N416MC
Service difficulty reports · 173
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 = 'N416MC' AND registry_match = 'registration' 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.
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 = 'N416MC' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR P5CA2010062101642Structure · damagedNR 4 ENGINE & NBSP; RIGHT CORE COWL DAMAGED DURING MAINTENANCE BY STAND. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4471A058, WITH FAA 8110-3 DATED 15 JUN 2010. DVI EVERY 2 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 25 FLIGHT CYCLES.SDR P5CA2010052401638Conduit · damagedRIGHT WING GEAR FLEXIBLE ELECTRICAL CONDUIT DAMAGED. PART ONE TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4425A157, WITH FAA 8110-3 DATED 24 MAY 2010. REPEAT DVI EVERY FLIGHT CYCLE AND PERMANENT REPAIR PRIOR TO 25 FLIGHT CYCLES AFTER PART 1 ACCOMPSDR P5CA2009110501609Depressor · damagedFOUND LWR AFT CARGO DOOR REAR SIDE UPPER DEPRESSOR SEAL DAMAGED 1/2 X 1/2. REMOVED/SMOOTH DAMAGED AREA AND APPLIED 2 LAYERS OF SPEED TAPE APPLIED IAW PART 1 OF EO 4453A303 IN ADDITION TO FAA 8110-3 ISSUED 5 NOV 2009. VISUAL INSP IS REQUIRED AT EVERY FLIGHT LSDR P5CA2009062501601Acm · defectiveIN CRUISE A LOUD RUMBLING WAS HEARD THROUGH THE PACK SYSTEM AND AN ODOR WAS NOTICED COMING THROUGH THE VENTS. CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-56 AND IT WAS CONFIRMED THERE IS A BAD PACK 1 ACM. PACK 1 WAS DEACTIVATED AND DEFERRED IAW MEL 21-SDR P5CA200904290195Grommet · loosePRE TAXI RUDDER CHECK UNSATISFACTORY. FOUND CABLE GROMMET LOOSE AND STICKING ON PULLEY. GROMMET RESECURED AND OP'S CHECKED OK IAW AMM 27-55-00 AND AMM 20-11-07-074-016.SDR P5CA0801571Structure · damagedDURING GROUND HANDLING THE TAIL JACK STRUCK THE TAIL SECTION OF THE AIRCRAFT NEAR THE TAIL POST FITTING IN SECTION 48 AT BS 2602. ACCOMPLISHED INTERIM REPAIR ACCORDING TO EO 4453A189, SRM 53-00-01 FIG 201, REPAIR 11. INITIAL AND REPEAT INSPECTIONS TO BE SCHESDR P5CA0801550Gimbal Joint · brokenDURING ROUTINE INSPECTION OF NR 3 THRUST REVERSER FOUND LT LOWER ACTUATOR MOUNTING BRACKET GIMBAL BROKEN. REMOVED THE NR 3 ENGING LOWER LT ANGLE GEARBOX HOUSING AND BALLSCREW ACTUATOR AS PER AMM 78-31-22, PERFORM DVI INSPECTIONS PER EO NR 4478A065 PRIOR TO EASDR P5CA0801547Inlet · damagedDURING THE OIL SERVICING OF THE NR 3 ENGINE DAMAGE OCCURRED TO THE RIGHT SIDE OF THE INLET COWLING AT THE 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER EO NR 4471A012 PART 1 PER SRM 54-15-01.SDR P5CA0701540Access Door · inflt separationNR 4 ENGINE STRUT I/B ACCESS DOOR PARTIALLY LOST IN FLIGHT AND NR 4 ENGINE STRUT O/B ACCESS DOOR PEELED BACK IN FLIGHT. MAJOR REPAIR AND PARTS REPLACEMENT ACCOMPLISHED PER XEO-51-120607, P/N: 323U2304-84, 323U2303-72.SDR P5CA0701539Roller Tray · damagedROLLER TRAY AND SEAT TRACK DAMAGE M/D STA 1650-1800. REPAIR ROLLER TRAYS AND SEAT TRACK PER XEO NR 53-111407 SRM 51-70-12 SOYM 20-44-04SDR PCCA0701536Drive System · failedSTATUS MESSAGE LE MULTI DRIVE AND EICAS FLAPS PRIMARY. GOT MSG AFTER EXTENDING FLAPS T/O. RETURNED TO GATE. REMOVED AND REPLACED 3-R L/E DRIVESDR P5CA0701535Isolation Valve · malfunctionedAPU EICAS MESSAGE AFTER T/O. ALSO HEARD LOUD SOUND FROM ABOVE MAIN DECK SIDE CARGO DOOR. AIR TURNBACK. REPLACED APU ISOLATION VALVE, INSEPCTED DUCTS NO DEFECTS NOTED. ACCOMPLISHED PRESSURIZATION CHECK OF CARGO DOOR AND INSPECTED SEALS. NO DEFECTS NOTED, PSDR P5CA0701533Structure · looseDURING DAILY CHECK, FOUND NR 1 THRUST REVERSER INNER WIRE MESH BONDING LOOSE AND MISSING BETWEEN 6 AND 10 O'CLOCK POSITIONS. INTERIM REPAIR ACCOMPLISHED AS PER XEO 78-091604/FAA 8110-3.SDR P5CA0701531Support Bracket · crackedDURING WALK AROUND INSPECTION IN THE LEFT WING FUELING SERVICE PANEL BRACKET SUPPORT CRACK. PERFORMED PART 1 PER XEO 57-082107 AND INTERIM REPAIR APPROVED.SDR P5CA0701527Unknown · unknownON CLIMB-OUT, BLEED HP ENG 4, ENG 4 LOW IDLE, NAI ENG 4 MESSAGES. DEFERRED BLEED HP ENG 4 PER MEL 36-11-3 AND 78-31-1A. DEFERRED NAI 4 MESSAGE PER MEL 30-21-1BSDR UIEA200700018Panel · missingON WALK AROUND, FOUND PANEL MISSING ON NR 1 PYLON RIGHT HAND SIDE, PANEL 452 CR. INSTALLED NEW PANEL IAW MM 54-62-00.SDR UIEA200700007Floorbeam · damagedAFT CARGO COMPARTMENT AFT FLANGE OF FLOORBEAM UPPER CHORD DAMAGED AT STA 1780 RBL 25.75. AFT CARGO COMPARTMENT AFT FLANGE OF FLOORBEAM REPAIRED AS PER SRM 51-70-12 REPAIR 1 AND EO 4453A100.SDR UIEA200700006Seat Track · damagedAFT CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STA 1780 RBL 25. AFT CARGO SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR NR 10 AND EO NR 4453A100.SDR UIEA200600275Manifold · chafedNR 4 ENGINE FUEL NOZZLE MANIFOLD LEAKING AT 12 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENGINE RT FUEL MANIFOLD IAW AMM 73-11-10. LEAK CHECK OK.SDR UIEA200600268Tire · separatedON TAKEOFF FROM HNL NR 8 TIRE TREAD COMPLETELY SEPARATED FROM MAIN CARCASS CAUSING DAMAGE TO 3 WING TO BODY FAIRINGS AFT OF LT BODY GEAR. HONEYCOMB PANELS 193BL,193CL,193DL INCLUDING WTB FRAMES AT STA1540,1580 & 1620. IMPACT DAMAGE TO ELEC CONDUIT ON RT BLG SDR UIEA200600018Skin · delaminatedDURING A-4 CHECK, LEFT HAND INBOARD T/E MID FLAP HAS IMPACT DAMAGE WITH DELAM ON LOWER AFT INBOARD SURFACE AS MARKED. REPAIR CARRIED OUT IAW SRM 51-70-06 AND SRM 57-53-01.SDR UIEA200500051Door · malfunctionedRT BODY GEAR DOOR OPENED AFTER RETRACTION WHEN GEAR LEVER PLACED IN OFF POSITION. STATUS MSG GEAR DOOR GEAR MONITOR. GEAR PINS INSTALLED. PRESSURIZED HYD SYSTEM. OPS CHECKED DOOR IAW MM. ALL INDICATIONS OK IN ALL HANDLE POSITIONS. RT BODY GEAR DOOR DID NSDR EVA07022004Engine · flamed outDURING AIRCRAFT DESCENT AT 30000 FT, ENGINE NR 3, NR 4 FLAMED OUT WHILE ENCOUNTERING HEAVY RAIN AND MODERATE TURBULENCE. BOTH ENGINES WERE BACK TO NORMAL AFTER RESTART. THIS CASE IS BEEN DETERMINED AS WEATHER CAUSED IFSD (IN-FLIGHT SHUT DONE) AT OCT/2004.
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