N26156

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 = 'N26156' 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 HYIA20251107002Crossbeam · chafedDURING MAINTENANCE CHAFING DAMAGE WAS VISUALLY IDENTIFIED ON THE FORWARD FACE OF THE LH CROSSOVER BEAM (OEM: 5654104-11). THIS CHAFE MEASURES APPROXIMATELY .700 LONG, .500 WIDE, WITH A DEPTH OF APPROXIMATELY .011. THIS BEAM HAS BEEN REPLACED.Nov 5, 2025 · N26156 · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20251107001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND INBOARD NACELLE FITTING. (P/N: 5292029-21) THIS CRACK MEASURES APPROXIMATELY .100 INCHES LONG ON THE INBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS FNov 5, 2025 · N26156 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20250131001Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE FORWARD FACE OF THE FWD LH UPPER FUSELAGE ATTACH FITTING PN: 0811350-9. THIS CORROSION MEASURES APPROXIMATELY .700 WIDE, AND .400 TALL, WITH AN APPROXIMATE DEPTH OF .025 AND IS CONSISTENT WIJan 30, 2025 · N26156 · Cessna 402C · Fuselage Main, Attach FittingsSDR HYIA20240718005Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE RIGHT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.Jul 16, 2024 · N26156 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20220909002Door Frame · corrodedDURING MAINTENANCE, CORROSION DAMAGE WAS NOTED UNDERNEATH THE STRIKER PLATE FOR THE UPPER CLAMSHELL DOOR PIN ENGAGEMENT HOLE LOCATED ON THE MAIN CABIN DOOR POST. (F.S. 213.6) THE DEPTH OF THIS CORROSION IN GREATER THAN 25% OF THE THICKNESS OF THE DOOR POST ANDSep 8, 2022 · N26156 · Cessna 402C · Fuselage Main, StructureSDR HYIA20220909001Rib · elongatedDURING MAINTENANCE, SEVERAL WORKING FASTENERS WERE NOTED ON THE RIGHT HAND CLOSE OUT RIB OF N26156 AT R.W.S. 106.79. THESE FASTENERS ARE COMMON TO THE AFT TRUNNION SUPPORT PLATE. THESE WORKING FASTENERS RESULTED IN ELONGATION OF THE HOLES THROUGH THE RIB BEYONSep 8, 2022 · N26156 · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20220701001Fitting · crackedWHILE PERFORMING A RECURRENT NDT INSPECTION (HFEC) TO SATISFY THE REQUIREMENTS OF TEXTRON 57-10-16, A CRACK WAS FOUND ON THE INBOARD SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK WAS MEASURED AT .055 IN LENGTH. THIS CRACK IS CONSISTENT WITH OTHJul 1, 2022 · N26156 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20201201001Pump · failedTHE PILOT REPORTED A BURNING SMELL IN THE CABIN INFLIGHT WITH THE HEATER TURNED ON AND DISSIPATED WHEN THE HEATER WAS TURNED OFF. MAINTENANCE INSPECTED AND FOUND THE FUEL PUMP DRIVE BROKEN AND REPLACED THE HEATER FUEL PUMP WITH NO FURTHER DEFECTS NOTED.Nov 30, 2020 · N26156 · Cessna 402C · Heating SystemSDR HYIA20190507001Fitting · crackedDURING MAINTENANCE TWO CRACKS WERE IDENTIFIED ON THE INBOARD LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING, (P/N: 5292029-23) THESE CRACKS WERE DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN MEL-54-02R2 TO SATISFY AD2017-10-09. PLEAMay 6, 2019 · N26156 · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20180404001Cylinder · damagedPILOT REPORTED LEFT ENGINE VIBRATION DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE NR 3 CYLINDER WITH A COLLAPSED EXHAUST LIFTER, BROKEN VALVE GUIDE AND THE PISTON PIN BUSHING DAMAGED AND CRACKED. THE CYLINDER AND CONNECTING ROD HAS BEEN CHAMar 30, 2018 · N26156 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160818001Connector · burnedPILOT REPORTED AN ELECTRICAL BURNING ODOR IN THE CABIN. MAINTENANCE INSPECTED AND FOUND WEATHER RADAR INDICATOR HAS BURNED INTERNAL CONNECTOR. PULLED AND COLLARED THE CIRCUIT BREAKER.Aug 17, 2016 · N26156 · Cessna 402C · Navigation System WiringSDR HYIA20160323001B-Nut · loosePILOT REPORTED FUEL SMELL IN CABIN. TIGHTENED UNION JAM NUT & B NUT FOR LINE LEADING INTO RT FUEL TANK, IN RT BOOST PUMP PANEL IAW MM CH 28. LEAK CHECKED GOOD.Mar 21, 2016 · N26156 · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20130306001Switch · failedDURING CRUISE FLIGHT, CREW NOTICED A BURNING ODOR IN COCKPIT AND A SMALL AMOUNT OF HAZE OR SMOKE. DIVERTED AND MADE AN UNSCHEDULED LANDING. ON MX INSPECTION, AVIONICS MASTER SWITCH WAS FOUND DEFECTIVE. SWITCH R & R IAW MM.Mar 4, 2013 · N26156 · Cessna 402C · Electrical Power SystemSDR HYIA20140414044Drag 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 BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A Jan 28, 2013 · N26156 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415022Drag 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 PROCEDURE OFeb 8, 2011 · N26156 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA26156Master Switch · unserviceableCREW REPORTED AVIONICS MASTER SWITCH INOP. MAINTENANCE REMOVED AND REPLACED MASTER SWITCH.Apr 21, 2009 · N26156 · Cessna 402C · Electrical Power SystemSDR GNB2004F00000Line · crackedPILOT PRE-FLIGHT, HYDRAULIC RESERVOIR LOW. MAINTENANCE PRESSURE CHECKED SYSTEM, FOUND NR 6 PRESSURE LINE CRACKED AT BEND RADIUS.Aug 25, 2004 · N26156 · Cessna 402C · Hydraulic System, MainSDR HYI2003F00007Master Switch · inoperativeAVIONICS MASTER SWITCH, INOPERATIVE. MAINTENANCE REPLACED SWITCH AND RETURNED THE AIRCRAFT TO SERVICE.Jun 22, 2003 · N26156 · Cessna 402C · Instrument System Wiring
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