLE AT THE MAIN CABIN DOOR FS 198 TO 203. REPAIRED ANGLE (P/N 9910078-9), PER EA99-103303.SDR CAL951053Splice · crackedHOU - INSPECTION FOUND A 4 INCH CRACK IN LEADING EDGE SPLICE BETWEEN NR 6 AND NR 7 SLAT TRACK. THE LEADING EDGE SPLICE WAS REPAIRED IAW ECRA 5710-01701. (M)SDR CAL950990Le Splice · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN LEADING EDGE SPLICE BETWEEN THE NR 3 AND NR 4 SLAT TRACK. A DOUBLER WAS INSTALLED IAW ECRA 5710-01697. (M)SDR CAL950989Spar Cap · corrodedHOU - INSPECTION FOUND INTERGRANULAR CORROSION ON LOWER SPAR CAP AT FXLS 325. THE SPAR CAP WAS REPAIRED IAW SRM 57-01, FIGURE 2. (M)SDR ABXA9600177Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED AT FS 237. REPLACED LONGERON 30 IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9600133Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON NR 30 CRACKED AT FS 237. REPLACED IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR 9516229608Fitting · corrodedDURING D-CHECK, FOUND CORROSION ON THE JACK SUPPORT FITTING. REPLACED FITTING PER SRM 51-01 AND DWG 59-17491. DUE TO INCORRECT AIRCRAFT NUMBER, ALL OTHER REFERENCES; MODEL NUMBER, SERIAL NUMBER, ETC HAVE BEEN CHANGED RESPECTIVELY.SDR 9516219921Striker · wornDURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR STRIKERSDR ABXA9600158Trap Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT TRAPEZIODAL PANEL HAD CORROSION INSIDE THE BOLT HOLES ABOVE THE FIXED SIDE BRACE. REPAIRED PANEL IAW ABX REA D953-13155-MR.SDR ABXA9600130Blkhd Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 CRACKED AT LONGERON 11R. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2.SDR ABXA9600129Blkhd Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 HAD A SMALL CRACK RADIATING FROM LIGHTENING HOLE BETWEEN LONGERON 12R AND 13R. REPAIRED CRACK IAW DC-9 SRM 53-01 FIGURE 2.SDR ABXA9600091Angle · crackedDURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9600090Angle · crackedDURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9600089Angle · crackedDURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9600088Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 92-22-08, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500983Te Skin · corrodedDURING CARGO MOD OFF WING INSPECTION, FOUND LEVEL 2 CORROSION IN TWO AREAS ON THE LOWER SKIN DOUBLER ALONG THE TRAILING EDGE. REPLACED CENTER SKIN IAW DC-9 DRAWING 5910411.SDR 95ZZZM682Door Beam · crackedSTL - DURING C-CHECK, FOUND TWO INCH CRACK IN NR 2 DOOR BEAM FORWARD END. REPAIRED PER SRM 51-30 AND STANDARD PRACTICES.SDR 9518589926Web · corrodedDURING H-CHECK, FOUND CORROSION IN THE LEFT MAIN LANDING GEAR WHEEL WELL FORWARD SLANT PRESSURE PANEL WEB. REPAIRED WEB (P/N 5956065-41), PER EA 99-102597.SDR 9518579926Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION IN THE BL 0 FLOOR CAP BETWEEN FS 689 TO 699. REPAIRED CAP (P/N 5910347-25), PER EA 99-103291.
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