N1804, cancelled Nov 8, 2013

Service difficulty reports · 44

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N1804' AND deregistration_id = 'N1804-2013-11-08'
  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 ARWA20021201WindshieldLOG PAGE # 109140. DISCREPANCY: APPROACHING FL350, CAPTAIN'S WINDSHIELD DEVELOPED MULTIPLE CRACKS. CORRECTIVE ACTION: REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-2; ALSO CAPTAIN'S WINDSHIELD CONTROLLER IAW MM 30-41-1. FOUND NORMAL OPS CHECK.Dec 1, 2002 · N1804 · Doug DC862 · Flight Compartment WindowsSDR ARWA20020903Transceiver · failedNR 2 RADAR ON CAPTAIN'S SIDE WILL NOT PAINT GROUND RETURNS OR WEATHER. NR 2 RADAR ON FIRST OFFICER'S SIDE WILL NOT PAINT GROUND RETURN OR WEATHER AND RADAR SPIKES. AIRCRAFT RETURNED TO DEPARTING BASE. REMOVED AND REPLACED NR 2 RADAR TRANSCEIVER IAW MM 34-0Sep 7, 2002 · N1804 · Doug DC862 · Weather Radar SystemSDR ARWA20020902Bleed ValveLOG PAGE # 112879. DISCREPANCY: DURING TAXI NOTICED # 3 ENGINE COMPRESSOR STALLING ACCELERATION OF ENGINE. CORRECTIVE ACTION: REMOVED AND REPLACED # 3 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3. OPERATIONS CHECKED OK; RUNUP FOUND NORMAL IAW DC-8 MM 71-00Sep 3, 2002 · N1804 · Doug DC862 · Compressor Bleed ValveSDR ARWA20020507Spar · crackedDURING C-CHECK, NR 4 PYLON INTERIOR, STA YN 165, RM UPPER CHORD WITH 4 INCH CRACK. REPAIRED UPPER SPAR CAP OF NR 4 PYLON IAW AS ELEVEN INC DRAWING AS 11403, SHEET 1 TO 6. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.May 7, 2002 · N1804 · Doug DC862 · Nacelle/Pylon, Frame/Spar/RibSDR ARWA20020502Splice · crackedDURING C-CHECK, FORWARD LOWER CARGO COMPARTMENT FUSELAGE FS 340, FS 360, FS 380, FS 400, FS 420, FS 440 & FS 460; LBL 62.5 FLOORBEAM SPLICE WITH 2.750 INCH CRACK. REMOVED AND REPLACED FLOORBEAM SPLICE PLATE IAW AS ELEVEN INC DRAWING AS 11077, SHEET 1 OF 9, DAMay 6, 2002 · N1804 · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA20020501Longeron · crackedDURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON L-21L AT FUSELAGE FS 280 WITH 2 INCH CRACK. FABRICATED SHIM & REPAIR ANGLE IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. INSTALLED PARTS IAW AS ELEVEN, INC DRAWING AS 11410, SHEET 1 & 2. ISSUED FAA FORMMay 6, 2002 · N1804 · Doug DC862 · Fuselage Main, Longeron/StringerSDR ARWA20011211Fitting · excess playDEPARTING KATL, GEAR NOT LATCHED LIGHT ILLUMINATED. ABNORMAL CHECKLIST COMPLETED AND LIGHT DID NOT EXTINGUISH, AFTER EACH UPLATCH CHECK (IN UPLATCH CHECK POSITION). CORRECTED PLAY AT RIGHT MLG UPLOCK ROLLER FITTING, ALSO LUBRICATED ALL GEARS. LANDING GEAR ODec 20, 2001 · N1804 · Doug DC862 · Landing Gear Position and WarningSDR ARWA20011205EngineLOG PAGE 101856. DISCREPANCY: ON ADVANCING THROTTLE FOR TAKE OFF #4 ENGINE HUNG, CARRIED OUT ABNORMAL PROCEDURE FOR ENGINE HUNG WITH THRUST LEVER IN REVERSE ENGINE STARTED TO ACCELERATE. CANCELED REVERSE THRUST ENGINE CONTINUED TO ACCELERATE WITH THROTTLE CLOSDec 11, 2001 · N1804 · Doug DC862 · Engine Fuel and ControlSDR ARWA0011008Indicator · inoperativeCAPTAIN COMPASS INOP, RETURNED TO KMIA. REMOVED AND REPLACED PICTORIAL DEVIATION INDICATOR IAW MM 34-00. PERFORMED OPERATIONAL CHECK IAW 34-21-0, FOUND ALL SYSTEMS NORMAL.Oct 16, 2001 · N1804 · Doug DC862 · Directional Gyro and Indicating SystemSDR ARWA0010602Selector Valve · leakingHYDRAULIC PRESS LOST OUT OF SLLP. AILERON AND RUDDER POWER LIGHTS CAME ON, CHECKLISTS WERE COMPLETED AND DIVERTED TO SPIM. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HYDRAULIC SYSTEM SELECTOR VALVE IAW MM 29-10-18. OPERATIONAL CHECKED OK, NO LEJun 3, 2001 · N1804 · Doug DC862 · Hydraulic System, MainSDR ARWA000401Engine · malfunctionedMIA - FLT 517 - NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY DROPPED TO .5 GALLON. A PRECAUTIONARY ENGINE SHUTDOWN WAS PERFORMED. OIL PRESSURE WAS DECREASING AND OIL TEMP WAS INCREASING. MAX TEMP WAS 125 CELSIUS AND LOWEST OIL PRESSURE WAS 37Apr 6, 2000 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR ARWA990703Outflow Valve · lack of lubeMIA - FLT 627 - UNABLE TO PRESSURIZE AIRCRAFT IN AUTO OR MANUAL DURING TAKEOFF. DUMPED FUEL AND RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT INVESTIGATED FOR DEFECTS. PRESSURIZATION NORMAL IAW MM 21-30-00. LUBED OUTFLOW VALVE AS PRECAUTIONARY. CHECKED NORMAJul 25, 1999 · N1804 · Doug DC862 · Pressure Regulator/Outflow ValveSDR ARWA990701Wheel · failedCLO - FLT 627 - INBOURND TO CALI, MESSAGE THAT MLG TIRE HAD SEPARATED FROM AIRCRAFT ON TAKEOFF FROM QUITO, ECUADOR. AIRCRAFT LANDED IN CALI WITHOUT INCIDENT. INSPECTION FOUND NR 2 MLG OUTBOARD WHEEL HALF BEAD HAD SEPARATED AND TIRE EJECTED. INCURRED DAMAGE Jun 27, 1999 · N1804 · Doug DC862 · Wheel/Ski/FloatSDR ARWA990307Oil Pump · failedMIA - NR 4 ENGINE OIL PRESSURE DROPPED TO 32 PSI. SHUTDOWN ENGINE AS PER ABNORMAL CHECKLIST. WINDMILL SPEEDS WERE N1, 13.5 PERCENT, N2 21 PERCENT, OIL PRESS 3 PSI. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 ENGINE OIL PUMP ASSY Mar 25, 1999 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR ARWA981221Fcu · failedPNX - FLT 515 - BLOCK TURNBACK, ON RIGHT RUNUP, NR 1 ENGINE DIDN'T ACCELERATE. ALL INDICATIONS REMAINED IN IDLE. INDICATION WITH SLIGHTLY FLUCTUATING EPR NEEDLE. FELT ENGINE VIBRATING AND HEARD 'KNOCKING' NOISE. IMMEDIATELY BROUGHT THROTTLE BACK TO IDLE ADec 29, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine EnginesSDR IH987518001Strut · damagedUPON DISASSEMBLY OF RT MLG STRUT FOR SEAL CHANGE, P/N 3598295 FOLLOWER FOUND TO BE FRACTURED CAUSING DAMAGE TO P/N 37673709-501 ADAPTER ASSY PACKING, P/N 3598375 SPACER. UPPER BEARING SPLIT, P/N 3598297 HEAD, PISTON, AND P/N 3598296 VALVE, REBOUND CHECK. VISDec 7, 1998 · N1804 · Doug DC862 · Main Landing Gear Strut/Axle/TruckSDR ARWA981064Vert Gyro · malfunctionedCAPT'S ADI GYRO FAILS IN ALL TURNS INTERMITTENTLY IN LEVEL FLIGHT ALSO WINDSHEAR FAIL ILUMINATED AT THE SAME TIME. R/R #1 VERT. GYRO I.A.W. DC-8 M/M 34-25-1 OPS CHECK OF HORIZONTAL SYSTEM, GOOD ON GROUND I.A.W. DC-8 M/M 34-25-0.Oct 30, 1998 · N1804 · Doug DC862 · Attitude Gyro and Indicating SystemSDR ARWA980602Fuel Contl Unit · failedAIR TURNBACK, AFTER DEPARTURE NR 3 ENGINE UNSPOOLED AND WHEN POWER LEVER WAS ADVANCED ENGINE WOULD NOT ACCELERATE. RETURNED TO TUS WITHOUT INCIDENT. INSPECTED ENGINE INLET, TAILPIPE, OIL AND FUEL FILTERS. NO DEFECTS NOTED. REMOVED AND REPLACED FCU, MAIN OIJun 6, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine EnginesSDR ARWA980506Mechanism · out of adjustIN FLT RETURN DUE TO LOUD RATTLING NOISE FROM NOSE WHEEL WELL AREA. UNABLE TO PRESSURIZE AIRCRAFT AUTO OR MANUALLY. ADJUSTED NOSE GEAR DOOR PER MM 32-10-0. RUN UP ENGINES PRESSURIZED OK IN MANUAL, AUTO INOP OPEN DMI ON AUTO PRESS. (M)May 19, 1998 · N1804 · Doug DC862 · Landing Gear Door Retract SectionSDR ARWA980407Hyd Line · leakingLOST HYDRAULIC FLUID TO STAND PIPE LEVEL, HYDRAULIC LOSS OF FLUID, EMERGENCY CHECKLIST WAS PERFORMED. PRESSURE CHECK OK. ABNORMAL CHECKLIST WAS FOLLOWED TO AND BEFORE LANDING CHECKS. LANDING AND ROLL-OUT WERE UNEVENTFUL. PRECAUTIONARY A/C TOW IN WAS REQUESApr 20, 1998 · N1804 · Doug DC862 · Hydraulic System, MainSDR ARWA980309Link · bentON OPENING OF MAIN CARGO DOOR FOUND FOUR LONG LINK ASSYS BENDING. REMOVED AND REPLACED 4 LONG LINK ASSY FOR FWD ACTUATOR END, FOUR ACT. AFT AND FWD IAW CARGO CONVERSION MM CHIP 7-08. OPS NORMAL ALL INDICATIONS NORMAL SEVERAL TIMES.Mar 30, 1998 · N1804 · Doug DC862 · Cargo/Baggage DoorsSDR ARWA980207Bolt · shearedUNABLE TO MOVE AILERONS IN MANUAL TO RIGHT. UNABLE TO MOVE RIGHT RUDDER PEDAL UPON FURTHER INSPECTION FOUND SHEARED BOLT AT LT MANUAL REVERSION MECHANISM LINKAGE JAMMING LINKAGE. REMOVED AND REPLACED BOLT, AILERON REVERSION SYSTEM OPS. CHECKED NORMAL IN MANFeb 24, 1998 · N1804 · Doug DC862 · Aileron Control SystemSDR ARWA980201Engine · failedCHECK NR 2 ENGINE FOR VIBRATIONS NR 2 THROTTLE AND START LEVEL HARD IN CRUISE. ACCOMPLISHED R/B 8269 REMOVED AND REPLACED NR 2 ENGINE IAW ARROW AIR J/C 6519 AND J/C 6528, OPERATIONS AND LEAK CHECKED NORMAL ON RUN UP, IAW J/C 6527.Feb 2, 1998 · N1804 · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA971006Filter · defectiveNR 2 ENGINE OIL PRESSURE ILLUMINATED, PERFORMED ABNORMAL CHECKLIST, LIGHT GOES OUT AFTER THROTTLE RETRACTED PARAMETERS MONITORED CONTINUED NORMAL OPERATION. DURING APPROACH LIGHT CAME ON, ENGINE PRECAUTIONARY SHUT DOWN AT 05044 Z. REMOVED AND REPLACED MAIN OOct 29, 1997 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR ARWA970604Cap · missingHYDRAULIC FAILURE IN CRUISE, HYD PRESS ZERO WITH MAIN PUMPS OR AUX PUMP, QUANTITY AND TEMP OK. FOUND MAIN HYD RESERVOIR CAP MISSING. REFILLED 15 GAL OF HYD FLUID. PERFORMED COMPLETE HYD POWER SYSTEM IAW MM 29-00. INSTALLED AND SAFETIED NEW CAP.Jun 19, 1997 · N1804 · Doug DC862 · Hydraulic Reservoir, MainSDR ARWA970601Battery Pack · dischargedMIA - FLT 615 - DURING PRE-FLIGHT INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECK NORMAL IAW MM 33-50-1. AMENDMENT TO ORIGINAL ARWA970601. (X)Jun 17, 1997 · N1804 · Doug DC862 · Emergency LightingSDR 95ZZZX6354Antenna · malfunctionedAIR TURN-BACK, RADAR UNRELIABLE AND PAINTING ERRATICALLY. REPLACED RADAR ANTENNA; OPS CHECK NORMAL.Oct 27, 1995 · N1804 · Doug DC862 · Weather Radar SystemSDR 95ZZZM668Skin · corrodedDURING B-3 INSPECTION, FOUND LEVEL 2 CORROSION AT LEFT WING LEADING EDGE ATTACH POINT STATION X 526. CORROSION REMOVED AND FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER OF .63 INCH 7075T6 AND .071 INCH 7075T6. PRIMED WITH ALODINEOct 16, 1995 · N1804 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM667Relief Valve · stuck openAFTER 27 MINUTES FLIGHT TIME, NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN AT 13:45Z. UPON INSPECTION AT BRO, FOUND OIL PRESSURE RELIEF VALVE NOT REGULATING. REPLACED RELIEF VALVE. ENGINE OPS CHECK NORMAL IAW MM 79-32-0.Oct 9, 1995 · N1804 · Doug DC862 · Turbine Engine Oil SystemSDR AR091351Skin · crackedFUSELAGE OUTER SKIN CRACKED 1.50 INCHES IN UPPER AFT CORNER OF FWD ENTRY DOOR CUT-OUT. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC-8 SB 53-075, AND DAC DWG SR 0850021. BLIND FASTENERS TO BE REPLACED AT NEXT C-CHECK PER DACO FAX DATED 9-15-95. (X)Sep 13, 1995 · N1804 · Doug DC862 · Fuselage Main, Plate/SkinSDR 95ZZZX3452Skin · corrosionLEFT WING INBOARD SLOT L/E HAS LEVEL 2 CORROSION. REPAIRED IAW SRM 57-2-1.Jul 6, 1995 · N1804 · Doug DC862 · Leading Edge DevicesSDR 95ZZZX3453Fitting · crackedDURING PRE-FLIGHT, MAINTENANCE CHECK FOUND LT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0.Jul 5, 1995 · N1804 · Doug DC862 · Elevator StructureSDR 95ZZZM266Fitting · crackedDURING PREFLIGHT MAINTENANCE CHECK, FOUND LEFT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0.Jul 5, 1995 · N1804 · Doug DC862 · Elevator StructureSDR 95ZZZX3457Floor Support · crackedDURING B-CHECK INSPECTION, FOUND RIGHT WW AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACKED AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39.Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZX3451Angle · crackedDURING B-CHECK INSPECTION, THE RT INBOARD FLAP, OUTBOARD, FORMER AND SCISSOR PANEL ATTACHMENT ANGLES FOUND CRACKED IN 2 LOCATIONS, BOTTOM AREA. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE IAW DER ARW 12565-128.Jul 3, 1995 · N1804 · Doug DC862 · Trailing Edge FlapsSDR 95ZZZX3449Floor Support · crackedDURING C-CHECK INSPECTION, FOUND THE RT W/W AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACK AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39.Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM268Longeron · corrodedPOPPED RIVET HEADS AND SKIN BULGE AT FS 208.00 AT LONGERON 28R. REMOVED SECTION OF LONGERON 28R AND TWO INTERCOSTALS. FOUND LEVEL 2 CORROSION ON L-28R. REPLACED 20 INCH SECTION OF L-28R AND REINSTALLED INTERCOSTALS PICKING EXISTING HOLES IAW SRM 53-2-2 AND 5Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Main, Longeron/StringerSDR 95ZZZM265Skin · corrodedLEFT ELEVATOR LOWER SKIN HAS LEVEL 2 CORROSION AT XE 195.33. SKIN SECTION REMOVED. FABRICATED NEW SKIN USING OLD AS TEMPLATE. INSTALLED NEW SKIN SECTION IAW SRM 55-2-0, 51-1-8 AND 51-1-21. REBALANCED ELEVATOR IAW SRM 51-4-4, DC8 SB 27-185 AND DOUGLAS FAX FJul 3, 1995 · N1804 · Doug DC862 · Elevator, Plate/SkinSDR 95ZZZM267Te Skin · corrodedFOUND LEVEL 2 CORROSION LEFT ELEVATOR OUTBOARD STATIC WICK ATTACH POINT. REMOVED LEFT ELEVATOR. REMOVED DAMAGED T/E SECTION. FABRICATED AND INSTALLED NEW T/E SECTION IAW SRM 51-1-21A. INSTALLED NEW STATIC WICK BASE IAW MM 23-60-00. REINSTALLED ELEVATOR AFMay 29, 1995 · N1804 · Doug DC862 · Elevator, Plate/SkinSDR 95ZZZX3450Slot Door · corrosionON A TYPE SERVICE 'A', FOUND RT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS' HEADS. CUT OUT DAMAGED AREAS, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED IAW SRM 57-2-1, FIGURE 2H.Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZW658Slot Door · corrodedON 'A' CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL II CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE.Apr 25, 1995 · N1804 · Doug DC862 · Leading Edge DevicesSDR 95ZZZW657Slot Door · corrodedON 'A' CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL II CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. (W)Apr 25, 1995 · N1804 · Doug DC862 · Leading Edge DevicesSDR 95ZZZM264Slot Door · corrodedON A-CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE. REMOVED SLOT DOOR L/E SECTION, CUT OUT DAMAGED AREAS, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/E.Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM263Slot Door · corrodedON A-CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. REMOVED SLOT DOOR L/E. CUT OUT DAMAGED AREAS, FABRICATED ADN INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/EApr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/Skin
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