N223PB

Service difficulty reports · 21

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 = 'N223PB' 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 HYIA20251113001Blade · crackedDURING DISASSEMBLY FOR SCHEDULED OVERHAUL A CRACK WAS IDENTIFIED AT A SINGLE BLADE ROOT. MULTIPLE BEARING RACES WERE FOUND TO BE CORRODED AND FAILED.Nov 12, 2025 · N223PB · Cessna 402C · Propeller Blade SectionSDR HYIA20251010001Switch · shortedPILOT REPORTED THE AUXILIARY CABIN FAN SWITCH FELT HOT WITH A BURNING SMELL AND NOTED SPARKS. COMPANY MAINTENANCE INSPECTED AND FOUND A BURNT WIRE TERMINAL. THE TERMINAL WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Oct 8, 2025 · N223PB · Cessna 402C · Air Conditioning System WiringSDR HYIA20230413001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPApr 12, 2023 · N223PB · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20221128001Spar Cap · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RH UPPER FWD SPAR CAP PN: 5122031-6. THIS CRACK IS LOCATED NEAR THE FORWARD RADIUS OF THE SPAR CAP AT APPROXIMATE RWS 70.94. THIS CRACK WAS CONFIRMED BY SURFACE EDDY CURRENT, MEASURES APPROXIMATELY 1 INNov 22, 2022 · N223PB · Cessna 402C · Wing SparSDR HYIA20221114002Crossbeam · crackedDURING MAINTENANCE ON N223PB, A MULTIPLE CRACKS WERE VISUALLY IDENTIFIED ON THE RH NACELLE CROSSOVER BEAM (P/N: 5654104-2). ONE CRACK ON THE FRONT FACE OF THE BEAM AT APPROXIMATE RWS 87.44 WITH AN APPROXIMATE LENGTH OF 3.780 INCHES. A SECOND CRACK WAS IDENTIFINov 10, 2022 · N223PB · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20220216001Fitting · crackedWHILE PERFORMING THE LIGHTED BOROSCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD RADIUS OR THE LEFT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .119 INCHES LONGFeb 8, 2022 · N223PB · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20211224001Blower · inoperativeTHE PILOT REPORTED A BURNING SMELL DURING CLIMB OUT. MAINTENANCE INSPECTED AND FOUND THE HEATER BLOWER INOPERATIVE. THIS WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Dec 19, 2021 · N223PB · Cessna 402CESSNA · Heating SystemSDR HYIA20180815001Angle · corrodedCORROSION WAS DISCOVERED ON ONE OF THE LEFT SIDE VERTICAL STABILIZER AFT ANGLES. REMOVED AND REPLACED THE ANGLE.Aug 13, 2018 · N223PB · Cessna 402C · Vertical StabilizerSDR HYIA20160718001Actuator · faultyPILOT REPORTED RT MLG DOWN AND LOCKED LIGHT INOPERATIVE AFTER EXTENSION, EMERGENCY T-HANDLE PULLED. MAINTENANCE INSPECTED AND REPLACED THE RT MLG ACTUATOR ASSEMBLY IAW 32-30-02, PERFORMED SEVERAL GEAR SWINGS AND OPERATIONALLY CHECKED GOOD. SERVICED THE EMERGJul 14, 2016 · N223PB · Cessna 402C · Landing Gear ActuatorSDR HYIA20150622001Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WERE FOUND AT LT WING LOWER FWD SPAR CAP STRAP, OEM PN 5292029-1, PREVIOUSLY INSTALLED VIA SERVICE KIT SK402-47 ON MARCH 10, 2004 TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB05-2 AS TERMJun 18, 2015 · N223PB · Cessna 402C · Wing SparSDR HYIA20150611001Brake · failedPILOT REPORTED LT BRAKE FAILURE. ACFT IS CURRENTLY IN HEAVY MX, CORRECTIVE ACTION NOT AVAILABLE AT THIS TIME.Jun 6, 2015 · N223PB · Cessna 402C · BrakeSDR HYIA20140421109Unknown · odorPILOT REPORTED A FUEL ODOR IN THE COCKPIT. PERFORMED A FUEL PRESSURE TEST & NO DEFECTS WERE NOTED, NO ACTION TAKEN.Apr 18, 2014 · N223PB · Cessna 402C · Air Distribution SystemSDR HYIA20120907001B-Nut · loosePILOT REPORTED THAT DURING PREFLIGHT INSPECTION, THERE WAS A STRONG ODOR OF FUEL IN THE COCKPIT. MX INSPECTED THE ENTIRE FUEL SYS IN ACFT AND IN THE HEATER. FOUND A LOOSE B-NUT IN LT WHEEL WELL WITH EVIDENT STAINS. B-NUT WAS TIGHTENED AND NO OTHER LEAKS WERSep 7, 2012 · N223PB · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20120904003B-Nut · looseTHE PILOT REPORTED THAT DURING FLIGHT, THERE WAS A FUEL ODOR PRESENT IN THE CABIN. ON LANDING AND INSPECTION, A B-NUT ON THE RT CROSSFEED LINE IN THE FUEL BOWL BAY WAS TIGHTENED. THIS RESOLVED THE ISSUE WITHOUT FURTHER DISCREPANCY.Aug 31, 2012 · N223PB · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA08242012001Wire Harness · misroutedDURING CLIMB, PILOT EXPERIENCED A MOMENTARY BURNING ODOR IN COCKPIT DURING GEAR RETRACTION. AFTER INSPECTION, THE DISCREPANCY WAS RESOLVED BY REPAIRING AND REROUTING WIRE BUNDLE IN NOSE GEAR WHEEL WELL.Aug 23, 2012 · N223PB · Cessna 402C · Landing Gear System WiringSDR HYIA20140415041Drag 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 5, 2011 · N223PB · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA223PBANNUCDiode · faultedIN CRUISE FLIGHT, CREW REPORTED, WITH LANDING GEAR UP AND LOCKED, AND ALL GEAR INDICATIONS NORMAL, NUMEROUS CAUTION/WARNING LIGHT FLICKERED AND THEN REMAINED ILLUMINATED. GEAR WARNING HORN ALSO SOUNDED FOR A SECOND. ANNUCIATOR LIGHTS THAT ILLUMINATED WERE, LFeb 24, 2010 · N223PB · Cessna 402C · Landing Gear Position and WarningSDR HYIA223PB1112NLGStrut · dischargedCREW REPORTED, AFTER TAKEOFF, HYD PRESSURE LIGHT AND GEAR UNLOCK LIGHT REMAINED ILLUMINATED. SECOND ATTEMPT RESULTED IN SAME INDICATIONS. CREW SELECTED GEAR DOWN WITH NORMAL INDICATIONS (3 GREEN DOWN AND LOCKED LIGHTS). AFTER LOW APPROACH, TOWER REPORTED GEAR Nov 12, 2009 · N223PB · Cessna 402C · Nose/Tail Landing Gear Strut/AxleSDR HYIA223PBGEAR1013Uplock Switch · dirtyCREW REPORTED AFTER TAKE OFF AND GEAR RETRACTION,(DOWN LOCK LIGHTS EXTINGUISHED) THE HYD PRESSURE LIGHT AND GEAR UNLOCK LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, SAME INDICATION. CREW ELECTED TO EXTEND GEAR, NORMAL EXTENSION (3 GREEN ILLUMINATED AND HYD PRESOct 13, 2009 · N223PB · Cessna 402C · Landing Gear Position and WarningSDR 135N223PBWire · unsecureON 08-05-07, LEFT ALTERNATOR OUT LIGHT CAME ON IN FLIGHT AND RT ALT OUT CAME ON INTERMITTENTLY. MX INSPECTED AND REPAIRED WIRING TO LT ALT AND SECURED WIRE TO RT ALT FUSE IN COCKPIT, SECONDARY INSP AND RUN UP WAS PERFORMED ON 08-06-07 WITH NO DEFECTS NOTED.Aug 5, 2007 · N223PB · Cessna 402C · Electrical Power System WiringSDR 135N223PB0502Circuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER.Jun 26, 2006 · N223PB · Cessna 402C · DC Power Distribution System
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