N771EA

Service difficulty reports · 18

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 = 'N771EA' 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.

SDR HYIA20210208001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .157 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTFeb 8, 2021 · N771EA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20181003007Beam · crackedDURING MAINTENANCE A CRACK WAS FOUND ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11) THIS CRACK BEGINS AT THE UPPER INBOARD FASTENER HOLE COMMON TO THE TURBOCHARGER MOUNTING BRACKET, AND MEASURES APPROXIMATELY .371 INCHES LONG. THIS BEAM WOct 3, 2018 · N771EA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20181003005Angle · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT SIDE AFT VERTICAL ANGLE (P/N: 5131007-5) OF THE VERTICAL STABILIZER BETWEEN APPROXIMATE W.L. 142.514 AND 145.380. THIS CORROSION IS 2.866 INCHES LONG, AND HAS EXFOLIATED THE FLANGE OF THE ANGLE FROM ITS OOct 3, 2018 · N771EA · Cessna 402C · Vertical Stabilizer Miscellaneous StructureSDR HYIA20181003004Door Frame · corrodedWHILE CONDUCTING OTHER MAINTENANCE, AN AREA OF CORROSION WAS NOTED ON THE FUSELAGE FRAME ASSEMBLY AT F.S. 214.00, JUST ABOVE THE 501110-12 STRIKER PLATE FOR THE LOWER PASSENGER DOOR PIN. THE 501110-12 STRIKER PLATE WAS REMOVED FOR FURTHER INSPECTION. UPON REMOOct 3, 2018 · N771EA · Cessna 402C · Fuselage Main, StructureSDR HYIA20181003003Fitting · corrodedDURING MAINTENANCE CORROSION WAS FOUND ON THE RIGHT HAND UPPER AFT WING FITTING (P/N: 0822550-46) THIS CORROSION MEASURED 1.612 INCHES LONG, .434 INCHES WIDE, AND .025 INCHES DEEP. THIS FITTING WILL BE REPLACED WITH A FACTORY NEW PART.Oct 3, 2018 · N771EA · Cessna 402C · Wing Miscellaneous StructureSDR HYIA20181003002Rib · crackedDURING MAINTENANCE A CRACK WAS FOUND ON THE RIGHT HAND CLOSE OUT RIB LOCATED AT RIGHT WING STATION 106.79 (P/N: 5122115-56). THIS CRACK STARTS FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT TRUNNION PLATE AND TRAVELS FORWARD APPROXIMATELY .595 IOct 3, 2018 · N771EA · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20181003001Spar Cap · corrodedDURING MAINTENANCE CORROSION DAMAGE WAS FOUND ON THE RIGHT WING AFT LOWER CAP (P/N: 5122041-24). THIS CORROSION IS LOCATED AT APPROXIMATE RIGHT WING STATION 204.71 AND MEASURES APPROXIMATELY .019 DEEP. THIS IS GREATER THAN REMOVABLE LIMITS ALLOWED UNDER MEB95-Oct 3, 2018 · N771EA · Cessna 402C · Wing SparSDR HYIA08242017001Spar Cap · corrodedWHILE REPAIRING A FUEL LEAK, CORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD RADIUS OF THE RT AFT OUTBOARD SPAR CAP. THE FIRST AREA OF CORROSION WAS DISCOVERED AT WS 208.1 AND WAS 1 INCH IN LENGTH. THE SECOND AREA WAS LOCATED AT WAug 15, 2017 · N771EA · Cessna 402C · Wing SparSDR HYIA20170705002Fitting · crackedWHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, A CRACK WAS IDENTIFIED IN THE RT INBOARD NACELLE FITTING.Jul 5, 2017 · N771EA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20160815001Shaft · wornPILOT REPORTED ELEVATOR VIOLENT SHUDDER AND PITCH DOWN WITH THE AMOUNT OF NOSE DOWN REQUIRED FOR 500 FPM DESCENT AT CRUISE POWER. MAINTENANCE PERFORMED INSPECTION OF ELEVATOR SYSTEM AND FOUND THE ELEVATOR TRIM TAB BINDING AND APPEARED TO HAVE SIGNIFICANT AMOUAug 12, 2016 · N771EA · Cessna 402C · Elevator Tab Control SystemSDR HYIA20160520001Clamp · looseDURING TAXI & TAKEOFF CLIMB, LT RUDDER POPS, LOUD SOUND, & SEEMS TO BIND. DURING INSPECTION RUDDER SYS FOUND LT RUDDER TUBE GUIDE INTERCONNECT SPRING ATTACHING PART CLAMP & TUBE GUIDE LOOSE. RE-POSITIONED LT RUDDER TUBE GUIDE, ADJUSTED & SECURED TUBE GUIDE CMay 13, 2016 · N771EA · Cessna 402C · Rudder Control SystemSDR HYIA03272015006Beam · crackedTHE RT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE Mar 27, 2015 · N771EA · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA03272015005Beam · crackedTHE LT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE Mar 27, 2015 · N771EA · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20136011103Fuel Line · chafedDURING PREFLIGHT, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT. MX DETERMINED THERE WAS A FUEL LEAK OTBD OF THE NACELLE AND FOUND A CHAFED FUEL LINE AFT OF FORWARD FLOAT VALVE. BOTH DISCREPANCIES WERE REPAIRED AND LEAK CHECK ACCOMPLISHED.May 27, 2013 · N771EA · Cessna 402C · Engine Fuel DistributionSDR HYIA20140415053Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDUREApr 18, 2011 · N771EA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA771EA 619Master Switch · unserviceableCREW REPORTED AVIONIC MASTER SWITCH INOPERATIVE. MX REMOVED AND REPLACED SWITCH, AND RETURNED ACFT TO SERVICEJun 19, 2009 · N771EA · Cessna 402C · Electrical Power SystemSDR HYI2003F00018Governor · unserviceableCREW REPORTED, DURING CRUISE LEVEL FLIGHT, 658 ENGINE BEGAN TO SURGE +/- 400 RPM. AFTER REDUCING POWER, AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC FOUND 6 FT PROP GOVERNOR FAILED. MECHANIC CHANGED GOVERNOR AND RELEASED AIRCRAFT BACK TO SERVICE.(K)Oct 31, 2003 · N771EA · Cessna 402C · Propeller GovernorSDR 20000808SH014Pin · destroyedON LANDING, AFT BRAKE LOCKED UP, AND MAIN WHEEL SEIZED. MAINTENANCE FOUND ONE CALIPER ANCHOR PIN SHEARED. REMOVED AND REPLACED MAIN WHEEL ASSY, BRAKE CALIPER, AND BRAKE BACKPLATE ASSY, THEN RETURNED AIRCRAFT TO SERVICE. AT THIS TIME, ALL ANCHOR PINS ARE BEIJul 12, 2000 · N771EA · Cessna 402C · Brake
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