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 ABXA9600142Frame · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A SPLICE REPAIR AT LONGERON 17L WITH A GAP AT THE LEFT FUSELAGE FRAME AT FS 639. REPAIRED FRAME IAW ABX REA D953-12780-MR.Nov 14, 1995 · N989AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9600123Web · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL 2 CORROSION ON THE WEBS AROUND THE AFT BAG BIN DOOR JAMB. REPLACED ALL WEBS AROUND AFT BAG BIN DOOR JAMB IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 14, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9522109608Frame · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 1168 CANTED FRAME BETWEEN LONGERONS 21L TO 22L. REPAIRED FRAME (P/N 9911843-501), PER EA 99-103125.Nov 14, 1995 · N608NW · Doug DC932 · Fuselage Main, FrameSDR 9518239608Blkhd Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD T-CAP TO FLOORBEAM TIE FITTING FS 996, RIGHT SIDE. REPLACED CASTING PER SRM 51-30-5 AND DWG 5911546.Nov 14, 1995 · N608NW · Doug DC932 · Fuselage Main, BulkheadSDR 9518029984Eel Power Supply · inoperativeDURING LINE CHECK, FOUND RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY, OPERATIONAL CHECK GOOD.Nov 14, 1995 · N984US · Doug DC932 · Emergency LightingSDR ABXA9600122Jamb · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL 2 CORROSION ON THE AFT BAG BIN DOOR JAMB. REPAIRED AFT BAG BIN DOOR JAMB IAW DC-9 SRM 53-05 FIG 44 SHEET 4.Nov 13, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9517949942Battery Pack · dischargedDURING LINE CHECK, FOUND THE FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED FOUR BATTERY PACKS, OPERATIONAL CHECK GOOD.Nov 13, 1995 · N3991C · Doug DC932 · Emergency LightingSDR CAL951117Angle · corrodedHOU - INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 160 - STA 200. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. (X)Nov 12, 1995 · N17533 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950913Eel Wires · brokenFLT NR 1080 - IAH - AN EMERGENCY FLOOR TRACK LIGHT IN FORWARD COACH SECTION WAS FOUND PULLED LOOSE AND THE LIGHT WAS INOPERATIVE. MAINTENANCE FOUND THE TRACK LIGHT HAD BROKEN WIRES. THE WIRING WAS REPAIRED AND THE TRACK WAS REINSTALLED. (M)Nov 12, 1995 · N27509 · Doug DC932 · Emergency LightingSDR ABXA9600163Doubler · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LOWER FORWARD CARGO COMPARTMENT DOOR JAMB LOWER DOUBLER CORRODED. REPAIRED DOOR JAMB DOUBLER IAW ABX REA D953-13204-MR.Nov 12, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9518219613Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 1.5 INCH CRACK IN SUPPORT MOUNT FITTING FS 1038 AT LONGERON 14R. REPLACED FITTING PER SRM 51-00.Nov 12, 1995 · N613NW · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95365Evac Slide · looseCREW REPORTS, UPON LANDING THE GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE BECAME LOOSE. MAINTENANCE RESECURED ESCAPE SLIDE, RETURNED A/C TO SERVICE.Nov 11, 1995 · N203ME · Doug DC932 · Emergency EquipmentSDR ABXA9600166Doubler · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A DOUBLER AT XRS 58.0 ON THE LEFT WING LOWER SURFACE CORRODED AND BLENDED OUT OF SRM LIMITS. REPLACED DOUBLER IAW DC-9 SRM 51-30-4, 51-30-5 AND REPAIRED FASTENER HOLES IAW ABX REA D957-12559.Nov 11, 1995 · N989AX · Doug DC932 · Wing Miscellaneous StructureSDR ABXA9600143Skin · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A REPAIR ON THE LOWER CENTER WING SKIN AT FS 658 BETWEEN BL 4.0 AND 24.0 THAT WAS NOT PER THE DC-9 SRM. REPAIRED LOWER WING CENTER SKIN IAW ABX REA D957-12798-MR.Nov 11, 1995 · N989AX · Doug DC932 · Wing, Plate/SkinSDR 95ZZZM750Wire · brokenSHV - DURING LANDING, WHEN GEAR HANDLE WAS EXTENDED, RIGHT GEAR RED AND GREEN LIGHTS DID NOT ILLUMINATE. A FLY-BY WAS PERFORMED TO ENSURE GEAR WAS DOWN AND LOCKED. REPLACED BROKEN WIRE, REFERENCE WIRING DIAGRAM 32-61-00. OPERATIONAL CHECK NORMAL.Nov 11, 1995 · N924L · Doug DC932 · Landing Gear System WiringSDR 95ZZZM710Relay · malfunctionedUPON ARRIVAL OF FLT 586, TPA TO ATL, EMERGENCY POWER WOULD NOT TURN OFF. MAINTENANCE REPLACED R2-7 TRANSFER BUS SENSE RELAY AND R2-7 GROUND REFUEL RELAY. (M)Nov 11, 1995 · N915VV · Doug DC932 · AC Generation SystemSDR CAL951112Longeron · crackedHOU - INSPECTION FOUND A 1.25 INCH CRACK AT FORWARD END OF LONGERON 13R. A NEW SPLICE AND LONGERON WAS INSTALLED IAW SRM 51-10-3. (X)Nov 10, 1995 · N17533 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL951111Belt Frame · crackedHOU - INSPECTION FOUND A .75 INCH CRACK IN BELT FRAME AT STA 1109, LONGERON 1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-11-4, FIGURE 4. (X)Nov 10, 1995 · N17533 · Doug DC932 · Fuselage Main, FrameSDR ABXA9600160Press Panel · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK IN AN EXISTING REPAIR ON THE UPPER PRESSURE PANEL LEFT SIDE AT FS 80. REPAIRED PRESSURE PANEL IAW ABX REA D953-13160-MR.Nov 10, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600154Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FUSELAGE SKIN DENTED, GOUGED AND CORRODED FROM FS 289 TO FS 588R, BETWEEN LONGERONS 18 AND 26R. REPLACED SKIN PANEL IAW DC-9 SRM 51-30-2, 51-30-5 AND ABX REA D953-13035-MR.Nov 10, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500933Uplock Switch · iced upNOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER RAISING GEAR ON TAKEOFF. RECYCLED GEAR, LIGHT REMAINED ON. LIGHT DID GO OUT ONCE WE SLOWED TO 170 KIAS. FOUND ICE AROUND UPLOCK SWITCH. REMOVED ICE AND ALL ICE IN NOSE WHEEL WELL AREA. LUBED NOSE GEAR, GEAR DOOR ACNov 10, 1995 · N903AX · Doug DC932 · Landing Gear Position and WarningSDR ABXA9600145Skin · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A REPAIR AT THE EXTERNAL POWER DOOR CUTOUT AT STATION 89L NOT PER THE SRM. REPAIRED SKIN IAW ABX REA D953-12801-MR.Nov 9, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 9518309950Fuel Control · malfunctionedNR 1 ENGINE EXPERIENCED COMPRESSOR STALLS ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTROL ASSEMBLY, PRBC AND PERFORMED A FULL ENGINE TRIM. SUBSEQUENT RUNUP WAS SATISFACTORY.Nov 9, 1995 · N9346 · Doug DC932 · Fuel Control/Turbine EnginesSDR 9517809987Eel Power Supply · malfunctionedDURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK GOOD.Nov 9, 1995 · N987US · Doug DC932 · Emergency LightingSDR 9518199603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 29R END FITTING AT FS 756. REPLACED FITTING PER SRM 51-00 AND 51-30.Nov 8, 1995 · N603NW · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600183Fitting · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29L END FITTING CRACKED BETWEEN FS 579 AND 598. REPLACED LONGERON END FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 7, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600182Fitting · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29R END FITTING CRACKED BETWEEN FS 579 AND 598. REPLACED END FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 7, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9500931Windshield · brokenOUTER PANE OF CAPTAIN'S WINDSHIELD SHATTERED AT FL 330, DURING CLIMB TO FL350. CREW DECLARED AN EMERGENCY AND LANDED AT IAH WITHOUT FURTHER INCIDENT. REPLACED WINDSHIELD IAW DC-9 MM 56-10-2.Nov 7, 1995 · N901AX · Doug DC932 · Flight Compartment WindowsSDR 96ZZZM69Clamps · looseFLT NR 278 - ATL-CMH - THE AIRCRAFT EXPERIENCED A TAIL COMPARTMENT HIGH TEMP INDICATION, THE FLIGHT DIVERTED TO CHA. FOUND SEVERAL LOOSE CLAMPS ON LEFT PACK AND FLOW CONTROL VALVE TIGHTENED SAME. RAN TO 1.9 EPR, NO LEAKS NOTED. (M)Nov 7, 1995 · N933VV · Doug DC932 · Cabin Cooling SystemSDR 9517559925Transceiver · failedDURING CRUISE, WEATHER RADAR RETURNS WERE INTERMITTENT. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER. OPERATIONAL TEST GOOD.Nov 7, 1995 · N925US · Doug DC932 · Weather Radar SystemSDR GTIA96NK134Support · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CHANNEL WITH CORROSION BETWEEN Y503 AND Y522, LONGERON 21 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK132Longeron · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 20, 21, 22 WITH CORROSION BETWEEN Y965 AND Y980 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK130Beam · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT HORIZONTAL BEAM WITH CORROSION BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK129Longeron · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 24 RIGHT WITH CORROSION BETWEEN Y945 AND Y980. REMOVED CORROSION AND TREATED METAL IAW 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK128Longeron · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT ATTACH FITTINGS ON LONGERONS 25 RIGHT AND 26 RIGHT WITH CORROSION IN Y945. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK127Skin · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN AND CHANNELS WITH CORROSION BETWEEN Y945 AND Y965 LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1 AND 53-04 FIG 38. (m)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA96NK126Frame · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y965 WITH CORROSION BETWEEN LONGERON 19 LEFT AND 23 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK125Frame · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y980 WITH CORROSION BETWEEN LONGERON 23 LEFT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK124Support · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL FLOOR SUPPORT PANELS WITH CORROSION BETWEEN Y 756 AND Y 889, LONGERON 27 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK123Longeron · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 24 LEFT WITH CORROSION IN SEVERAL PLACES BETWEEN Y889 AND Y965. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK122Skin · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN Y889 AND Y916, LONGERON 28 LEFT AND 29 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 53-04. AREA WITHIN LIMITS IAW SRM 53-04 FIG 38. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA96NK121Support · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y889 LONGERON 27 LEFT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 51-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK120Frame · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y935 WITH CORROSION BETWEEN LONGERON 25 LEFT AND 30 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK119Longeron · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29 RIGHT AND FRAME Y869 WITH CORROSION. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK118Frame · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y889 WITH CORROSION BETWEEN LONGERON 29 RIGHT AND 27 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK117Channel · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL WITH CORROSION SPOTS BETWEEN Y756 AND Y775 ON LONGERON 26 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA96NK116Longeron · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FILLING SUPPORT FLOOR PANEL WITH CORROSION IN Y775 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)Nov 6, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9522099608Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE INNER SKIN AT LONGERON 18L BETWEEN FS 205 TO 209. REPAIRED SKIN (P/N 5956879-1), PER EA 99-103113.Nov 6, 1995 · N608NW · Doug DC932 · Fuselage Main, Plate/SkinSDR 9518179608Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 996 FITTING BETWEEN LONGERONS 27L TO 28L. REPLACED FITTING PER SRM 51-01.Nov 6, 1995 · N608NW · Doug DC932 · Fuselage Miscellaneous StructureSDR 9517429991Eel Power Supply · failedDURING LINE CHECK, FOUND THREE AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD.Nov 6, 1995 · N8957E · Doug DC932 · Emergency Lighting
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