N478CT, cancelled Aug 8, 2014

Service difficulty reports · 43

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 = 'N478CT' AND deregistration_id = 'N478CT-2014-08-08'
  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 22AA201000070Proximity Switch · inoperativeAFTER TAKEOFF WITH GEAR HANDLE UP ALL (4) RED UNSAFE LIGHTS REMAINED ILLUMINATED. COMPLETED APPROPIATED CHECK LIST, NO CHANGE IN THE LIGHTS INDICATION. NOTIFIED ATC, FLIGHT CONTROL AND MX CONTROL. RETURNED TO DEPARTURE. IAW TAFI 32-30-00, R & R PROXIMITY ELECTMay 3, 2010 · N478CT · Doug DC1030F · Landing Gear Position and WarningSDR 22AA201000066Skin · crackedDURING "C" CHECK, LOWER FUSELAGE, ALONG LONGERON 44L, ALONG STA 1701 FUSELAGE SKIN FOUND CRACKED THROUGH. NON-ROUTINE NR 0425, CRACK AREA AT LONGERON 44L ALONG STATION 1701 FUSELAGE SKIN REPAIRED IAW SRM 53-20-00 FIGURE 6 VOLUME I REVISION 96.Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Main, Plate/SkinSDR 22AA201000065Roller Tray · corrodedDURING "C" CHECK, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY FOUND CORRODED AFTER CARGO SIDE GUIDE RAIL REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1697 TO STA 1781. NON-ROUTINE NR 0450, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY REPAIR CARRIEFeb 24, 2010 · N478CT · Doug DC1030F · Fuselage Floor PanelSDR 22AA201000064Seat Track · corrodedDURING "C" CHECK, CABIN CORROSION FOUND ON INNER SURFACE OF SEAT TRACK AT STATION 1139 TO STATION 1156, X= 47.5. NON-ROUTINE NR 0314, SEAT TRACK FROM STATION 1129 TO STATION 1169, X= 47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME 1 REVISION 96.Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 22AA201000063Intercostal · corrodedDURING "C" CHECK, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL FOUND CORRODED AFTER SIDE GUIDE RAIL, REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1764, L42 TO L43L (REFER CNTRL NR 0425). NON-ROUTINE NR 0449, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL REPAIR Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Miscellaneous StructureSDR 22AA201000062Skin · corrodedDURING "C" CHECK, CABIN CORROSION FOUND ON CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT). NON-ROUTINE 0220, CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT) CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01 VOLUME II AT S 21 FFeb 24, 2010 · N478CT · Doug DC1030F · Wing, Center BoxSDR 22AA201000061Rib · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000060Rib · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000059Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED IAW 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FROM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000058Rib · wornDURING "C" CHECK, NR 2 ENG RT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0201, WORN AREA AT NR 2 ENGINE RT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030 · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000057Skin · wornDURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000056Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000055Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000054Rib · wornDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000053Longeron · crackedDURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FFeb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000052Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000051Longeron · crackedDURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000050Longeron · crackedDURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000049Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW EN 1016-10 AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA200900032Control Box · failedANTI-SKID TESTED NORMAL ON BEFORE LANDING CHECKLIST UPON NORMAL LANDING (NO EMERGENCY DECLARED) AND AFTER EXITING RUNWAY TOWER REPORTED OBSERVING SPARKS FROM RT WING LANDING GEAR, EMERGENCY VEHICLES WERE OUT TO INSPECT, FOUND NO FIRE OR DAMAGE, CLEARED TO TAXIDec 19, 2009 · N478CT · Doug DC1030F · Brake Anti-Skid SectionSDR 22AA200900029Oil System · lowENG NR 3 ESN NR 455-780 IN FLIGHT SHUT DOWN DUE TO OIL / PRESS, QTY DROP & COMPRESSOR STALL AND CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 3 ENG. ON ENGINE RUN UP, OPS CHECKED NORMAL.Oct 16, 2009 · N478CT · Doug DC1030 · Turbine Engine Oil SystemSDR 22AA20090404Slide · unwanted deployLOG PAGE NR 130754: L-1 DOOR INADVERTED OPENED (BY GROUND HANDLER) WHILE ARMED DEPLOYING SLIDE. ENTERED ON DMI NR 22611 IAW MEL 52-10-2, CATEGORY ''C''. REMOVED AND REPLACED L1 EVACUATION SLIDE/RAFT CONTAINER IN ACCORDING WITH DC-10 MAINTENANCE MANUAL 25-61-01Apr 30, 2009 · N478CT · Doug DC1030F · Escape SlideSDR 22AA20090102Manifold · crackedAT APPROXIMATELY 1740 Z. ENGINE NR 1 FAILED FUEL PRESSURE, APPROXIMATELY 50 PSI. ATTEMPTED TO START, CROSS FEED FAILED. DIVERT TO SKCL. REMOVED AND REPLACED LT, RT Y-FUEL MANIFOLD NR 1 ENGINE IN ACCORDING WITH MAINTENANCE MANUAL 73-11-01. NO LEAKS NOTED. Jan 6, 2009 · N478CT · Doug DC1030F · Engine Fuel DistributionSDR ARWA20080501Cowling · dentedNR 3 ENGINE NOSE COWL LIP HAS A DENT AT 5 O'CLOCK POSITION. TRANSFERRED TO CARRY-OVER ITEM NR 7584 IN ACCORDANCE WITH ARROW CARGO GMM 5-08-1 AND EO NR AS11722 FOR TRACKING OF DENT.May 16, 2008 · N478CT · Doug DC1030F · Engine Cowling SystemSDR ARWA20080403Control Panel · damagedHEADING KNOB WORKING IN FAST MODE ONLY. ENTERED ON DMI NR 21598 AS PER MEL 22-1-(L) CAT "C". REMOVED AND REPLACED HDG GUIDANCE CONTROL PANEL IN ACCORDANCE WITH M/M 22-00-00. CHECK GOOD IN ACCORDANCE WITH M/M 22-00-00. CLEARED DMI NR 21598; PLACARD REMOVED.Apr 7, 2008 · N478CT · Doug DC1030F · Auto Flight SystemSDR ARWA20080402Adc · malfunctionedNR 1 AUTO PILOT PORPOSES IN CRUISE; TRANSFERRED TO DMI NR 21586 AS PER MEL NR 22-1-2(A) CAT "C". REMOVED AND REPLACED NR 1 AIR DATA COMPUTER IN ACCORDANCE WITH M/M 34-16-01. CHECK GOOD IN ACCORDANCE WITH MM 34-16-00 AND MM 22-10-00 CLEARED DMI NR 21586; PLACApr 7, 2008 · N478CT · Doug DC1030F · Air Data ComputerSDR ARWA20080305Adc · intermittentCAPTAIN'S AIR DATA COMPUTER (ADC) CONTINUOUSLY FAILS IN FLIGHT. REMOVED AND REPLACED NR 1 CAPTAIN'S AIR DATA COMPUTER (CADC) IN ACCORDANCE WITH M/M 34-16-00. NO LEAKS NOTICED AT THIS TIME IN ACCORDANCE WITH M/M 34-11-00.Mar 24, 2008 · N478CT · Doug DC1030F · Air Data ComputerSDR ARWA20080204Engine · stalledDURING ROTATION, NR 3 ENGINE SUFFERED COMPRESSOR STALL AND THE TOWER AND VICINITY AIRCRAFT NOTED FIRE COMING OUT OF ENGINE AFT END. REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH ARROW AIR WORK CARD 143R7101M AND DC-10 M/M 71-00-00. PERFORMED ENGINE RUNFeb 23, 2008 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop)SDR ARWA20080202Connector · dirtyUPON ADVANCING, THE POWER LEVERS FOR TAKEOFF, NR 3 START VALVE LIGHT ILLUMINATED, LIGHT EXTINGUISHED WHEN POWER LEVERS WERE RETARDED TO IDLE. CLEANED AND SECURED CONNECTOR AT NR 3 ENGINE STARTED VALVE, OPERATIONAL CHECK AT BLAST FENCE TAKEOFF POWER IAW MM 71-Feb 3, 2008 · N478CT · Doug DC1030F · Engine Starting System WiringSDR ARWA20071103Wire · brokenAFTER GEAR RETRACTION, NOSE GEAR RED LIGHTS REMAINED ILLUMINATED ON BOTH THE FORWARD AND F/E PANELS, CYCLED GEAR ONCE AS PER CHECK LIST, BUT NO HELP. PERFORMED ELECTRICAL TROUBLE SHOOTING, SYSTEM FOUND BROKEN WIRE AT NOSE GEAR PROXIMITY SENSOR; REPAIRED WIRINNov 7, 2007 · N478CT · Doug DC1030F · Landing Gear System WiringSDR ARWA20071101Handle · stuckAFTER TAKEOFF GEAR HANDLE WILL NOT GO UP. ACCOMPLISHED EXPANDED CHECKLIST, NOT HELP. RETURN TO KMIA. ACCOMPLISHED FUEL DUMP PROCEDURE TO BRING A/C TO MAX LANDING WEIGHT. REMOVED AND REPLACED RUPTURED BOGIE TRIM LINE ON LT MAIN LANDING GEAR. BLEAD SYSTEM Nov 1, 2007 · N478CT · Doug DC1030F · Landing Gear SelectorSDR ARWA20071003Engine · making metalAFTER DEPARTURE FROM SVVA, FELT VIBRATION IN COCKPIT, THEN SMOKE IN COCKPIT, NR 1 ENGINE OIL QUANTITY TO ZERO AND OIL PRESSURE BEGAN FLUCTUATING; SHUTDOWN ENGINE NR 1 AT 1758Z. TROUBLESHOOT NR 1 ENGINE PER TAFI 79-00-00; FOUND METAL CONTAMINATION ON SCAVAGE POct 26, 2007 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop)SDR ARWA20071001Oil System · leakingNR 1 ENGINE OIL QUANTITY STEADY CAME DOWN TO 1 1/2 QUARTS OF OIL REMAINING AND PRESSURE BEGAN TO FLUCTUATE, SHUT DOWN FOR PRECAUTION AT 1321-Z. 10-19-07 FOUND NR 1 ENGINE WAS REMOVED AND REPLACED AS PER ARROW W/C 141R7101M AND DC10 MM 71-00-00. OPERATOct 9, 2007 · N478CT · Doug DC1030F · Turbine Engine Oil SystemSDR ARWA20061201Bleed Valve · malfunctionedNR 3 PNEUMATIC TEMPERATURE HIGH, LIGHT ON; TEMP AT RED LINE. FOUND NR 3 ENGINE FAN AIR VALVE STICKING CLOSED; REMOVED AND REPLACED NR 3 ENGINE FAN AIR VALVE IN ACCORDANCE WITH M/M 36-13-03; ALSO REMOVED AND REPLACED HIGH STAGE TEMPERATURE SENSOR IN ACCORDANCEDec 5, 2006 · N478CT · Doug DC1030F · Compressor Bleed ValveSDR ARWA20060802Flap System · lack of lubeWHEN SELECTING FLAP 15, THE FLAP DISAGREE LIGHT CAME ON AND HAD A SLIGHT ROLL TO THE RIGHT. PERFORMED ABNORMAL CHECK FOR NO FLAPS. LUBED LT & RT WING FLAP AND SLAT SYSTEM IAW MM 12-21-04. PERFORMED TEST FLAP MECHANICAL CONTROL AND TEST FLAP HYDRAULIC ACTUATAug 21, 2006 · N478CT · Doug DC1030F · Trailing Edge Flap Control SystemSDR ARWA20060402Compressor · dirtyBETWEEN 50 AND 60 PERCENT N1 NR 3 ENGINE HEAVY VIBRATION. REMOVED, CLEANED, LUBRICATED AND RE-INSTALLED FIRST STAGE FAN ROTOR BLADES IN ACCORDANCE WITH DC-10 A/M/M PAGE 811, M/M 72-21-00; RAN NR 3 ENGINE AT IDLE P/P AND MAX. NO EVIDENCE OF VIBRATION AT ANY SApr 28, 2006 · N478CT · Doug DC1030F · Turbine Engine Compressor SectionSDR ARWA20060205Indicator · inoperativeNO AIR SPEED ON FIRST OFFICER'S SIDE; TAKEOFF ABORTED AT 90 KTS. PERFORMED ADC BOX SELF TEST NO FLAG SHOWED TO AIR SPEED INDICATOR IN ACCORDANCE WITH DC-10 M/M 34-13-00; MAINTENANCE CONTROL ADVISED.Feb 27, 2006 · N478CT · Doug DC1030F · Airspeed/Mach IndicatorSDR ARWA20051001Unknown · unknownAT TOP OF CLIMB; AIR TRAFFIC CONTROL (ATC) REPORTED AIRCRAFT OFF COURSE. COULD NOT CORRECT AND REQUESTED VECTORS BACK TO SJU. RESET POWER IN A/C, REPROGRAMMED I.N.S. 1-2-3, ALL CHECKED NORMAL. NO FAULTS FOUND IN ACCORDANCE WITH M/M 34-43-0.Oct 6, 2005 · N478CT · Doug DC1030F · Navigation SystemSDR ARWA20050801Wire Harness · burnedNR 1 AUXILIARY PUMP POPS C/B. T/S FOUND WIRE BUNDLE IN RT WHEEL WELL BURNED AT STA. 1381 FORWARD BULKHEAD; REROUTED WIRE BUNDLE RT WHEEL WELL FORWARD BULKHEAD STATION 1381 IN ACCORDANCE WITH 20-50-02; AUXILIARY PUMP CHECKED NORMAL IN ACCORDANCE WITH M/M 29-21Aug 9, 2005 · N478CT · Doug DC1030F · Hydraulic Power System WiringSDR ARWA20050706Windshield · crackedAFTER LANDING CAPTAIN'S WINDSHIELD OUTSIDE CRACKED. REMOVED AND REPLACED CAPT WINDSHIELD IN ACCORDANCE WITH M/M 56-11-00; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 30-41-00 AND M/M 30-42-00 FOUND NORMAL.Jul 31, 2005 · N478CT · Doug DC1030F · Flight Compartment WindowsSDR ARWA20050607Connector · unsecureWEATHER RADAR SYSTEM FAILED DURING FLIGHT (CLIMBOUT); UNABLE TO FIX; RETURNED TO KMIA. CLEANED AND RE-SECURED CONNECTORS AT ANTENNA RADOME; PERFORMED TEST RADAR SYSTEM IN ACCORDANCE WITH M/M 34-41-00; NO DUPLICATE FAIL AT THIS TIME.Jun 24, 2005 · N478CT · Doug DC1030F · Weather Radar SystemSDR ARWA20050604Pump · failedAFTER LANDING IN KMIA, NR 2 ENGINE OIL PRESSURE DROP DOWN TO 20 PSI; SHUTDOWN ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND REMOVED AND REPLACED OIL PUMP IN ACCORDANCE WITH DC-10 M/M 9-20-04. OPERATIONAL CHECK NORMAL IN ACCORDANCJun 10, 2005 · N478CT · Doug DC1030F · Turbine Engine Oil SystemSDR ARWA20050506Transmitter · malfunctionedLOG PAGE NR 117738. DURING TAXI, ENGINE NR 1 OIL PRESSURE INDICATOR DROPPED TO (ZERO). ALL OTHER PARAMETERS NORMAL, RETURN TO BLOCK IAW AOM ALTERNATE PROCEDURES. REMOVED AND REPLACED ENGINE NR 1 OIL PRESSURE TRANSMITTER IAW MM 79-33-01. OPERATIONAL CHECK May 23, 2005 · N478CT · Doug DC1030F · Engine Oil Pressure
Back to N478CT, cancelled Aug 8, 2014