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.

SDR ABXA9801168Longeron · crackedDURING C-CHECK, FOUND LONGERON 30 CRACKED AT SPLICE BETWEEN STATION 794 TO 813. REPAIRED LONGERON IAW DC9 SRM 53-02.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9801167Longeron · crackedDURING C-CHECK, FOUND LONGERON 25L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9801166Longeron · crackedDURING C-CHECK, FOUND LONGERON 24L CRACKED AT STATION 200. REPAIRED IAW DC9 SRM 53-02.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9801165Longeron · crackedDURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 945. REPAIRED LONGERON IAW DC9 SRM 53-02.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9801164Longeron · crackedDURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM DWG K05864.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9801163Longeron · crackedDURING C-CHECK, FOUND LONGERON 2R CRACKED AT STATION 1076. REPAIRED LONGERON 2R IAW DC9 SRM 53-02.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9801148Bulkhead Web · corrodedDURING C-CHECK, FOUND LEFT PYLON BULKHEAD FORWARD LOWER SIDE CORRODED. REPLACED WEB ON PYLON BULKHEAD IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9801147Fitting · crackedDURING C-CHECK, FOUND CENTER WING FORWARD SPAR ATTACH FITTING AT STATION 600 AND LONGERON 24R CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.Nov 23, 1998 · N982AX · Doug DC932 · Wing Miscellaneous StructureSDR ABXA9801146Angle · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH ANGLE RIGHT SIDE CRACKED AT LOWER AFT CORNER. REPAIRED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.Nov 23, 1998 · N982AX · Doug DC932 · Vertical StabilizerSDR ABXA9801145Blkhd Fitting · crackedDURING C-CHECK, FOUND RIGHT PYLON BULKHEAD AT STATION 965 INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Nov 23, 1998 · N982AX · Doug DC932 · Nacelle/Pylon, Bulkhead/FirewallSDR ABXA9801144Fitting · crackedDURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERNAL ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.Nov 23, 1998 · N982AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9801143Skin · crackedDURING C-CHECK, FOUND INTERNAL FUSELAGE SKIN AT STATION 1080 CRACKED BETWEEN LONGERON 1R AND 2R. REPAIRED IAW DC9 SRM 53-04.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9801142Skin · crackedDURING C-CHECK, FOUND SKIN CRACKED AT STATION 194, LONGERON 22L. REPAIRED SKIN IAW ABX EA 53300001-003.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABX9801162Longeron · crackedDURING C-CHECK, FOUND LONGERON 2L CRACKED AT STATION 1076. REPAIRED LONGERON IAW DC9 SRM 53-02.Nov 23, 1998 · N982AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800629Fire Loop · malfunctionedFIRE DETECTION LOOP LIGHT ILLUMINATED WITH FIRE HANDLE LIGHT FLICKERING ON NR 1 ENGINE. PERFORMED LOOP TEST PER AOM AND FLIGHT CREW ELECTED TO SECURE NR 1 ENGINE. DECLARED EMERGENCY LANDING BUT LANDING WAS NORMAL AND NO EVACUATION WAS PERFORMED. REPLACED FINov 22, 1998 · N933VV · Doug DC932 · Fire DetectionSDR VJ9800622Retract Mech · malfunctionedNLG WOULD NOT RETRACT AFTER TAKEOFF. ALL GEAR INDICATIONS NORMAL WITH GEAR IN DOWN POSITION. CREW ELECTED TO RETURN TO DEPARTING STATION. INSPECTED GEAR FOR BROKEN, MISSING PARTS, AND LEAKS; NONE FOUND. PINNED GEAR AND FERRIED AIRCRAFT TO ATL MAINTENANCE BNov 22, 1998 · N966VV · Doug DC932 · Landing Gear Retraction/Extension SystemSDR VJ9800634Skin · crackedDURING SCHEDULED INSPECTION, THE FUSELAGE AT FS 965 L16R TO L17R WAS FOUND CRACKED. CUT OUT CRACK, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 51-10-3, 51-20-1, 51-10-4, 53-04 FIGURE 17 AND AIRTRAN RES 981976.Nov 20, 1998 · N947VV · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9801090Web · crackedDURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED UNDER FLOOR TRACK AT RBL 54, STATION 658. REPAIRED IAW DC9 SRM 53-01.Nov 20, 1998 · N982AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9801089Angle · crackedDURING C-CHECK, FOUND VERTICAL ANGLE/BRACKET CRACKED ON OUTBOARD SIDE OF NR 2 PYLON, UNDER THROTTLE CONDUIT JAM NUT. REPLACED BRACKET/ANGLE IAW DC9 SRM.Nov 20, 1998 · N982AX · Doug DC932 · Nacelle/Pylon StructureSDR ABXA9801088Floorbeam · crackedDURING C-CHECK, FOUND FLOORBEAM AT STATION 680 AND LBL 54 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5.Nov 20, 1998 · N982AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9801087Support · crackedDURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 680 AND RBL 44. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.Nov 20, 1998 · N982AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9801086Bulkhead Fitting · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED JUST ABOVE DOOR WARNING SWITCH. REPLACED FITTING IAW DC9 SRM 51-30-5.Nov 20, 1998 · N982AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9801085Floorbeam · corrodedDURING C-CHECK, FOUND FLOORBEAM AT STATION 965 CORRODED FROM LBL 22 TO LBL 44. REPAIRED FLOORBEAM IAW ABX REA D953-25565MR.Nov 20, 1998 · N982AX · Doug DC932 · Fuselage Main, Floor BeamSDR 9811429916Bulkhead Angle · crackedDURING M CHECK, FOUND T ANGLE CRACKED ON BULKHEAD FS 47 NEAR CENTER LINE. REPAIRED PER EA 99-159528.Nov 20, 1998 · N949N · Doug DC932 · Fuselage Main, BulkheadSDR 9811419926Spar Cap · crackedDURING M CHECK, FOUND CRACK ON RIGHT HORIZONTAL STABILIZER XRS 223 UPPER AFT SPAR OUTBOARD END. REPAIRED PER EA 99-159470.Nov 20, 1998 · N926NW · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR VJ9800628Panel · leakingLT WING FUEL ACCESS PANEL LEAKING. FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. INSPECTED AIRCRAFT AND FOUND NO RESIDUAL FLUID BUT INSTALLED DOME NUT ON FUEL INSPECTION PLATE IAW MM 28-00. LEAK CHECKED GOOD.Nov 19, 1998 · N949VV · Doug DC932 · Wing, Plate/SkinSDR VJ9800621O-Riing · failedAFTER TAKEOFF FLIGHT CREW PERCEIVED THE ODOR OF FUMES IN COCKPIT AND ELECTED TO RETURN TO ATL MAINTENANCE BASE. INVESTIGATED BY MAINTENANCE AND FOUND FUEL SHROUD GOING TO APU TO NOT BE PROPERLY SEATED. REPLACED O-RING AND SEAL TO INSURE INTEGRITY OF FUEL LINNov 19, 1998 · N921VV · Doug DC932 · APU Engine Fuel and ControlSDR MWEA981090Structure · bird strikeON CLIMBOUT, AIRCRAFT TOOK MULTIPLE BIRD STRIKES AND RETURNED TO MKE. MKE MTC COMPLETED A BIRD STRIKE INSPECTION AND NO DAMAGE WAS FOUND. REMOVED TWO STRIKE MARKS.Nov 19, 1998 · N204ME · Doug DC932 · Aircraft StructuresSDR VJ9800613Power Supply · inopEMERGENCY LIGHT AT AFT AIR STAIR ENTRY OUT. REPLACED POWER SUPPLY AND BATTERIES, OPS CHECKED GOOD IAW MM 33-00.Nov 18, 1998 · N919VV · Doug DC932 · Emergency LightingSDR MWEA981089Longeron · crackedFOUND LONGERON 13L AT STATION 965 CRACKED. MTC SPLICED IN NEW SECTION OF LONGERON.Nov 18, 1998 · N302ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA981088Longeron · crackedFOUND CRACKS ON LONGERON 16L AND 17L AT STATION 965. MTC SPLICED IN NEW SECTION OF LONGERON.Nov 18, 1998 · N302ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800630Panel · corrodedDURING SCHEDULED INSPECTION AT AERO CORP, FOUND THE R-1 FORWARD AND AFT GIRT BAR ATTACH FITTING IN THE FLOOR SPINNING. MECHANICALLY REMOVED THE CORROSION, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED NEW TRANSITION PANEL IAW DC9 SRM 51-30-2, 51-10-5, 51-Nov 17, 1998 · N947VV · Doug DC932 · Emergency EquipmentSDR VJ9800647Seat Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, THE SEAT TRACK AT FS 398 TO 740 RBL 44 WAS FOUND WITH CORROSION IN NUMEROUS PLACES. REMOVED AND REPLACED THE SEAT TRACK IAW DC9 SRM 53-05 FIG 4F.Nov 16, 1998 · N948VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800633Skin · dentedDURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN AT FS 229 TO 399 L18R TO 26R WAS REMOVED AND REPLACED DUE TO NUMEROUS DENTS OUT OF LIMITS AND TWO LARGE EXISTING REPAIRS.Nov 16, 1998 · N947VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800594Valve · failedDURING INITIAL TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS, FLIGHT CREW RECEIVED A MASTER CAUTION WARNING. FLIGHT CREW APPLIED BRAKES WITH ANTISKID SYSTEM ON AND THERE WAS NO BRAKE PRESSURE. TURNED ANTISKID SYSTEM OFF AND BRAKE PRESSURE WAS AVAILABLE. AIRCRAFT SNov 16, 1998 · N933VV · Doug DC932 · Brake Anti-Skid SectionSDR VJ9800636Seat Tracks · corrodedSCHEDULED INSPECTION, SEAT TRACKS WERE FOUND WITH CORROSION AND OUT OF LIMITS IN THE FOLLOWING LOCATIONS: LBL 22 BS 275 TO 589, LBL 44 BS 275 TO 589, RBL 22 BS 398 TO 550 AND FS 936 TO 996. REMOVED AND REPLACED SEAT TRACKS IAW DC9 SRM 53-05 FIG 4F, 51-10-3 ANov 14, 1998 · N947VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR 9810369985Lamp · failedFLIGHT CREW NOTED THE RIGHT LANDING GEAR INDICATION (GREEN) DID NOT ILLUMINATE UPON LANDING GEAR EXTENSION. LANDING GEAR WAS RECYCLED WITH SIMILAR RESULTS. INDICATOR LAMP WAS REPLACED BY FLIGHT CREW. INDICATION CHECKED NORMAL AND AIRCRAFT LANDED AT DESTINATNov 13, 1998 · N985US · Doug DC932 · Landing Gear Position and WarningSDR VJ9800646Bulkhead Angle · corrodedSCHEDULED INSPECTION, THE ANGLE ON THE PRESSURE BULKHEAD WAS FOUND CORRODED AT L30 FS966. GAINED ACCESS TO AREA, REMOVED AND REPLACED ANGLE. REINSTALLED ALL PARTS REMOVED FOR ACCESS IAW DC9 SRM 51-10-4, 51-30-2, 51-30-1, 51-10-3, AND SB53-147 PG 44.Nov 12, 1998 · N948VV · Doug DC932 · Fuselage Main, BulkheadSDR VJ9800588Battery Pack · dischargedEMERGENCY EXIT LIGHTS IN BUSINESS CLASS FAILED TO DISARM. REPLACED NICAD BATTERY, OPS CHECKED GOOD.Nov 11, 1998 · N901VJ · Doug DC932 · Emergency LightingSDR MWEA981051Slide · fell offTHE GALLEY DOOR SLIDE FELL OFF DOOR. MTC REINSTALLED SLIDE.Nov 11, 1998 · N215ME · Doug DC932 · Emergency EquipmentSDR VJ9800645Skin · corrodedSCHEDULED INSPECTION, THE RIGHT WING UPPER SURFACE FIXED PANEL, FWD OF THE AILERON FROM XRS 445 TO XRS 400 APPROXIMATELY WAS FOUND WITH SURFACE CORROSION ON THE UNDERSIDE IN SEVERAL PLACES. CUT OUT CORROSION AND DELAMINATION IN THE SPECIFIED AREA. FABRICATEDNov 10, 1998 · N948VV · Doug DC932 · Wing, Plate/SkinSDR VJ9800639Skin · crackedDURING A SCHEDULED INSPECTION, THE COCKPIT FLOOR PANEL UNDER THE CO-PILOTS SEAT WAS FOUND CRACKED AND CORRODED AROUND THE SCREW HOLES. REMOVED THE UPPER SKIN, FABRICATED AND INSTALLED A NEW SKIN IAW DC9 SRM 51-30-2 AND 53-21-0 FIG 2D.Nov 10, 1998 · N947VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800587Fuel Pump · failedAFTER TAKEOFF AT 500 FEET ALTITUDE, NR 2 ENGINE FAILED, NO VIBRATION OR BANG EXPERIENCED. FOUND NR 2 ENGINE FUEL PUMP DRIVE SHAFT SHEARED. REPLACED FUEL PUMP IAW DC9 MM 73-10-1 AND FUEL CONTROL REPLACED IAW DC9 MM 73-20-1 AS PRECAUTIONARY MEASURE. OPS CHECKNov 9, 1998 · N925VV · Doug DC932 · Engine Fuel PumpSDR CA981130013Actuator · failed(CAN) UNABLE TO ARM SPOILERS ON APPROACH, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT. REPLACED AUTO SPOILER ACTUATOR.Nov 9, 1998 · Doug DC932 · Leading Edge Slat ActuatorSDR VJ9800584Cover · dislodgedFWD MAIN PASSENGER DOOR SLIDE COVER DISLODGED. REINSTALLED IAW MM 25-62-0 AND PERFORMED REQUIRED INSPECTION.Nov 6, 1998 · N940VV · Doug DC932 · Emergency EquipmentSDR VJ9800638Seat Track · corrodedDURING A SCHEDULE INSPECTION, THE RT O/B SEAT TRACK RBL 44 FS 200 WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, FABRICATED AND INSTALLED REPAIR MEMBER IAW DC9 SRM 53-05 FIG 4F AND 51-10-3.Nov 4, 1998 · N947VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800579Cover · dislodgedFWD PASSENGER DOOR ESCAPE SLIDE COVER DISLODGED WHEN DOOR OPENED. REINSTALLED AND PERFORMED REQUIRED INSPECTION.Nov 4, 1998 · N910VJ · Doug DC932 · Emergency EquipmentSDR CA981230053Spacer · fractured(CAN) NR 2 ENGINE HAD HIGH VIBRATION AFTER TAKEOFF. ENGINE WAS SHUT DOWN AT 16,000 FEET. POST-FLIGHT INSPECTION FOUND THE SPACER BETWEEN THE 3-4 STAGE OF THE TURBINE WITH A 4 PIECE MISSING. THE DAMAGE INITIATED FROM A CRACK IN THE TIE ROD BOLT HOLE INNER THNov 4, 1998 · Doug DC932 · Turbine SectionSDR VJ9800611Skin · dentedDENT AT FS 123L, L23-24. .035 X 1 DX=29, 124L, L23-24, .010 X .25 DX=25, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, CONDITION 1B-3. NO FURTHER ACTION REQUIRED PER AIRTRAN RES 981872.Nov 3, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800610Skin · dentedDENT AT FS 211L, L15, .055 X 3 DX=55, 212L, L15-16, .052 X 3 DX=58, 213L, L15-16, .016 X 1/4 DX=16, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, SHEET 38. COLD WORKED DENTS. VERIFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, Nov 3, 1998 · N937VV · Doug DC932 · Fuselage Main, Plate/Skin
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