Douglas DC-9-31

Service difficulty reports · 7,433

Newest first. General aviation reporting is voluntary.

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 = 'DC931'
  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 TWAA0007505Floorboard · damagedDURING OP 16 MAINT CHECK, FOUND REPAIRS HAD BEEN MADE TO SOFT SPOTS IN CABIN AISLE FLOOR. FABRICATED PANEL NEW PER SSRM 53-00-104, FIG 201, PAGE 201. TREATED PER SSRM 51-10-3.May 8, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0007504Floorboard · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR PANEL NUMBER 10 WAS CORRODED. NEW FLOOR PANEL FABRICATED PER SRM 6-70-01, PAGE 2, AND SSRM 53-00-104.May 8, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0007503Floorboard · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANELS 7, 12, AND 16 WERE CORRODED. FABRICATED NEW PANEL FOR EACH POSITION PER SSRM 53-00-104.May 8, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR USAAD00068Valve · stuckPIT-ALB - FLT 390 - DURING DESCENT, THE LEFT ENGINE FUEL HEAT LIGHT WAS ON WHEN THERE WAS A FUEL HIGH TEMP LIGHT. A SHORT TIME LATER THE LEFT ENGINE OIL TEMPERATURE GAUGE RAPIDLY APPROACHED THE RED LINE. THE ENGINE WAS SHUTDOWN. THE AIRCRAFT LANDED AT ITS DMay 7, 2000 · N955VJ · Doug DC931 · Fuel HeaterSDR TWAA0007405Angle · crackedLT CANTED KEEL AREA, TIE ANGLE FROM THE LOWER FUSELAGE SKIN TO THE WING IS CRACKED AT A BOLT HOLE FS 608 APPROX. REMOVED CRACKED TIE ANGLE AND INSTALLED NEW TIE ANGLE TWA SN 17-5259 AND INSTALLED FASTENERS PER SRM 51-30-1 AND SRM 51-30-5 AND SEALED. OP-16 05May 5, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0007101Oxygen Mask · deployedIN CRUISE FLIGHT CREW ERROR CONTRIBUTED TO A LOSS OF PRESSURIZATION. PASSENGER OXYGEN MASKS DROPPED AUTOMATICALLY. SEAT ROW 7 RT SIDE THE OXY MASK VALVE PULL PINS WERE MISSING PREVENTING THE FLOW OF OXYGEN, AND AT ROW 22 RT SIDE THE MASKS DID NOT DEPLOY. BOMay 5, 2000 · N976Z · Doug DC931 · Passenger Oxygen SystemSDR TWAA0007203Frame · crackedDURING OP 16 MAINT CHECK, FOUND STA 980 FORMER CRACKED AT LONGERON 17R. REPLACED SECTION OF FORMER FROM FLOOR TO LONGERON 10R, (P/N 9958238-7) PER SRM 53-03.May 3, 2000 · N984Z · Doug DC931 · Fuselage Main, FrameSDR 0001699944Duct · stuckSLAT DISAGREEMENT ANNUNCIATOR ON DURING SLAT EXTENSION ON APPROACH TO MSP. ACCOMPANIED BY A ROLL TO THE LEFT. EXPERIENCED TURBULENCE AND BOTH SLATS EXTENDED. RETRACTED SLATS AND AN UNEVENTFUL NO-SLAT LANDING WAS MADE. MAINTENANCE LUBED ''T'' DUCT AND DEFERMay 2, 2000 · N1309T · Doug DC931 · Leading Edge Slat Control SystemSDR TWAA0007202Skin · lightning strikeDURING OP 16 MAINT CHECK ON THE RT SIDE FUSELAGE WINDOW NUMBER 22, FWD OF EMERGENCY EXIT, HAD LIGHTNING STRIKE ON WINDOW FRAME. ACCOMP EDDY CURRENT ON FRAME AFTER BLENDING. MATERIAL LEFT WAS IN LIMITS AT 0.076, 0.087, AND 0.097. BLENDED PER SRM 53-05, FIG 1May 1, 2000 · N984Z · Doug DC931 · Fuselage Main, Plate/SkinSDR 0001709990Wire · failedSMOKE AND ELECTRICAL SMELL IN COCKPIT. CAPTAIN''S DECLARED AN EMERGENCY AND PROCEEDED TO BUF. SMOKE CLEARED IN 5 MINUTES. CFR WAS CALLED OUT AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND BURNT WIRE TO MAP LIGHT AND PLACED ON MEL. AIRCRAFT RETURNED TO SERVMay 1, 2000 · N8950E · Doug DC931 · Light System WiringSDR TWAA0006805Skin · corrodedIN THE AFT CARGO BIN, FOUND PILLOWING OF FUSELAGE SKIN AT STA 948, LONGERON 28R TO 29, AND AT STA 945 TO 950 LONGERON 30 TO 28R. REMOVED CORROSION PER SRM 51-10-3, PAGE 35, AND SPM 6-80-01 PAGES 1 TO 3. REPAIRED DAMAGED AREA PER SRM 53-04, FIG 128 SHEET 5. Apr 30, 2000 · N992Z · Doug DC931 · Fuselage Main, Plate/SkinSDR USAAD00064Battery · dischargedIND - THE COCKPIT, SERVICE DOOR AND MAIN ENTRY DOOR EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Apr 29, 2000 · N924VJ · Doug DC931 · Emergency LightingSDR TWAA0006906Angle · crackedDURING OP 16 MAINT CHECK, FOUND ON LT PYLON, ANGLE CRACKED BELOW FWD UPPER PYLON COWL LATCH. FABRICATED NEW ANGLE PER SRM 54-10-0, PAGE 5 FIGURE 3 ITEM 21, AND DOUGLAS DRAWING 5910308. TREATED PART PER SRM 51-10-3. REPLACED PART PER SRM 6-70-01.Apr 29, 2000 · N984Z · Doug DC931 · Nacelle/Pylon StructureSDR TWAA0006905Floorboard · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 53 HAD CORROSION ON PANEL SKIN. REPLACED PANEL 53 WITH NEW FABRICATED PANEL AND HAT SECTIONS PER SRM 53-00-104, PAGE 201.Apr 28, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0006801Skin · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FUSELAGE SKIN UNDER FINGER DOUBLER AT STA 775 TO 794, STRINGER 29R TO 30. REMOVED CORROSION PER SPM 6-80-01 AND INSTALLED NEW DOUBLER PER ARA 16722 AND SRM 53-04 FIG 53.Apr 28, 2000 · N984Z · Doug DC931 · Fuselage Main, Plate/SkinSDR USAAD00063Battery · dischargedDAY - THE MAIN ENTRANCE DOOR EMERGENCY EVACUATION SLIDE ACTIVATED LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Apr 27, 2000 · N958VJ · Doug DC931 · Emergency LightingSDR TWAA0006904Floorboard · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR PANEL 38 WAS CRACKED AT BOLT HOLE. REPAIRED CRACK PER SRM 53-05 PAGE 1, CLASS B, FIG 3, PAGE 5. CUT OUT DAMAGE, FILLER AND DOUBLER.Apr 27, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0006802Structure · crackedDURING OP 16 MAINT CHECK, FOUND ON FUSELAGE, THIRD FROM BOTTOM AFT STOP HOLE HAD A CRACK INDICATION PER EDDY CURRENT, FWD ENTRY DOOR, .125 INCH LONG. REPAIRED BY INSTALLING DOUBLER PER EMLR 70776A.Apr 26, 2000 · N984Z · Doug DC931 · Fuselage Main, StructureSDR TWAA0006706Frame · crackedDURING OP 16 MAINT CHECK IN THE AFT ACCY COMPT FOUND CRACK APPROX .75 INCH LONG IN FORMER FOOT AT STA 1059, BELOW LONGERON 15L. CRACK VERIFIED BY NDT. REMOVED AND REPLACED CRACKED FOOT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-60-0. TREATED PART PERApr 26, 2000 · N984Z · Doug DC931 · Fuselage Main, FrameSDR TWAA0006705Floorboard · crackedDURING OP 16 MAINT CHECK, CABIN FLOOR PANEL NUMBER 48 HAD RIB CRACKED AND PANEL END HAD SMALL CRACKS. FABRICATED NEW PANEL PER SRM 53-00-104, PAGE 201.Apr 25, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0006703Frame · damagedDURING OP 16 MAINT CHECK, FOUND ON UPPER FUSELAGE A REPAIR OF A FORMER AT STA 1038, STRINGER 11L AND 12L. REPLACED FORMER AND INSTALLED FASTENERS PER SRM 51-30-2, AND SRM 51-30-5.Apr 25, 2000 · N984Z · Doug DC931 · Fuselage Main, FrameSDR USAAD00061Battery · dischargedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Apr 24, 2000 · N919VJ · Doug DC931 · Emergency LightingSDR TWAA0006606Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND IN CABIN, LT AFT LAV AT STA 983, LBL 53, FLOOR SUPPORT ANGLE HAD MARKED CORROSION. REMOVED CORROSION AND CLEANED AREA PER SPM 6-80-1. TREATED PER SRM 51-10-3.Apr 24, 2000 · N984Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0006605Bolt · corrodedDURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT MOUNTING BOLTS FOR DOOR BUNGEES HAD CORROSION AROUND HEADS, FWD AND AFT BUNGEES. AT AFT CARGO COMPT DOOR CABLE REEL MOUNT, BOLTS WERE REPLACED WITH 4 NEW BOLTS, NUTS, AND WASHERS, PER SRM 51-31 AND 51-10-4.Apr 24, 2000 · N984Z · Doug DC931 · Cargo/Baggage DoorsSDR TWAA0006604Web · crackedDURING OP 16 MAINT CHECK FOUND IN AFT CABIN, A CRACKED MEMBRANE AT RIVET APPROX STA 908, RT SIDE, ABOVE AFT CARGO DOOR HINGE AREA. REPAIRED MEMBRANE AND CUT OUT DAMAGED AREA PER SRM 53-01-00, PAGE 18 FIG 4, SHEET 3. PRIMED PER SRM 51-10-3.Apr 24, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006603Longeron · corrodedDURING OP 16 MAINT CHECK IN RT CANTED KEEL AREA, CORROSION WAS FOUND ON AND UNDER LONGERON 27R, FROM STA 604 TO 634. REMOVED SURFACE CORROSION PER SPM 6-80-01 AND PAINTED FOR CORROSION PROTECTION PER SRM 51-10-3.Apr 24, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0006602Frame · crackedDURING OP 16 MAINT CHECK, FOUND DOUBLER CRACKED BETWEEN STRINGER 15R AND 16R, STA 945. FORMER REPAIRED PER MO 72J14.Apr 24, 2000 · N984Z · Doug DC931 · Fuselage Main, FrameSDR TWAA0006505Floorbeam · damagedDURING OP 16 MAINT CHECK, FOUND IN CABIN CENTER SECTION, FLOOR MEMBRANE DAMAGED AT STA 737 TO 756, RT SIDE. FABRICATED PER SAMPLE PER SRM 53-11-3, ITEM 6. INSTALLED USING ORIGINAL TYPE FASTENERS PER SRM 51-30-2.Apr 24, 2000 · N984Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0006420Stringer · crackedDURING OP 16 MAINT CHECK, STRINGER 29R WAS CRACKED AT STA 585. REMOVED AND REPLACED WITH NEW LONGERON PER SRM 53-02.Apr 23, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0006419Tee Chord · corrodedDURING OP 16 MAINT CHECK, FOUND TEE CORD AT STA 604 BETWEEN LONGERON 28L AND 29L TO L28R AND L29R, HAD CORROSION. REMOVED BAD SECTION OF TEE CORD AND REPLACED PER SRM 53-03.Apr 23, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006418Longeron · crackedDURING OP 16 MAINT CHECK, FOUND CRACK IN LONGERON 30, STA 579R FLANGE. REMOVED AND REPLACED WITH NEW LONGERON PER SRM 53-02.Apr 23, 2000 · N984Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 0001469968Transceiver · failedDURING CLIMB, THE NR 1 AND NR 2 RADIOS FAILED TO TRANSMIT AND HAD INTERMITTENT RECEPTION. AIRCRAFT RETURNED TO MSP AFTER A BRIEF RECEPTION FROM THE TOWER CLEARING THE FLIGHT TO LAND. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BOTH VHF CONTROL PANELS AND AUDApr 22, 2000 · N9332 · Doug DC931 · VHF Communications SystemSDR TWAA0006417Spar Cap · crackedDURING OP 16 MAINT CHECK, ON LT WING A CRACK IN LOWER SPAR CAP AT I/B FLAP HINGE SUPPORT FITTING, I/B LOWER HOLE, WAS FOUND. REPAIRED PER DOUGLAS DRAWING JO60271.Apr 22, 2000 · N984Z · Doug DC931 · Wing SparSDR GTIA000170Battery · overheatedACY - FLT 654 - AS WE PUSHED BACK AFTER ENGINE START SMOKE WAS NOTED COMING FROM VENT HOLE IN E/E COMPARTMENT AREA. SMOKE COMING FROM RIGHT A/C BATTERY VENT HOLE. REMOVED AND REPLACED BOTH A/C BATTERIES. OPS CHECK GOOD IAW DC-9 MM 24-30-01. (M)Apr 21, 2000 · N969ML · Doug DC931 · Battery/Charger SystemSDR TWAA0006608Fastener · corrodedDURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT, RUSTED HARDWARE FROM APPROX STA 898 TO 935, ABOVE AFT CARGO DOOR AT CUSP LINE DOOR HINGE AREA. REPLACED RUSTY FASTENERS PER SRM 51-30.Apr 21, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006607Web · crackedDURING OP 16 MAINT CHECK, FOUND IN AFT CABIN, CRACKED MEMBRANE AT RIVET APPROX STA 925, RT SIDE, ABOVE AFT CARGO DOOR HINGE AREA. REPAIRED MEMBRANE AND CUT OUT DAMAGED AREA PER SRM 53-01, PAGE 18 FIG 4 AND SHEET 3. PRIMED PER SRM 51-10-3.Apr 21, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006416Floorboard · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR PANEL 15 WAS CORRODED. FABRICATED NEW FLOOR PANEL PER SPM 6-70-01, PARAGRAPH 2. TREATED AND PRIMED PER SRM 51-10-3. FABRICATED OUT OF 7075-T6.Apr 21, 2000 · N984Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0006415Skin · bentDURING OP 16 MAINT CHECK, THE NUMBER 2 CARGO DOOR, OUTER SKIN WAS BENT JUST BELOW THE HANDLE. ROUTED AND STRENGHTENED AREA. INSTALLED 3 SCUFF PLATE WITH HL 329-6 HI-LOKS, MS21042L3 NUT AND MS 1252-10L WASHERS PER SRM 52-05, FIG 30 SHEET 1 AND 2.Apr 21, 2000 · N984Z · Doug DC931 · Cargo/Baggage DoorsSDR USAAD00058Control Box · failedPIT-SYR - FLT 521 - UPON LANDING GEAR RETRACTION AFTER TAKEOFF THE RIGHT MLG RED LIGHT ILLUMINATED. THE LANDED WAS CYCLED BUT THE RED LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PROXIMApr 20, 2000 · N981VJ · Doug DC931 · Landing Gear Position and WarningSDR TWAA0006601Casting · crackedDURING OP 16 MAINT CHECK, THE LT WING T/E NR 4 AILERON HINGE CASTING WAS CRACKED IN AFT MOUNT CLIP FOR WING T/E, TOP PANEL. REPLACED CRACKED BRACKET WITH NEW BRACKET USING NON MAGNETIC ATTACHMENTS PER SPM 6-70-01 AND FASTENER INSTALLATION PER SRM 51-30 AND SRApr 20, 2000 · N984Z · Doug DC931 · Wing, Control Surface Attach FittingsSDR TWAA0006414Skin · crackedDURING OP 16 MAINT CHECK, THE FWD LT CABIN DOOR CUTOUT, INNER SKIN HAD A CRACK APPROX .5 INCH FROM STOP HOLE TO DOOR EDGE. EDDY CURRENT BY HFEC 51-00-03 PART 6 CONFIRMED CRACK. INSTALLED DOUBLERS AND REPAIRED PER DOUGLAS PRINT SRO 9530252-7001.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0006413Door Frame · crackedDURING OP 16 MAINT CHECK, FOUND ON FUSELAGE UPPER AFT STOP HOLE HAD CRACK INDICATION .125 INCH LONG PER EDDY CURRENT, AT FWD ENTRY DOOR. INSTALLED DOUBLER AND REPAIRED PER DOUGLAS PRINT SRO 9530252-7001.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006412Frame · corrodedDURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT, CORROSION ON LOWER SIDE OF FORMER AT STA 775, LONGERON 29R TO 30. REMOVED SURFACE CORROSION PER SRM 6-80-01 AND PAINTED PER SRM 51-10-3, FIG 20.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Main, FrameSDR TWAA0006411Web · corrodedDURING OP 16 MAINT CHECK, IN AFT CARGO COMPT, FOUND WEB FROM STA 935 TO 943, LONGERON 25R TO 29R, WAS CORRODED. REMOVED SURFACE CORROSION PER SPM 6-80-01. PAINTED PER SRM 51-10-3, FIG 20.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006410Floor Support · crackedDURING OP 16 MAINT CHECK IN AFT CARGO COMPT FOUND CRACKS IN FLOOR SUPPORT ON FORMER AT STA 889, LONGERON 29R TO 28R. REMOVED FLOOR SUPPORT, STOP DRILLED AND HAD IT WELDED PER SSRM 53-00-16. TREATED PER SRM 51-10-30. REINSTALLED USING ORIGINAL TYPE HARDWARE.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006409Bracket · corrodedDURING OP 16 MAINT CHECK, AFT CARGO COMPT FLOOR SUPPORT MOUNT BRACKET AT STA 889, BETWEEN LONGERON 27R AND 28R, WAS CORRODED. REMOVED BRACKET AND FABRICATED NEW BRACKET PER SRM 53-11-3, FIG 3A, SHEET 2 ITEM 17. INSTALLED AND TREATED PER SRM 51-10-3.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006408Floor Support · crackedDURING OP 16 MAINT CHECK, FOUND IN CABIN NUMBER 5 FLOOR PANEL SUPPORT HAD A CORNER CRACKED. INSTALLED REPAIR DOUBLER PER SRM 53-01.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006407Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND IN CABIN, TOP OF VERTICAL STIFFENER WAS CRACKED ON REAR PRESSURE BULKHEAD, ABOVE THE AFT ENTRY DOOR STRINGER NUMBER 1, FWD SIDE OF BULKHEAD. REPAIRED STIFFENER PER SRM 53-01, PAGE 10 FIG 2.Apr 20, 2000 · N984Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA0006406Floor Support · crackedDURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT CRACKS IN FORMER FLOOR SUPPORT AT STA 870, LONGERON 30 TO 28R. REMOVED CRACKED FORMER FLOOR SUPPORT FOR WELDING REPAIR AND SSRM 53-00-106. REINSTALLED USING ORIGINAL HARDWARE PER SRM 51-30-2 AND SRM 51-30-51Apr 19, 2000 · N984Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006405Floorboard · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR PANEL NUMBER 71 WAS CORRODED. FABRICATED NEW PANEL WITH 2024-T3, 0.040 PER SSRM 53-00-104.Apr 19, 2000 · N984Z · Doug DC931 · Fuselage Floor Panel
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