Douglas DC-9-32

Service difficulty reports · 12,755

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 = '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 ABXA050244Engine · defectiveNR 1 ENGINE HIGH OIL TEMP. LEFT ENGINE SHUTDOWN AT FLT LEVEL 310 DUE TO OIL TEMP IN THE RED ZONE. INITIALLY TEMP WAS AT TOP OF YELLOW BAND, THEN WENT TO RED, THEN PEGGED ON SHUTDOWN. REMOVED AND REPLACED LEFT ENGINE IAW ABX JOB CARD 90900010.Oct 3, 2005 · N986AX · Doug DC932 · Turbine Engine Oil SystemSDR 0501399921Hose · separatedWHILE CRUISING AT FL 350, THE CABIN PRESS WARNING ILLUMINATED AND INDICATION SHOWED THE CABIN CLIMBING THROUGH 9500 FEET. FLT CREW INITIATED AN EMERGENCY DESCENT DOWN TO 10,000 FT AND DIVERTED TO DTW. LOG PAGE STATES THAT THE CABIN PRESSURE CONTROL RETURNED Sep 4, 2005 · N943N · Doug DC932 · Cabin Pressure Control SystemSDR ABXA050221Spar Cap · crackedRIGHT HORIZONTAL STABILIZER UPPER REAR SPAR TEE CAP MOST OUTBOARD END CRACKED. REPAIRED HORIZONTAL REAR SPAR CAP IAW DC-9 SRM 55-02.Sep 2, 2005 · N900AX · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR ABXA050220Frame · crackedRIGHT FORWARD MAIN FRAME, STA 699, CRACKED AT POINTS G AND J, AFT FLANGE REQUIRED 5935650 REPAIR INSTALLED. REPAIRED MAIN FRAME AT FS 699 IAW EA 53400120-001-1.Sep 1, 2005 · N900AX · Doug DC932 · Fuselage Main, FrameSDR ABXA050219Frame · crackedRIGHT MAIN FRAME STA 718 HAD CRACK IN S/B SECTION. CRACK HAD GROWN INTO ATTACHMENT HOLES FOR REPAIR. FRAME REQUIRED REPLACEMENT PER S/B 53-100. FRAME WAS REMOVED AND REPLACED ON EA 53400324-0021-2.Sep 1, 2005 · N900AX · Doug DC932 · Fuselage Main, FrameSDR ABXA050218Frame · crackedPREVIOUSLY REPAIRED LEFT WHEEL WELL MAIN FRAME 718 HAD SEPARATION IN PREVIOUS CRACKS WITH CORROSION INSIDE CRACKS. ALSO HAD CORROSION AROUND MAIN FRAME BOTTOM BOLT IN FORWARD FLANGE. REMOVED AND REPLACED MAIN FRAME STA 718 LEFT ON JOB CARD EA 53400323-001-2.Sep 1, 2005 · N900AX · Doug DC932 · Fuselage Main, FrameSDR ABXA050191Frame · crackedFRAME 1104 CANTED CRACKED AT LONGERON 14 RIGHT AND LONGERON 15 RIGHT. REMOVED AND REPLACED FRAME IAW DC-9 SRM 51-30-5.Aug 9, 2005 · N989AX · Doug DC932 · Fuselage Main, FrameSDR ABXA050190Attach Angle · crackedFORWARD LOWER CARGO AFT BULKHEAD LOWER ATTACH ANGLES CRACKED AT LONGERON 24 RIGHT. REPLACED ATTACH ANGLES IAW DC-9 SRM.Aug 9, 2005 · N989AX · Doug DC932 · Fuselage Main, Attach FittingsSDR 0501239618Controller · malfunctionedAT FL270 CABIN BEGAN TO CLIMB 2000 FPM. FOLLOWED COM AND RAPID DESCENT TO 10000 FT. MASKS DID NOT DEPLOY. FLT CONTINUED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE CONTROLLER. OPERATION CHECKS GOOD.Aug 6, 2005 · N618NW · Doug DC932 · Cabin Pressure ControllerSDR 0501159950Apu · smokeDURING CRUISE FLIGHT LEFT AFT LAV SMOKE DETECTOR SOUNDED AND CREW REPORTED SMOKE/SMELL. FLIGHT CREW DIVERTED AC TO MKE AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND AN OIL LEAK AT APU GENERATOR DRIVE PAD SEAL. APU AREA CLEANED AND APU PLACED ON MELJul 26, 2005 · N9346 · Doug DC932 · APU Oil SystemSDR 0501119601Duct · separatedWHILE AT CRUISE AT FL350 THE RED "CABIN PRESS" LIGHT ILLUMINATED. COM COMPLIED WITH, FOLLOWED RED BORDERED CHECKLIST, AND A POWER DESCENT WAS INITIATED. CREW WAS ABLE TO RECOVER CONTROL OF CABIN PRESSURE AS THEY PASSED THROUGH FL290 BUT THEN LOST CONTROL AGAINJul 25, 2005 · N601NW · Doug DC932 · Air Distribution SystemSDR 0501109601Control System · malfunctionedIN LEVEL FLIGHT AT FL340 THE CABIN ALTITUDE ROSE ABOVE 10,000 FEET. CREW PERFORMED AN EMERGENCY DESCENT, COMPLIED WITH COM, UTILIZED THE RED BORDERED CHECKLIST, AND DIVERTED TO DEN. CABIN PRESSURE WAS REGAINED AT FL180 BUT CABIN MASKS HAD DEPLOYED. LANDING WASJul 17, 2005 · N601NW · Doug DC932 · Cabin Pressure Control SystemSDR ABXA050168Fitting · crackedNR 2 BEAM AFT END FITTING CRACKED ON AFT LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.Jul 12, 2005 · N986AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA050167Fitting · crackedNR 4 BEAM FORWARD END FITTING CRACKED ON AFT LOWER CARGO DOOR. REMOVED AND REPLACED FITTING AT NR 4 FORWARD BEAM IAW DC-9 SRM 51-30-5.Jul 12, 2005 · N986AX · Doug DC932 · Fuselage Main, Attach FittingsSDR 0500969918Frame · crackedDURING M-CHECK FOUND CRACKED FRAME AT VENTRAL STAIR CUTOUT BS 1087. REPAIRED PER EA 99-203533.Jun 27, 2005 · N940N · Doug DC932 · Fuselage Main, FrameSDR ABXA050164Door Frame · crackedLEFT AFT UPPER DOOR JAMB CRACKED, EMERGENCY EXIT, IN 2 PLACES. REPAIRED LEFT AFT UPPER DOOR JAMB IAW DC-9 SRM 53-05.Jun 17, 2005 · N982AX · Doug DC932 · Fuselage Main, StructureSDR ABXA050163Threshold · corrodedSERVICE DOOR THRESHOLD SKIN BULGING AT STA 176, RIGHT BUTT LINE 58. REPAIRED AREA IAW DC-9 SRM 51-10-2.Jun 16, 2005 · N982AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA050162Frame · crackedSHEAR TIE CRACKED IN RADIUS FRAME STA 813 BETWEEN LONGERON 29 LEFT AND 30. REPAIRED SHEAR TIE IAW DC-9 SRM 53-03 AND DWG SR09530212.Jun 15, 2005 · N982AX · Doug DC932 · Fuselage Main, FrameSDR ABXA050152Outflow Valve · frozenAT 35,000 FEET, RED CABIN PRESS LIGHT ILLUMINATED AND OUTFLOW VALVE WAS FROZEN IN PLACE. ONCE DESCENDED TO FL 190, PRESSURIZATION WORKED OKAY IN MANUAL AND AUTO. OPS CHECKED CABIN PRESS SWITCH IAW DC-9 MM 21-30-00-0-0202. OPS NORMAL, NO DEFECTS NOTED. THISJun 15, 2005 · N900AX · Doug DC932 · Pressure Regulator/Outflow ValveSDR ABXA050161Floorbeam · corrodedLOWER LEG OF FLOORBEAM WAS CORRODED ON UPPER AND LOWER SURFACE AT STA 313, BUTTLINE 38 RIGHT. REPAIRED FLOORBEAM IAW DC-9 SRM 53.Jun 14, 2005 · N982AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA050159Retainer · crackedSTA 756, LONGERON 15 RIGHT, HAD CRACK AT WINDOW RETAINER. REMOVED AND REPLACED DAMAGED CLIP. FABRICATED AND INSTALLED NEW CLIP IAW DACO DWG 3914137 AND DC-9 SRM 51-30-5.Jun 14, 2005 · N982AX · Doug DC932 · Fuselage Main, StructureSDR ABXA050160Retainer · crackedSTA 598, LONGERON 10 RT, HAD CRACK AT WINDOW RETAINER. REPAIRED WINDOW RETAINER AT FS 598, LONGERON 10 RIGHT IAW DC-9 SSRM DWG K07226.Jun 14, 2005 · N982AX · Doug DC932 · Fuselage Main, StructureSDR 0501069623Skin · crackedDURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 69.5 LBL 18. REPAIRED PER EA 96-203594.Jun 10, 2005 · N623NW · Doug DC932 · Fuselage Main, Plate/SkinSDR 0500919623Door Frame · crackedDURING L-CHECK, FOUND CRACK IN FORWARD UPPER CORNER OF FORWARD SERVICE DOOR FRAME. REPAIRED PER EA 96-203593.Jun 9, 2005 · N623NW · Doug DC932 · Fuselage Main, StructureSDR ABXA050128Shear Tie · crackedSHEAR TIE CRACKED AT STA 1090, 8 INCHES OUTBOARD OF RT CENTER LINE. REMOVED AND REPLACED SHEAR TIE AT STA 1090 IAW DC-9 SRM 51-30-5 AND 53-30-2.May 21, 2005 · N980AX · Doug DC932 · Fuselage Internal Mounting StructureSDR ABXA050129Skin · crackedFUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 2 INCHES TO THE RIGHT SIDE OF VERTICAL STAB, SKIN CRACKED OUT OF HI-LOK APPROXIMATELY .25 INCH LONG. REPAIRED FUSELAGE SKIN AT FS 1090, RIGHT SIDE OF VERTICAL STAB IAW DC-9 SRM 53-01.May 20, 2005 · N980AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA050127Skin · crackedFUSELAGE SKIN CRACKED FS 1090, ONE O'CLOCK POSITION FACING AFT. CRACK APPROXIMATELY 2.5 INCHES LONG, LEFT SIDE OF VERTICAL STABILIZER. MANUFACTURED REPAIR DOUBLER FROM 2014T6 .063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01.May 20, 2005 · N980AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA050130Skin · crackedFUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 4 INCHES TO THE LEFT OF VERTICAL STAB. MANUFACTURED REPAIR DOUBLER FROM 2014-T6 .063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01.May 20, 2005 · N980AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 0500669601Line · kinkedAT FL340, CREW NOTICED THE CABIN ALTITUDE CLIMBING THROUGH 10,000 FEET. A RAPID DESCENT WAS INITIATED AND COMPLIED WITH COM PROCEDURES. CONTROL OF THE CABIN PRESSURE WAS REGAINED ON DESCENT WHEN THE AIRFOIL ANTI-ICE WAS SECURED. AIRCRAFT CLIMBED BACK UP TO Apr 30, 2005 · N601NW · Doug DC932 · Cabin Pressure SensorSDR 0500639611Controller · malfunctionedAT FL290 ON DESCENT, THE AIRCRAFT LOST AUTO PRESSURE CONTROL. CREW ATTEMPTED MANUAL CONTROL BUT RIGHT PACK WENT INTO OVERHEAT CONDITION AND SHUT DOWN. CABIN CLIMBED AT 1500 FPM, CREW DECLARED AN EMERGENCY, PERFORMED COM PROCEDURES, AND QUICKLY DESCENDED. PAApr 26, 2005 · N611NA · Doug DC932 · Cabin Temperature ControllerSDR ABXA050097Skin · crackedDURING ROUTINE JOB CARD MAINTENANCE, A CRACK WAS FOUND AT FS 737, BETWEEN LONGERON 1 AND LONGERON 2 RIGHT, SKIN EXTERIOR. REPAIRED AREA IAW DC-9 SRM 53-04 FIG 12B.Apr 24, 2005 · N983AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA050106Door Frame · crackedFORWARD DOOR JAMB CRACKED. INBOARD END FORWARD OF DOOR HINGE. REPAIRED AREA IAW DC-9 SRM 53-01.Apr 19, 2005 · N985AX · Doug DC932 · Fuselage Main, StructureSDR ABXA050087Cusp Web · corrodedCUSP WEB CORRODED AT FS 200, BETWEEN SEAT TRACKS, RBL 44.5 - RBL 54.5. CUT OUT CORRODED SECTION OF CUSP WEB AT FS 200 RBL 49. INSTALLED REPAIR DOUBLER IAW DC-9 SRM 53-01 AND 51-30-5.Apr 7, 2005 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA050233Pan · corrodedSERVICE DOOR PAN CORRODED. REMOVED AND REPLACED LOWER SECTION OF SERVICE DOOR JAMB PAN IAW DC-9 SRM 53-05.Apr 5, 2005 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA050232Cusp Web · corrodedCUSP WEB ANGLE AT SERVICE DOOR THRESHOLD CORRODED. REPAIRED CUSP WEB ANGLE IAW DC-9 SRM 53-05.Apr 5, 2005 · N903AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA050231Skin · crackedFUSELAGE SKIN CRACKED AFT OF SERVICE DOOR CUTOUT, AT LOWER AFT CORNER. REPAIRED AFT LOWER CORNER OF DOOR IAW DC-9 SRM 53-05.Apr 3, 2005 · N903AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA050230Skin · corrodedFUSELAGE SKIN FORWARD OF KIDNEY PANEL WAS BULGING AROUND FASTENERS FROM JUST ABOVE SKIN SPLICE AT LONGERON 26 LEFT TO SPLICE AT LONGERON 26 RIGHT. INNER SKIN CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED NEW SKIN AND LONGERON IAW DC-9 SRM 51-30-2 AND 51-Apr 1, 2005 · N903AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA050229Frame · crackedCENTER OVER WHEEL WELL MAIN FRAME RIGHT SIDE IN WHEEL WELL, HAD CRACK EXTENDING INTO TWO EACH FASTENERS. MAIN FRAME NEEDED REPLACED PER SERVICE BULLETIN DC9-53-100. MAIN FRAME REPLACED ON EA 53400324-001-2.Apr 1, 2005 · N903AX · Doug DC932 · Fuselage Main, FrameSDR 0500489611Spar Cap · crackedDURING M-CHECK FOUND CRACK IN RT WING REAR SPAR CAP AT XRS 267. REPAIRED PER EA 96-201450.Apr 1, 2005 · N611NA · Doug DC932 · Wing SparSDR 0500479611Door Frame · corrodedDURING M-CHECK FOUND CRACK IN LT SIDE AFT ENTRY DOOR JAMB FRAME. REPAIRED PER EA 96-203207.Apr 1, 2005 · N611NA · Doug DC932 · Fuselage Main, StructureSDR ABXA050074Battery · dischargedEMERGENCY EXIT LIGHTS FAILED TO REMAIN ON WITH POWER, FAILURE. REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY IAW DC-9 MM 24-30. OPS CHECKED GOOD.Mar 30, 2005 · N903AX · Doug DC932 · Emergency LightingSDR 0500829606Vertical Support · crackedDURING H-CHECK, FOUND CRACK IN BULKHEAD VERTICAL SUPPORT AT BS 756 L26L AND L26R. REPAIRED PER EA 96-202532.Mar 29, 2005 · N606NW · Doug DC932 · Fuselage Main, BulkheadSDR 0500719983Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT BS 239 LBL 25. REPAIRED PER EA 99-202920.Mar 20, 2005 · N983US · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR 0500359926Computer · malfunctionedWHILE CRUISING AT FL340, THE AUTOPILOT PITCH BEGAN TO FLUCTUATE +/- 500 FPM WHILE IN "ALTITUDE HOLD". FLIGHT CREW SUSPECTED ALTERNATE TRIM WAS CAUSING THE DEVIATIONS. COMPLIED WITH COM PROCEDURES FOR RUNAWAY TRIM AND FLUCTUATIONS STOPPED. THEN AGAIN AT FL12Mar 14, 2005 · N926NW · Doug DC932 · Altitude ControllerSDR 0500509602Stiffener · crackedDURING M-CHECK FOUND CRACK IN BULKHEAD VERTICAL STIFFENER AT BS 756 L28R. REPAIRED PER EA 96-202516.Mar 9, 2005 · N602NW · Doug DC932 · Fuselage Miscellaneous StructureSDR 0500319613Bleed Air Sys · contaminatedDURING ROTATION, SMOKE ENTERED THE COCKPIT AND CABIN. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE FOUND OIL IN NR 1 ENGINE 8TH STAGE BLEED. REPLACED THE NR 1 ENGINE. OPERATIONAL CHECK GOMar 8, 2005 · N613NW · Doug DC932 · Engine Bleed Air SystemSDR ABXA050055Check Valve · not seatedCABIN PRESSURE ANNUNCIATOR ILLUMINATED PASSING 10,000 FT MSL. UNABLE TO PRESSURIZE AIRCRAFT MANUALLY OR WITH AUTOMATIC CONTROLLER. VISUALLY INSPECTED AIRCRAFT, NO DEFECTS NOTED. FOUND GROUND AIR CONDITIONING CHECK VALVE NOT SEATED. MANUALLY CYCLED CHECK VAMar 5, 2005 · N989AX · Doug DC932 · Air Distribution SystemSDR 0500219610Coupling · separatedDURING CRUISE FLIGHT, THE CABIN CONTINUED TO CLIMB. WHEN CABIN PRESSURE REACHED 9500 FEET, THE CREW SWITCHED TO MANUAL PRESSURE CONTROL AND STILL UNABLE TO STOP THE LOSS OF PRESSURE. BOTH PACKS WERE AT FULL COLD WITH 18-20 PSI, ALL ANTI-ICE OFF, AND OUTFLOW Feb 20, 2005 · N610NW · Doug DC932 · Humidity Control SystemSDR 0500259610Stiffener · crackedDURING H-CHECK FOUND CRACK IN AFT CARGO COMPARTMENT FORWARD BULKHEAD VERTICAL STIFFENER AT BS 756 L26L. REPAIRED PER EA 99-201836.Feb 8, 2005 · N610NW · Doug DC932 · Fuselage Main, BulkheadSDR 0500239610Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AND DOUBLER BETWEEN L22 TO L23R. REPAIRED PER EA 96-202500.Feb 2, 2005 · N610NW · Doug DC932 · Fuselage Main, Bulkhead
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