N477AC, cancelled Mar 21, 2013

Service difficulty reports · 34

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 = 'N477AC' AND deregistration_id = 'N477AC-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 CALA0100439Battery · dischargedFORWARD ENTRANCE DOOR PORTABLE EMERGENCY LIGHT INOP AND WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-53-00.May 4, 2001 · N477AC · Doug DC982 · Emergency LightingSDR CALA9900741Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. REPAIR DOUBLERS WERE INSTALLED IAW DRAWING SR09530003.Jun 28, 1999 · N477AC · Doug DC982 · Fuselage Main, FrameSDR CALA9900740Frame · wornINSPECTION FOUND FORWARD UPPER CORNER OF RT MLG WHEEL WELL FORWARD DOOR JAMB FRAME WORN. THE FRAME WAS REPLACED AND A SPLICE REPAIR WAS INSTALLED IAW DOUGLAS DRAWING 5930584.Jun 28, 1999 · N477AC · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900739Clip · out of adjustTHE CLIP TENSION AT TAIL CONE RELEASE EXTERIOR HANDLE WAS TOO LOW. A NEW HANDLE RETAINING CLIP WAS INSTALLED AND ADJUSTED IAW MM 53-53-00, PAGE 519.Jun 28, 1999 · N477AC · Doug DC982 · Aerodynamic FairingsSDR CALA9900730Cables · out of adjustTHE TAIL CONE RELEASE PULL WAS EXCESSIVE USING THE INTERIOR AND EXTERIOR HANDLES AND AFT ENTRY DOOR. THE TAIL CONE CABLES WERE ADJUSTED/TESTED IAW MM 53-53-00, PARAGRAPH 3(A)&(B). DROP TEST PULLED WITHIN ALLOWABLE LIMITS.Jun 27, 1999 · N477AC · Doug DC982 · Aerodynamic FairingsSDR CALA9900722Bulkhead Angle · wornINSPECTION FOUND ANGLE STIFFENER WORN THREE QUARTERS OF WAY THROUGH FROM STAINLESS LINE ON LT SIDE OF APB AFT FACE. REPAIRED IAW ECRA 5330-02837.Jun 25, 1999 · N477AC · Doug DC982 · Fuselage Main, BulkheadSDR CALA9900714Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN AT AFT END OF MAIN CABIN DOOR NR 7 BEAM. REPAIRED IAW SRM 52-05, FIGURE 31, SHEET 12.Jun 22, 1999 · N477AC · Doug DC982 · Passenger/Crew DoorsSDR CALA9900713Skin · dentedINSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 313-350, LONGERON 19L. REPAIRED IAW ECRA 5331-01056.Jun 21, 1999 · N477AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900711Skin · dentedINSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 294 ON LT SIDE JUST FORWARD OF CABIN OUTFLOW VALVE, LONGERON 25L. A REPAIR WAS INSTALLED IAW ECRA 5330-02377.Jun 20, 1999 · N477AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900707Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACK CORRODED UNDER GALLEY AREAS NR 3 AND NR 4 AT STA 1030-1305. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Jun 18, 1999 · N477AC · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900702Drive Shaft · lack of lubeINSPECTION FOUND RT WING OVERWING EMERGENCY ESCAPE LINE HARD TO PULL FROM REEL. THE DRIVE SHAFT ASSEMBLY WAS CLEANED AND LUBRICATED IAW MM 25-60-00.Jun 17, 1999 · N477AC · Doug DC982 · Emergency EquipmentSDR CALA9900701Stop · corrodedINSPECTION FOUND FORWARD DOOR STOP FLANGE AT MAIN BAGGAGE BIN DOOR JAMB CORRODED. A REPAIR DOUBLER WAS INSTALLED ON FORWARD STOP PAD LOWER AREA AT MAIN BAG BIN Z-ANGLE IAW SRM 53-05, FIGURE 63.Jun 17, 1999 · N477AC · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900700Seat Track · corrodedINSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 200-250. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-01, FIGURE 4, SHEET 1.Jun 17, 1999 · N477AC · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900673Longeron · crackedINSPECTION FOUND A 4 INCH CRACK IN LONGERON 29L SPLICE AT STA 1204. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-5.Jun 15, 1999 · N477AC · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA9900671Seat Track · corrodedINSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 230. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1.Jun 14, 1999 · N477AC · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900667Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 120.5 ABOVE LONGERON 19L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B.Jun 13, 1999 · N477AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900665Seat Track · corrodedINSPECTION FOUND LEFT I/B SEAT TRACK CORRODED UNDER GALLEY AREAS NUMBER 3 AND 4 AT STA 1030-1305. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.Jun 11, 1999 · N477AC · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9802193Compressor · damagedTHE NR 1 AND NR 2 ENGINES INGESTED ICE ON TAKEOFF FROM CLE AND ON ROTATION THE NR 1 ENGINE EPR FELL TO 1.1. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH ENGINES HAD FAN BLADE DAMADec 22, 1998 · N477AC · Doug DC982 · Turbine Engine Compressor SectionSDR CALA9700987Panel · corrodedINSPECTION FOUND AFT LAV SERVICE PANEL CORRODED AROUND LOWER DUMP CABLE THROUGH HOLE. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5330-02540.Jun 25, 1997 · N477AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9700985Longeron · corrodedINSPECTION FOUND LONGERON 30 CORRODED AT STA 256 TO 275. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Jun 25, 1997 · N477AC · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA9700984Beltframe · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT BELTFRAME CORRODED AT STA 1309, LONGERON 23L TO 27R. INSTALLED REPAIR PARTS IAW SRM 51-10-3.Jun 24, 1997 · N477AC · Doug DC982 · Fuselage Main, FrameSDR CALA9700983Jamb · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT LOWER DOOR JAMB PAN CORRODED AROUND THE DOOR STOP SUPPORT BRACKET. REPAIRED IAW SRM 53-05, FIGURE 44, SHEET 2.Jun 24, 1997 · N477AC · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9700986Beam · crackedINSPECTION FOUND A 1.5 INCH CRACK AT FORWARD END AND A 1 INCH CRACK AT AFT END OF MAIN CABIN DOOR BEAM NR 1. DOUBLERS WERE INSTALLED IAW SRM 52-05, FIGURE 31.Jun 20, 1997 · N477AC · Doug DC982 · Passenger/Crew DoorsSDR CALA9700982Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.Jun 20, 1997 · N477AC · Doug DC982 · Passenger/Crew DoorsSDR CALA9700348Lamp · failedWHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH, THE NOSE GEAR LIGHT DID NOT ILLUMINATE. THE MECHANICAL INDICATION SHOWED GEAR WAS DOWN. AN EMERGENCY GEAR EXTENSION WAS USED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH GREEN LIGHT LAMPS FMar 17, 1997 · N477AC · Doug DC982 · Landing Gear Position and WarningSDR CALA9700074Cylinder · inoperativeTHE LT MLG RED LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER TAKEOFF FROM IAH. THE GEAR WAS CYCLED THREE TIMES WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG BUNGEE Jan 25, 1997 · N477AC · Doug DC982 · Landing Gear Retraction/Extension SystemSDR CALA9700096Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN TAIL SECTION SKIN AT CANTED BULKHEAD, STA 1485. THE SKIN WAS REPAIRED IAW SRM 53-08 FIGURE 2 SHEET 3.Jan 23, 1997 · N477AC · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9601209Acm · inoperativeAN ELECTRICAL ODOR WAS OBSERVED IN FLIGHT, AIRCRAFT HAS HISTORY. THE ODOR WAS STRONGEST IN AFT LAV NEAR CEILING. THERE WAS NO SMOKE OR HEAT PRESENT AND NO ABNORMAL ELECTRICAL LOADS WERE OBSERVED. THE FLIGHT WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE FOUNDAug 23, 1996 · N477AC · Doug DC982 · Cabin Cooling SystemSDR CALA9601208Transformer · overheatedA MILD ELECTRICAL ODOR WAS OBSERVED AT LEFT AFT LAV IN FLIGHT. NO OTHER ADVERSE CONDITIONS WERE NOTED, ONLY THE ODOR. THE FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEMS REPORTED. MAINTENANCE FOUND T1-2 TRANSFORMER FOR LIGHTS AT AFT LEFT LAVAug 22, 1996 · N477AC · Doug DC982 · Passenger Compartment LightingSDR CAL960409Frame · puncturedLGA - FLT 1807 - TUG PUNCTURED LT SIDE OF FUSELAGE DURING PUSHBACK AT LGA WITH RESULTANT DAMAGE TO LONGERONS 23L TO 26L, FRAME, AND SKIN AT STA 229 TO STA 303. THE LT FLYING GEAR DOOR WAS ALSO DAMAGED AT LOWER TRAILING EDGE. THE LONGERONS AND SKIN WERE REPAIMar 21, 1996 · N477AC · Doug DC982 · Fuselage Main, FrameSDR CAL951180Batteries · dischargedEWR - INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. THE BATTERIES FOR THE EMERENCY LIGHTS IN FIRST CLASS CABIN WERE REMOVED AND REPLACED AND OPERATION WAS RESTORED. (M)Dec 28, 1995 · N477AC · Doug DC982 · Emergency LightingSDR CAL950865Eel Wiring · brokenMIA - FLT 0378 - INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING AT ROWS 2-6 OFF THE TRACK AND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES AT TWO SECTIONS. THE WIRING WAS REPAIRED AND OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED. (X)Sep 27, 1995 · N477AC · Doug DC982 · Emergency LightingSDR CAL950536Support · corroded31J - INSPECTION FOUND THE FLOOR SUPPORT STRUCTURE CORRODED AT STA 180. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01. (X)May 29, 1995 · N477AC · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL950089Eel Wiring · failedFLT NR 0151 - SFO - SEVERAL EMERGENCY AISLE PATH LIGHTS WERE FOUND INOPERATIVE IN THE FIRST CLASS CABIN. MAINTENANCE FOUND BROKEN WIRING UNDER FORWARD CABIN FLOOR TRACK. THE WIRING WAS REPAIRED AND OPERATION OF AISLE PATH LIGHTING WAS RESTORED. (Z)Feb 5, 1995 · N477AC · Doug DC982 · Emergency Lighting
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