Douglas DC-9-14

Service difficulty reports · 1,736

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 = 'DC914'
  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 0401939153Pulley · wornON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND THE RT FLAP INDICATOR WAS AT 30 DEGREES. CREW EXECUTED MISSED APPROACH PROCEDURES TO ALLOW TIME FOOct 26, 2004 · N8912E · Doug DC914 · Trailing Edge Flap Control SystemSDR COOSDR040041Fitting · crackedFUSELAGE NOSE LANDING GEAR WHEEL WELL RT SIDE AT Y STA 69.55-X 24 INCH -Z16 INCH FITTING (PN 49568801) WITH CRACK. (K)Sep 24, 2004 · N700ME · Doug DC914 · Fuselage, Landing Gear Attach FittingsSDR ABXA040302Pan · corrodedWHILE PERFORMING AN X-RAY OF THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB, FOUND THE LOWER DOOR JAMB PAN PRIOR SERVICE REWORK REPAIR CORRODED BEYOND LIMITS. REMOVED AND REPLACED SERVICE REWORK DOOR JAMB PAN P/N J060228-9 IAW DC-9 SRM 53-05.Aug 30, 2004 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR 0400339155Line · brokenAT FL330, THE CABIN BEGAN TO CLIMB AT 500 FPM AND COULD NOT BE CORRECTED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT AND THEN WAS ABLE TO CLIMB BACK TO A HIGHER ALTITUDE IN STAGES. EVENTUALLY THE AIRCRAFT HAD TO DESCEND BACK DOWN TO 17,000 FT TO MAINTAFeb 28, 2004 · N8914E · Doug DC914 · Pressure Regulator/Outflow ValveSDR 0400099152Line · leakingTHE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED SAFELY AT 100 KTS AT IND. MAINTENANCE FOUND THE PRESSURE LINE ON THE RIGHT HYDRAULIC SYSTEM ELECTRIC PUMP LEAKING. PRESSURE LINE, SYSTEM FILTER, AND ENGINE DRIVJan 11, 2004 · N8911E · Doug DC914 · Hydraulic System, MainSDR COOSDR030065Floor Support · crackedAFT AND FORWARD CARGO COMPARTMENT, FLOOR SUPPORT LATERAL ANGLES AT B/S Y:STA 351, 427, 465, AND 737 BETWEEN LONG 28L AND 28R, WITH CRACKS.Jan 1, 2004 · N600ME · Doug DC914 · Fuselage Miscellaneous StructureSDR 0302149150Controller · malfunctionedDURING CLIMBOUT ON DEPARTURE, THE OUTFLOW VALVE STARTED FLUCTUATING FULL OPEN TO FULL CLOSE. AT FL240, THE AIRCRAFT LOST PRESSURIZATION ACCOMPANIED WITH MASK DEPLOYMENT. ALL WARNING INDICATORS ILLUMINATED, AN EMERGENCY DESCENT WAS PERFORMED, AND THE FLIGHT RDec 5, 2003 · N8908E · Doug DC914 · Cabin Pressure ControllerSDR MWEA030442Switch · intermittentINTERIOR TAIL CONE RELEASE HANDLE SWITCH IS INTERMITTENT. REMOVED AND REPLACED SWITCH.Nov 4, 2003 · N700ME · Doug DC914 · Emergency EquipmentSDR ABXA030443Floor Support · crackedFLOOR SUPPORT STRAP, ATTACH ANGLE CRACKED, FS 768 AT LONGERON 27 RIGHT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.Oct 31, 2003 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR ABXA030442Floor Support · corrodedSTA 218 FLOOR SUPPORT WAS CORRODED ABOVE LONGERON 30. REPAIRED FRAME AT FS 218, LONGERON 30 IAW DC-9 SRM 53-03.Oct 31, 2003 · N925AX · Doug DC914 · Fuselage Miscellaneous StructureSDR ABXA030441Skin · corrodedRIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5.Oct 30, 2003 · N925AX · Doug DC914 · Wing, Plate/SkinSDR ABXA030440Fitting · crackedAFT LOWER CARGO DOOR, TRAILING EDGE NR 5 BEAM END FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.Oct 30, 2003 · N925AX · Doug DC914 · Cargo/Baggage DoorsSDR 0302039153Rib · crackedDURING L-CHECK FOUND CRACK IN PYLON CLOSING RIB AT STATION YN 165 LT. REPAIRED PER EA 91-196348.Sep 27, 2003 · N8912E · Doug DC914 · Nacelle/Pylon, Frame/Spar/RibSDR MWEA030318Fuel Control · malfunctionedCREW OBSERVED THE N2 SLOWLY DROP TO 40 PERCENT. REMOVED AND REPLACED ROD END AND PERFORMED ENGINE TRIM ALL PARAMETERS NORMAL. ALSO REPLACED FUEL CONTROL.Aug 18, 2003 · N700ME · Doug DC914 · Fuel Control/Turbine EnginesSDR 0301439153Reservoir · defectiveWHILE AT CRUISE, THE RIGHT HYDRAULIC PRESSURE LOW ANNUNCIATOR LIGHT ILLUMINATED. THE RIGHT HYDRAULIC PRESSURE AND HYDRAULIC QUANTITY INDICATORS WENT TO ZERO. COMPLIED WITH COM PROCEDURES AND LANDED WITH LANDING GEAR DOORS OPEN. MAINTENANCE FOUND THE RIGHT HJul 31, 2003 · N8912E · Doug DC914 · Hydraulic Reservoir, MainSDR 0301329156Skin · crackedDURING "L" CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 19. REPAIRED IAW EA 91-195858.Jul 25, 2003 · N8915E · Doug DC914 · Fuselage Main, Plate/SkinSDR 0301369156Skin · crackedDURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 LBL 18 TO LBL 19. REPAIRED PER EA 91-195861.Jul 21, 2003 · N8915E · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA030286Starter · failedLEFT ENGINE WOULD NOT START. REMOVED AND REPLACED LEFT STARTER.Jul 8, 2003 · N700ME · Doug DC914 · Engine CrankingSDR 0301029151Seal · leakingCLIMBING THROUGH FL 270 THE "CABIN PRESSURE" WARNING ILLUMINATED. CABIN WAS AT 10,000 AND 4.2 PSI DIFFERENTIAL WITH OUTFLOW VALVE FULLY CLOSED. BOTH PACKS WERE INDICATING NORMAL PRESSURE. CREW INITIATED AN EMERGENCY DESCENT WITH POWER ON TO FL 170 UNTIL CABIN May 20, 2003 · N8909E · Doug DC914 · Passenger/Crew DoorsSDR MWEA030199Windshield · crackedFIRST OFFICER'S WINDOW SUDDENLY CRACKED. REMOVED AND REPLACED WINDSHIELD.May 1, 2003 · N600ME · Doug DC914 · Flight Compartment WindowsSDR MWEA030191Wire · arcedA BURNING ODOR WAS NOTICED IN THE COCKPIT AND SMOKE WAS OBSERVED COMING OUT OF THE FIRST OFFICERS MAP LIGHT AREA. FOUND GROUND WIRE TO RHEOSTAT BROKEN CAUSING WIRE TO ARC. REMOVED AND REPLACED FIRST OFFICER'S LIGHT ASSEMBLY.Apr 29, 2003 · N700ME · Doug DC914 · Light System WiringSDR MWEA030143Packing · leakingEPR DROPPED DOWN TO DOWN SLIGHTLY ADVANCED THROTTLE, POWER CAME ON BACK AFTER A FEW MORE MINUTES, POWER STARTER FALLING AGAIN. REMOVED AND REPLACED RIGHT PRESSURE AND DUMP VALVE LINE PACKING.Mar 21, 2003 · N700ME · Doug DC914 · Fuel Controlling SystemSDR MWEA030134Control Valve · inoperativeLEFT BRAKE DOES NOT WORK WITH RIGHT HYDRAULIC SYSTEM SELECTED. REMOVED AND REPLACED RIGHT WHEEL WELL BRAKE CONTROL VALVE.Mar 9, 2003 · N500ME · Doug DC914 · Master Cylinder/Brake ValveSDR ABXA030081Wire · burnedPRIMARY TRIM NR 1 CIRCUIT BREAKER TRIPPED. FOUND WIRES C104C10, C1203C10, C1202C10, C1202B10, C1203B10, C1204B10, C1213A10, C1213B10, C1211B10 BURNED. FOUND WIRE C1205D16 NOT CONNECTED. FOUND RELAY R20-16 BADLY BURNED. REPAIRED ALL WIRING AND REPLACED RELAFeb 19, 2003 · N925AX · Doug DC914 · Electrical Power System WiringSDR 0204199153Engine · damagedENGINE NR 1 FAILED AND SHUTDOWN AFTER A THRUST REDUCTION AT 17,000 FEET. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND ENGINE FOD DAMAGE AND REPLACED THE ENGINE.Dec 29, 2002 · N8912E · Doug DC914 · Engine (Turbine/Turboprop)SDR 0203899150Separator · contaminatedDURING CLIMB, SMOKE AND FUMES ENTERED THE CABIN WITH ASSOCIATED LAVATORY SMOKE DETECTORS ACTIVATING. AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE FOUND WATER SEPARATORS SATURATED WITH OIL. MAINTENANCE REPLACED THE WATER SEPARATORS AND PERFORMED ENGINE BURN OFF Nov 20, 2002 · N8908E · Doug DC914 · Humidity Control SystemSDR MWEA020690LongeronPOSSIBLE CRACK AT STATION 525 LONGERON 7 RIGHT REQUIRES INTERNAL OPEN UP FOR VISUAL INSPECTION. -- FABRICATED AND INSTALL LONGERON SECTION AND REPAIR SPLICES.Nov 12, 2002 · N600ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA020689Shear Tie · crackedSHEAR TIE AND DOUBLER AT STATION 840 LONGERON LEFT 14 CRACKED. -- FABRICATED AND INSTALLED FORMER.Nov 12, 2002 · N600ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA020687Gear · defectiveCREW REPORTED GEAR DOOR OPEN LIGHT STAYED ON WITH GEAR HANDLE UP. -- REMOVED AND REPLACED STIFFENER.Nov 8, 2002 · N500ME · Doug DC914 · Landing Gear DoorsSDR MWEA020670Doubler · crackedAFT CARGO DOOR DOUBLER AT HANDLE IS CRACKED. -- FABRICATED NEW REPAIR DOUBLER, INSTALLED NEW DOUBLER.Nov 8, 2002 · N600ME · Doug DC914 · Fuselage Main, FrameSDR MWEA020668Ring · brokenLANDING GEAR HANDLE WOULD NOT RETRACT. -- FOUND NOSE LANDING GEAR PISTON INNER RING BROKEN AND DAMAGED SEVERAL PARTS. REPLACED #74 RING, #75 SPACER, #77 VALVE, #80 RETAINER AND #82 STOP.Oct 31, 2002 · N700ME · Doug DC914 · Landing Gear Retraction/Extension SystemSDR MWEA020630Landing Gear · malfunctionedCREW WAS UNABLE TO RAISE LANDING GEAR. -- FOUND TENSION ON CABLE RUN 116 A & B LOW. PERFORMED STEPS 1-5 OF ADJUSTMENT TEST, SERVICED NOSE STRUT AND REMOVED AND REPLACED LEFT AND RIGHT NOSE TIRE.Oct 24, 2002 · N700ME · Doug DC914 · Landing Gear Retraction/Extension SystemSDR MWEA020596Floorbeam · corrodedRIGHT LAV FLOOR BEAM AT FRAME STATION 817 HAS CORROSION AROUND 3 NUTPLATES APPROXIMATELY 24" RIGHT OF CENTER LINE. -- REMOVED DAMAGED AREA, FABRICATED, LOCATED AND DRILLED REPAIR ANGLE, INSTALLED REPAIR ANGLE,FILLER AND NUTPLATES.Sep 25, 2002 · N700ME · Doug DC914 · Fuselage Main, Floor BeamSDR MWEA020595Frame · crackedCRACK ON FRAME AROUND FASTENER HOLE AT FRAME STATION 25 RIGHT SIDE OF NOSE WHEEL WELL AREA ABOUT 1" DOWN FROM CEILING. -- REMOVED FASTENERS, FABRICATED AND LOCATED REPAIR DOUBLER AND INSTALLED DOUBLER.Sep 25, 2002 · N700ME · Doug DC914 · Fuselage Main, FrameSDR 0203189154Bulkhead · crackedDuring Hck in ATL, a typical crack was found in the pressure panel at sta 105 and X=35. Also, corrosion was found between x=-25 and x=-35. Repaired per EA 91-190674.Sep 22, 2002 · N8913E · Doug DC914 · Fuselage Main, StructureSDR MWEA020577Attach Angle · crackedRIGHT SIDE OF VERTICAL TO FUSELAGE ATTACH ANGLE HAS A CRACK AT STATION 951. -- STOP DRILLED CRACK, DRILLED HOLES IN REPAIR ANGLE, INSTALLED REPAIR ANGLE, REMOVED HIGH AND LOW FASTENERS AND INSTALLED OVERSIZED FASTENERS. REINSTALLED HEAD KNOCKER COVER PANEL.Sep 20, 2002 · N700ME · Doug DC914 · Fuselage Main, StructureSDR MWEA020578Slide · defectiveTAILCONE EMERGENCY SLIDE WILL NOT DEPLOY WHEN TAILCONE IS DROPPED USING TAILCONE SLIDE. -- REMOVED TAILCONE PANEL, ADJUSTED FORWARD HOLD DOWN STRAP ON SLIDE COVER AND REINSTALLED TAILCONE.Sep 20, 2002 · N700ME · Doug DC914 · Escape SlideSDR 0203179154Skin · crackedDuring Hck in ATL, cracks have been found on the fuselage skin at sta 503 between L17 and L18 LHS. Repaired per EA 91-190691.Sep 13, 2002 · N8913E · Doug DC914 · Fuselage Main, StructureSDR 0203169154Skin · corrodedDuring an HCK in ATL, two areas of corrosion were found in the fuslage skin. Repaired per EA 91-190676.Sep 13, 2002 · N8913E · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA020541Window Frame · tool damageWINDOW FRAME RETAINER FOR THE MOST FORWARD RIGHT PLUG WINDOW LOWER FORWARD CORNER HAS TOOL MARKS STATION 218 RIGHT -- BLENDED TOOL MARKS FABRICATED AND INSTALLED ANGLE.Sep 11, 2002 · N700ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA020540Floorboard · corrodedFLOOR BOARD ATTACH FASTENER HOLES AND FORWARD EDGE LIGHTLY CORRODED ON SEAT TRACK #3 BETWEEN STATIONS 200 AND 218. -- REMOVED CORROSION, LOCATED AND DRILLED NEW SEAT TRACK, INSTALLED NUTPLATES.Sep 6, 2002 · N700ME · Doug DC914 · Fuselage Main, Attach FittingsSDR MWEA020538Floorboard · corrodedFLOORBOARD ATTACH FASTENERS HOLES ARE LIGHTLY CORRODED ON J-CHANNEL BETWEEN STATIONS 160 AND 200 FORWARD OF SEAT TRACK 4. REMOVED CORROSION AND INSTALLED FLOOR SUPPORT.Sep 5, 2002 · N700ME · Doug DC914 · Fuselage Floor PanelSDR MWEA020537Elevator · crackedLEFT ELEVATOR LOWER FORWARD SPAR FLANGE IS CRACKED APPROXIMATELY 2" AT STATION XE200. -- FABRICATED AND INSTALLED REPAIRED PART.Sep 5, 2002 · N700ME · Doug DC914 · Elevator Control SystemSDR 0203159154Longeron · crackedDuring Hck in ATL, a crack was found in the forward end of longeron 29L at staion 361 under a production splice. Repaired per EA 91-190684.Sep 4, 2002 · N8913E · Doug DC914 · Fuselage Main, StructureSDR 0202869151Controller · malfunctionedLOST PRESSURIZATION AT FL290, CABIN ALTITUDE WENT TO 12,000 FEET. CREW INITIATED A RAPID DESCENT TO 10,000 FEET. MASKS DID NOT DEPLOY. AUTO PRESSURE CONTROLLER RESTORED CABIN PRESSURE CONTROL BUT CONTINUED TO OPERATE ERRATICALLY IN AUTO. AIRCRAFT LANDED SASep 4, 2002 · N8909E · Doug DC914 · Cabin Pressure ControllerSDR ABXA020123Link · crackedNR 2 LOWER AFT LEFT THRUST REVERSER DRIVER LINK WAS CRACKED. REPLACED THE NR 2 LOWER LEFT DRIVE LINK IAW DC-9 MM 78-31-05-2-0001, NEA 7830001, TASK NEA 13435, AD 75-14-06, AD 96-10-11, AND SERVICE BULLETIN 78-66.Aug 23, 2002 · N925AX · Doug DC914 · Engine Thrust ReverserSDR 0202789150Engine · failedDURING TAKEOFF ROLL, THE RIGHT ENGINE EXPERIENCED AN UNCONTAINED FAILURE AND RELATED ENGINE FIRE. CREW ABORTED TAKEOFF AND DISCHARGED THE RIGHT ENGINE FIRE BOTTLE. MAINTENANCE REPLACED THE FIRE BOTTLE AND RIGHT ENGINE. AIRCRAFT RETURNED TO SERVICE.Aug 22, 2002 · N8908E · Doug DC914 · Engine (Turbine/Turboprop)SDR MWEA020513Stiffener · crackedRADIAL STIFFENER AT 5 O'CLOCK POSITION IS CRACKED AT ATTACH FASTNER LEFT ENGINE. -- REMOVED AND REPLACED STIFFENER.Aug 14, 2002 · N800ME · Doug DC914 · Engine Cowling SystemSDR MWEA020511Stiffener · crackedRECEPTACLE UNDER RADIAL STIFFENER AT 10 O'CLOCK POSITION #6 LEFT FOUND TO BE CRACKED IN 2 PLACES. -- DRILLED UP AND INSTALLED RECEPTACLE.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA020501Stiffener · crackedAFT PRESSURE BULKHEAD RADIAL STIFFENER ON AFT SIDE AT 10 O'CLOCK POSSITION HAS A SMALL CRACK AT THE RIGHT SIDE. -- FABRICATED AND INSTALLED STIFFENER.Aug 14, 2002 · N800ME · Doug DC914 · Fuselage Main, Bulkhead
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