N120PC

Service difficulty reports · 22

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 = 'N120PC' 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 HYIA20220701002Fitting · crackedWHILE PERFORMING THE LIGHTED BORESCOPE PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02 R2 TO SATISFY AD2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE LEFT HAND OUTBOARD FITTING. THIS CRACK MEASURES .129 IN LENGTH, AND IT'S LOCATION IS CONSISTENT WIJul 1, 2022 · N120PC · Cessna 402C · Fuselage Main, StructureSDR HYIA20200508003Fitting · corrodedWHILE PERFORMING LIGHTED BOROSCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-09, A SPOT OF CORROSION WAS IDENTIFIED ON THE RIGHT HAND OUTBOARD NACELLE FITTING (P/N: 5292029-24). THIS CORROSION IS LOCATED ON THE BOTTOM OF THE May 7, 2020 · N120PC · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20200521002Cylinder · low pressurePILOT REPORTED ROUGH RUNNING ENGINE. MAINTENANCE INSPECTED AND FOUND RIGHT #5 CYLINDER NO COMPRESSION. REMOVED AND REPLACED ENGINE WITH NO FURTHER DEFECT NOTED, AS WAS SCHEDULED FOR REMOVAL WITHIN 87 HOURS.May 6, 2020 · N120PC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20190731001Fitting · corrodedDURING MAINTENANCE, TWO AREAS OF CORROSION WERE DISCOVERED ON THE HORIZONTAL FLANGE OF THE UPPER LEFT HAND AFT WING FITTING (P/N 0822550-45.) THESE AREAS OF CORROSION MEASURED .750 BY .250 WITH A DEPTH OF .042, AND .400 BY .250 WITH A DEPTH OF .031. THIS FITTIJul 31, 2019 · N120PC · Cessna 402C · Wing, Attach FittingsSDR HYIA20190724001Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT HAND LOWER AFT SPAR CAP P/N: 5122041-23. THIS CORROSION IS LOCATED IN THE FORWARD RADIUS OF THE HORIZONTAL AND VERTICAL LEGS OF THE CAP AT APPROXIMATE LWS 228.71. THIS CORROSION HAS A DEPTH OF APPROXIMATEJul 24, 2019 · N120PC · Cessna 402C · Wing SparSDR HYIA20190718001Spar Cap · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS IDENTIFIED ON THE HORIZONTAL LEG OF THE LEFT HAND UPPER OUTBOARD SPAR CAP (P/N: 5122041-21). THIS CORROSION IS LOCATED AT APPROXIMATE LEFT WING STATION 197.71 AND MEASURES APPROXIMATELY .022 INCHES DEEP. THIS IS IN EJul 16, 2019 · N120PC · Cessna 402C · Wing SparSDR HYIA20161010171Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 10, 2016 · N120PC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160815073Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 14, 2016 · N120PC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160520002Selector · out of rigLEFT ENG FUEL FLOW WENT TO 0 IN FLIGHT. FOUND FUEL SELECTOR OUT OF RIG & RIGGED & RELEASED ACFT FOR FLIGHT CHECK. INSPECTED FUEL BOWL AS PRECAUTION.May 14, 2016 · N120PC · Cessna 402C · Fuel Selector/Shut-Off ValveSDR HYIA20141231001Fan · malfunctionedTHE LT ANNUNCIATOR INTERMITTENT & AN ELEC SMELL IN CABIN. INSPECTED, R & R LT ALTERNATOR OUT SENSOR IAW MM CH 34-30-0. OPERATIONS CHECKED GOOD. THE SMELL WAS DETERMINED TO BE THE CABIN VENT FAN WHICH WAS PLACED ON MEL. NO FURTHER DEFECTS NOTED.Dec 28, 2014 · N120PC · Cessna 402C · Air Distribution FanSDR HYIA20140606001Sight Tube · splitPILOT REPORTED AFTER DEPARTURE FROM MAZ & DURING TRANSITION FROM CLIMB TO CRUISE SMOKE & FUMES WERE DETECTED COMING FROM DEFROST VENT. PILOT CLOSED DEFROST, RAM AIR & CABIN AIR VENT VLVS. UPON CLOSING CABIN VENTILATION VLVS, PILOT REPORTS SMOKE & FUMES NO LOMay 14, 2014 · N120PC · Cessna 402C · Hydraulic Quantity IndicatorSDR HYIA20120910003Spar · corrodedDURING A REGULARLY SCHEDULED MX, DAMAGE WAS DISCOVERED TO THE RT SPAR STRAP. DAMAGE WAS A MISDRILL AND INTERGRANULAR CORROSION. BASED ON THE DAMAGE NOTED, REMOVED DAMAGED PART AND INSTALLED NEW PART.Sep 10, 2012 · N120PC · Cessna 402C · Wing Main, Frame StructureSDR HYIA20120910002Spar · crackedDURING REGULARLY SCHEDULED MX INSPECTION, DAMAGE WAS NOTED TO THE AFT CARRY THROUGH SPAR ASSY UPPER FORWARD AND AFT WEB FLANGES. FLANGES WERE FOUND TO BE CRACKED AT FLOOR SUPPORT MOUNT LOCATIONS. OPENSep 10, 2012 · N120PC · Cessna 402C · Fuselage Main, StructureSDR HYIA201205170001Spar · damagedDURING A SCHEDULED MX EVENT, IT WAS NOTED THAT THE RT SPAR STRAP HAD PREVIOUSLY SUSTAINED DAMAGE. UPON NOTING THIS DISCREPANCY, A WO WAS SUBMITTED TO MRO FOR REMOVAL AND REPLACEMENT OF THE RT SPAR STRAP. THE ACFT IS GROUNDED AWAITING THE REQUIRED REPAIRS.May 16, 2012 · N120PC · Cessna 402C · Wing SparSDR HYIA201203198521Indication Sys · inaccurateDURING CRUISE, LEFT ENGINE STARTED TO LOOSE POWER. PILOT NOTICED LT FUEL FLOW LOWER THAN 70 LBS MIN AND DECREASING. PILOT SWITCHED THE LT AUX FUEL PUMP TO HIGH AND ENGINE RAN NORMAL. AFTER 30 SECONDS, THE FUEL FLOW STARTED TO DECREASE AGAIN. THE ENGINE BECMar 19, 2012 · N120PC · Cessna 402C · Fuel Indicating SystemSDR HYIA20140415066Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, 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 OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJul 13, 2011 · N120PC · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIAN120PCLITESDimmer · failedCREW REPORTED BURNING ELECTRICAL ODOR FLOWED THROUGH COCKPIT. ALL NON-ESSENTIAL EQUIPMENT WAS TURNED OFF. SHORTLY AFTER, A SMALL STREAM OFF SMOKE AROSE FROM AREA JUST FWD OF THROTTLE LEVERS. IFR CLEARANCE CANCELLED, DIVERTED, AFTER COMPLYING WITH SMOKE IN THEFeb 22, 2010 · N120PC · Cessna 402C · Flight Compartment LightingSDR HYIA120PC AVMSTRCircuit Breaker · unserviceableCREW REPORTED AVIONICS MASTER SWITCH TRIPPED ONCE DURING FLIGHT. MX REMOVED AND REPLACED CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.Dec 26, 2009 · N120PC · Cessna 402C · DC Power Distribution SystemSDR 1350516N120PCMaster Switch · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Jul 24, 2006 · N120PC · Cessna 402C · Alternator-Generator DriveSDR HYI2003F00016Distributor Gear · failedON CLIMB OUT, PILOT REPORTED RIGHT ENGINE RUNNING ROUGH, RETURNED W/O INCIDENT. MECHANIC FOUND RT ENGINE/ LEFT MAGNETO DIST GEAR FAILED. REMOVED AND REPLACED MAGNETO AND RETURNED A/C TO SERVICE.Aug 27, 2003 · N120PC · Cessna 402C · Magneto/DistributorSDR HYI2001F00011Drag Brace · crackedDURING SCHEDULED INSPECTION, MECHANIC FOUND NOSE GEAR DRAG BRACE CRACKED AT ACTUATOR ATTACH LUG. REMOVED AND REPLACED DRAG BRACE AND RETURNED AIRCRAFT TO SERVICE.Nov 20, 2001 · N120PC · Cessna 402C · Landing Gear Retraction/Extension SystemSDR 96ZZZX1248Switch · burnedDURING CRUISE FLIGHT, CABIN STARTED FILLING WITH SMOKE. SMOKE WAS ORIGINATING FROM AVIONICS MASTER SWITCH - UNABLE TO TURN SWITCH OFF, SO CIRCUIT BREAKERS WERE PULLED. SMOKE EVACUATION PROCEDURES WERE INITIATED AND SMOKE SUBSIDED. A NORMAL LANDING WAS MADE.May 8, 1995 · N120PC · Cessna 402C · DC Power Distribution System
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