N478AC, cancelled Mar 21, 2013

Service difficulty reports · 28

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 = 'N478AC' AND deregistration_id = 'N478AC-2013-03-21'
  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 CALA0001586Harness · burnedMAINTENANCE FOUND APU FEEDER CABLES BURNT AT TERMINAL BLOCK S3-23 STA 148 WHILE TROUBLESHOOTING PLACARD ON APU. TWO SECTIONS OF APU FEEDER CABLE WIRE WERE SPLICED FROM STA 220 UP TO TERMINAL BLOCK S3-23 IAW MM 20-50-01. THE TERMINAL BLOCK WAS ALSO REMOVED ANOct 12, 2000 · N478AC · Doug DC982 · AC Power Distribution SystemSDR CALA0001005Battery · inoperativeTHE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00.Jul 3, 2000 · N478AC · Doug DC982 · Emergency LightingSDR CALA0000594Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHT AT ROWS 9 - 14 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5-32 PER MAINTENACE MANUAL 33-53-00 PAGE 501.May 3, 2000 · N478AC · Doug DC982 · Emergency LightingSDR CALA9900876Fitting · crackedINSPECTION FOUND A 1 CRACK IN L-1 DOOR LOWER HINGE FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-10-4.Jul 27, 1999 · N478AC · Doug DC982 · Passenger/Crew DoorsSDR CALA9900856Support · damagedINSPECTION FOUND ELONGATED BOLT HOLES IN FORWARD BAGGAGE BIN FLOORBOARD SUPPORT BEAM AT STA 465 FROM STRINGER 227R TO 27L. THE FLOORBOARD SUPPORT BEAM AND FASTENERS WERE REPLACED IAW ECRA 5320-01588.Jul 23, 1999 · N478AC · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900855Skin · crackedINSPECTION FOUND A 1.25 INCH CRACK IN SKIN AT FASTENER HOLE OF STA 200-207, LONGERON 15L. THE SKIN WAS REPAIRED IAW EA PD80-53-006.Jul 21, 1999 · N478AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900854Skin · dentedINSPECTION FOUND RT O/B FLAP PANEL O/B LOWER SURFACE DENTED WITH A BULGE ON O/B END. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3.Jul 21, 1999 · N478AC · Doug DC982 · Trailing Edge FlapsSDR CALA9900812Skin · delaminatedINSPECTION FOUND RUDDER TRIM TAB DELAMINATED ON TRAILING EDGE AT AFT TOP CORNER AND BOTTOM CORNER. THE RUDDER TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-2 AND SRM 51-90-2.Jul 8, 1999 · N478AC · Doug DC982 · Rudder, Tab StructureSDR CALA9900811Track · corrodedINSPECTION FOUND AFT CARGO TIE DOWN TRACK CORRODED AT STA 1007-1155. THE TIE DOWN TRACK WAS REPLACED IAW SRM 51-30-1.Jul 8, 1999 · N478AC · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900810Skin · crackedINSPECTION FOUND THE RT LOWER FUSELAGE SKIN AFT OF NOSE GEAR CRACKED COMPLETELY THROUGH. REMOVED AND INSTALLED LOWER FUSELAGE SKIN IAW SRM 53-05.Jul 8, 1999 · N478AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900853Skin · gougedINSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT L-1 DOOR AFT CUTOUT. REPAIRED IAW SRM 53-05, FIGURE 26A.Jun 28, 1999 · N478AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9800990Air Seal · wornTHE NR 1 ENGINE FAILED ACCOMPANIED BY A LOUD BANG DURING CLIMB-OUT OF EWR AT 10,000 FEET. THE CREW SHUT THE ENGINE DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND AJun 7, 1998 · N478AC · Doug DC982 · Turbine Engine Compressor SectionSDR CALA9800723B-Nut · looseWHEN HYDRAULICS WERE SWITCHED TO LOW DURING CLIMBOUT. THE LEFT HYDRAULIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO. THE LEFT SWITCHES WERE TURNED TO OFF AND THE LEFT HYDRAULIC QUANTITY SLOWLY INCREASED TO 16 QUARTS. THE FLIGHT WAS CONTINUED TO ATL WHERE IT Apr 29, 1998 · N478AC · Doug DC982 · Hydraulic System, MainSDR CALA9701237Blade · failedTHE NR 1 ENGINE GAVE OFF A LOUD BANG AND QUIT DURING CLIMBOUT. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED C-7 BLADE FAILURE.Aug 24, 1997 · N478AC · Doug DC982 · Turbine Engine Compressor SectionSDR CALA9700790Fitting · brokenINSPECTION FOUND THE RT WING LEADING EDGE NR 3 SLAT OUTBOARD TRACK ATTACH FITTING BROKEN. A NEW FITTING WAS INSTALLED IAW SRM 51-00.May 15, 1997 · N478AC · Doug DC982 · Leading Edge DevicesSDR CALA9700792Longeron · corrodedINSPECTION FOUND LONGERON 22L CORRODED JUST AFT OF FUSELAGE STA 1287 BELOW AFT NOZZLE VALVE. A REPAIR WAS INSTALLED IAW SRM 53-02.May 7, 1997 · N478AC · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA9700794Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED IN TWO AREAS JUST AFT OF MAIN CABIN DOOR AT STA 218 AND 237. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-01535.May 6, 1997 · N478AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9700793Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 320, LONGERON 21. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, PAGE 39.May 6, 1997 · N478AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9700791Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING FIXED LEADING EDGE NOSE RIB TWENTY INCHES OUTBOARD OF NR 2 SLAT TRACK (XRS 30) AND A .75 INCH CRACK WAS FOUND FOURTEEN INCHES OUTBOARD OF NR 2 SLAT TRACK (XRS 25). DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW May 5, 1997 · N478AC · Doug DC982 · Wing, Rib/BulkheadSDR CALA9601857Wire · failedTHE CIRCUIT BREAKER FOR CENTER FUEL TANK AFT BOOST PUMP POPPED AND ALL FUEL QUANTITY GAUGES WENT BLANK AT TAKEOFF. BOTH A AND B CHANNELS WERE BLANK. THE CIRCUIT BREAKER WAS RESET, BUT IT POPPED AGAIN. THE CIRCUIT BREAKER FOR FUEL QUANTITY POWER TRANSFER WASDec 19, 1996 · N478AC · Doug DC982 · Electrical Power System WiringSDR CALA9601557Apu · leaking oilSMOKE WAS REPORTED IN THE AFT AND FORWARD SECTION OF CABIN DURING INITIAL CLIMB OUT OF IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU INLET AND BLEED OIL SOAKED. THE APU WAS REMOVED AND REPLACED. THE APU INNov 4, 1996 · N478AC · Doug DC982 · APU Oil SystemSDR CALA9601543Apu · overservicedSMOKE AND ODOR ENTERED THE CABIN SHORTLY AFTER TAKEOFF. BOTH THE SMOKE AND ODOR DISAPPEARED AFTER PULLING THE RECIRCULATING FAN CIRCUIT BREAKER. MAINTENANCE FOUND NO PROBLEMS WITH THE RECIRCULATING FAN. THE APU WAS CLEANED AND RUN WITH NO LEAKS NOTED. MAINNov 1, 1996 · N478AC · Doug DC982 · APU Oil SystemSDR CAL951048Strut · low pressureFLT NR 0289 - CLE - THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING CLE. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE FOUND THE NOSE STRUT PRESSURE LOW. THE NOSE STRUT WAS SERVICED TO PROPERNov 17, 1995 · N478AC · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CAL950823Limit Switch · looseFLT NR 0392 - PBI - ALL THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE GEAR WAS CYCLED WITH NO CHANGE, BUT THE RED GEAR LIGHTS EXTINGUISHED WITH THROTTLE MOVEMENT. MAINTENANCE TIGHTENED BOTH THE LEFT AND RIGHT AUTO THROTSep 17, 1995 · N478AC · Doug DC982 · Power LeverSDR CAL950602Switch · inoperativeFLT NR 0603 - CLE - ALL LANDING GEAR RED LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE UP. WHEN THE GEAR WAS EXTENDED FOR RETURN TO CLE, ALL INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LJul 18, 1995 · N478AC · Doug DC982 · Landing Gear Position and WarningSDR CAL950476O-Ring · leakingFLT NR 0436 - IAH - THE RT THRUST REVERSER ACCUMULATOR LIGHT ILLUMINATED WHILE AT CRUISE EN ROUTE FROM LAX TO SAT. THE LIGHT EXTINGUISHED AFTER PULLING CIRCUIT BREAKER AND TURNING OFF RIGHT SYSTEM, BUT REAPPEARED ABOUT TWO MINUTES LATER. SEVERAL MINUTES LATERJun 12, 1995 · N478AC · Doug DC982 · Hydraulic System, MainSDR CAL950445`Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN THE RADIUS OF THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT FS 1474. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05. (M)Apr 28, 1995 · N478AC · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL950293Battery Pack · inoperativeFLT 182 - IAH - INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS AFT OF ROW 26 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W)Apr 18, 1995 · N478AC · Doug DC982 · Emergency Lighting
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