N2611X

Service difficulty reports · 36

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 = 'N2611X' 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 HYIA20250725001Fitting · crackedDURING SCHEDULED NONDESTRUCTIVE TESTING AS NOTED IN CESSNA SUPPLEMENTAL INSPECTION DOCUMENT (SID) 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND INBOARD NACELLE FITTING (OEM P/N: 5292029-30) THIS CRACK MEASURES APPROXIMATELY .104 INCHES LONG ON THE LOWER OJul 23, 2025 · N2611X · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20250203001Transistor · burnedPILOT REPORTED A BURNING SMELL IN THE CABIN AFTER TURNING ON INSTRUMENT LIGHTS. MAINTENANCE INSPECTED AND FOUND CO PILOT DIMMING CONTROLLER RESISTOR R1 AND HEAT SINK TRANSISTOR ASSY #7 TRANSISTOR BURNT. REMOVED AND REPLACED RESISTOR AND HEAT SINK ASSY WITH NO Jan 31, 2025 · N2611X · Cessna 402C · Flight Compartment LightingSDR HYIA20241213002Circuit Breaker · failedPILOT REPORTED PLASTIC BURNING SMELL IN CABIN SMELLS FROM LEFT C/B PANEL. MAINTENANCE INSPECTED AND FOUND THE STROBE LIGHT SWITCH INOP. THE SWITCH WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Dec 12, 2024 · N2611X · Cessna 402C · Electrical Power SystemSDR HYIA20240830001Switch · failedPILOT REPORTED STRONG BURNING SMELL IN COCKPIT. NOTICED PROP DE-ICE GAUGE WAS ON BUT THE SWITCH WAS OFF. CYCLED SWITCH BREAKER. DE-ICE GAUGE TURNED OFF, BUT SWITCH REMAINED LOOSE. THEY PULLED C/B'S AS PRECAUTION. MAINTENANCE TROUBLESHOT TO BAD SWITCH. BYPASSEDAug 29, 2024 · N2611X · Cessna 402C · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HYIA20240524003Nut · excess playUPON REMOVAL OF AN ALTERNATOR FOR AN INTERNAL OIL LEAK, THE HUB NUT WAS FOUND TO BE LOOSE, ALLOWING THE THRUST WASHER TO ROTATE BY HAND. THE COTTER PIN REMAINED IN PLACE. THE UNIT WAS REMOVED FROM SERVICE PENDING FURTHER INVESTIGATION.May 20, 2024 · N2611X · Cessna 402C · DC Generating SystemSDR HYIA20200422001Bushing · migratedDURING ROUTINE INSPECTION AND REPLACEMENT OF THE RIGHT ENGINE CYLINDER #6 IT WAS DISCOVERED THAT THE CONNECTING ROD BUSHING OF THE #6 CYLINDER WAS FOUND TO BE LOOSE AND MIGRATING. THE CONNECTING ROD AND CYLINDER WILL BE REPLACED.Apr 21, 2020 · N2611X · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20200313001Hose · brokenPILOT REPORTED RIGHT BRAKE FAILURE. MAINTENANCE INSPECTED AND FOUND THE FLEXIBLE HOSE CONNECTED TO THE RIGHT MASTER CYLINDER BROKEN. REMOVED AND REPLACED THE FLEXIBLE HOSE, AND PREFORMED BLAKE BLEEDING PROCEDURES. NO FURTHER DEFECTS NOTED.Mar 10, 2020 · N2611X · Cessna 402C · Landing Gear Brake SystemSDR HYIA20161108181Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 16, 2016 · N2611X · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160913147Cylinder · low pressureCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Sep 17, 2016 · N2611X · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201609020114Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 30, 2016 · N2611X · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160802003Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jun 8, 2016 · N2611X · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160104002Caliper · defectivePILOT REPORTED BRAKES FAILED ON PARKING. R & R THE LT BRAKE CALIPER & SERVICED BOTH LT & RT BRAKE SYSTEMS. OPERATIONAL & LEAK CHECKED GOOD.Dec 30, 2015 · N2611X · Cessna 402C · BrakeSDR HYIA20151223003Alternator · intermittentPILOT REPORTED BOTH ALTERNATORS KEPT GOING OUT INFLIGHT. INSPECTED ALTERNATORS IAW MM CH 24. RAN ENGS & ALTERNATORS, ALL OPERATIONS CHECKED GOOD.Dec 19, 2015 · N2611X · Cessna 402C · DC Generator-AlternatorSDR HYIA20150918001Door · openPILOT REPORTED THE LT WING LOCKER OPENED DURING FLIGHT. INSPECTED THE DOOR WITH NO DISCREPANCIES FOUND.Sep 14, 2015 · N2611X · Cessna 402C · Wing, Plate/SkinSDR HYIA20150624001Line · faultyPILOT REPORTED LT ENG NOT RESPONSIVE TO THROTTLE CHANGES, DEVELOPING AMBIENT PRESS. ENG SHUTDOWN IN FLIGHT. INSPECTED THE LT ENG & FOUND A BAD MANIFOLD PRESS, MAP, LINE. REPLACED LINE, RAN ENG & FOUND TO BE WITHIN OPERATING LIMITS IAW MM CHAPTER 72 & 81.Jun 17, 2015 · N2611X · Cessna 402C · Manifold Pressure (MP) IndicatingSDR HYIA20140439114Spar · crackedDURING A SCHEDULED MX EVENT, TWO CRACKS WERE FOUND AT THE AFT CARRY THROUGH SPAR WEB FLANGES. THE CRACKS WERE APPROXIMATELY .75 INCHES IN LENGTH & WERE LOCATED AT FS 186.15, RBL 7.75 AT THE FWD & AFT SPAR FLANGE. THE DAMAGE WAS REPAIRED IAW ENGINEERING DRAWIApr 28, 2014 · N2611X · Cessna 402C · Wing SparSDR HYIA20130629106Starter · looseDURING TAKEOFF, THE CREW REPORTED LT ENGINE DECREASING OIL PRESSURE. THE CREW ELECTED TO FEATHER THE PROP, SHUTDOWN THE ENGINE AND RETURN TO ORIGINAL BASE. CONTRACT MX PERFORMED AN INITIAL INSP AND DETERMINED THE LEFT STARTER HAD SEPARATED FROM THE STARTER AJun 26, 2013 · N2611X · Cessna 402C · Engine StarterSDR HYIA20130605100Web · crackedDURING A ROUTINE SCHEDULED INSPECTION, A .62" CRACK WAS FOUND IN THE RT SIDE OF THE FORWARD SPAR WEB AT BS 154.50. DAMAGE WAS MAPPED AND SENT TO ENGINEERING. THE DAMAGED AREA WAS REPAIRED IAW A REPAIR DEFINITION SUPPLIED AND SUBSTANTIATED BY REPORT AAS-SSR-1May 31, 2013 · N2611X · Cessna 402C · Fuselage Miscellaneous StructureSDR HYIA20130426001Engine · damagedFLIGHT CREW REPORTED THAT DURING CRUISE, NOTICED DECREASING MANIFOLD PRESSURE AS WELL AS DIMINISHING OIL PRESSURE ON THE RT ENGINE AT 6,000". CREW SHUTDOWN ENGINE IN FLIGHT. LANDED SAFELY AT DESTINATION AIRPORT. ON MX INSPECTION, DISCOVERED CONNECTING RODS Apr 25, 2013 · N2611X · Cessna 402C · Engine (Reciprocating)SDR HYIA20140414030Drag 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 Nov 28, 2012 · N2611X · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20121126002Bolt · missingPILOT REPORTED THAT DURING LANDING ROLLOUT, THE AIRPLANE YAWED TO THE RIGHT. THE PILOT WAS ABLE TO SAFELY TAXI THE ACFT OFF THE RUNWAY. UPON MX INSPECTION, IT WAS DISCOVERED THAT THE BOLT WAS MISSING FROM THE RT MLG TORQUE LINK AND THAT THE GEAR HAD SPUN 180Nov 24, 2012 · N2611X · Cessna 402C · Main Landing GearSDR HYIA20120817001Alternator · failedPILOT REPORTED AT APPLICATION OF TAKEOFF POWER, SMOKE BEGAN ENTERING THE COCKPIT FROM THE RT SIDE. TAKEOFF WAS ABORTED AND ACFT WAS SUBSEQUENTLY SHUTDOWN AND EVACUATED. ON INSPECTION BY MX, SEVERAL PANELS IN COCKPIT WERE INSPECTED AND FOUND NO EVIDENCE OF SMOAug 13, 2012 · N2611X · Cessna 402C · DC Generator-AlternatorSDR HYIA20140415077Drag 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 IAWAug 9, 2012 · N2611X · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA2012021339811Switch · arcedHEATER FAILED IN FLIGHT. ACFT DIVERTED, DUE TO ODOR OF ELECTRICAL BURNING AND SMALL AMOUNT OF SMOKE IN THE COCKPIT AREA. MX FOUND THE CYCLING SWITCH POINTS ON THE HEATER WERE ARCHING. R & R THE HEATER AND CYCLING POINTS TO CLEAR DISCREPANCY.Feb 13, 2012 · N2611X · Cessna 402C · Heating SystemSDR HYIA20140415042Drag 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 · N2611X · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA2611XKG102Gyro · odorIN CLIMB CONFIGURATION, (APPROX 1800 FT), CREW REPORTED HEADING FLAG IN VIEW. CLIMBING THROUGH 2000 FT, CREW REPORT STRONG SMELL "CHLORINE LIKE ODOR". CREW ELECTED TO RETURN TO BASE, AFTER CONCLUDING THAT THERE MAY BE AN ELECTRICAL SHORT CIRCUIT, OR POSSIBLEMar 29, 2010 · N2611X · Cessna 402C · Directional Gyro and Indicating SystemSDR HYIA2611XWSStatic Inverter · burnedCREW REPORTED DURING CLIMB OUT, THE WIRING LOCATED ON THE LT SIDE OF THE HEATED (ELECTRIC) WINDSHIELD SPARKED, AND SMOKE IMMEDIATELY DEVELOPED. WINDSHIELD HEAT WAS TURNED OFF, AND THE SMOKE DISCONTINUED. ICE BEGAN TO DEVELOPE ON WINDSHIELD, RESULTING IN A TURNJan 5, 2010 · N2611X · Cessna 402C · Pitot/Static SystemSDR HYIA2611XNLG105Switch · out of rigCREW REPORTED, ON APPROACH, NORMAL GEAR DOWN INDICATION UNTIL FLAPS WERE SELECTED BEYOND 15 DEGREES. GEAR UNLOCK LIGHT ILLUMINATED, AND NOSE GEAR DOWN LOCK LIGHT FLICKERED, GEAR WARNING HORN SOUNDED. ABORTED APPROACH TO TROUBLESHOOT SYS. SUBSEQUENT GEAR EXTOct 5, 2009 · N2611X · Cessna 402C · Landing Gear Position and WarningSDR HYIA2611XAVSWXCircuit Breaker · unserviceablePREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE. MX REMOVED AND REPLACED CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.Aug 30, 2009 · N2611X · Cessna 402C · DC Power Distribution SystemSDR HYIAN2611XEngine · failedON FINAL APPROACH, PILOT REPORTED LEFT ENGINE STARTED TO SPUTTER, AND RUN ROUGH, FOLLOWED BY SEVERE VIBRATION AND ENGINE STOPPAGE. MAINTENANCE FOUND CATASTROPHIC FAILURE OF THE LEFT ENGINE WITH A LARGE HOLE IN THE TOP ENGINE CASE FROM CONNECTING ROD PENETRATIJun 7, 2009 · N2611X · Cessna 402C · Engine (Reciprocating)SDR HYIA20090330001Limit Switch · unserviceableCREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AIRCRAFT, DETERMINED SOURCE OF SMOKE TO BE FROM AIRCRAFT HEATER DUCT LIMIT SWITCH. MAINTENANCE REMOVED AND REPLACED HEATER DUCT LIMIT SWITCH. AIRCRAFT RETURNED TO SERVICE.Mar 30, 2009 · N2611X · Cessna 402C · Heating SystemSDR HYIA2611XEngine · failedRIGHT ENGINE FAILURE ON 1/2 MILE FINAL TO RUNWAY 25 AT PVC, CREW FEATHERED ENGINE AND LANDED. LATER INSPECTION ON 5-27-07 FOUND INTERNAL FAILURE IN THE RIGHT ENGINE. ENGINE REMOVED AND REPLACED ON 5-28-07. A/C RETURNED TO SERVICE AND ENG TO BE SENT TO MANUFMay 27, 2007 · N2611X · Cessna 402C · Engine (Turbine/Turboprop)SDR HYIA052707Engine · failedRIGHT ENGINE FAILURE ON 1/2 MILE FINAL TO RUNWAY 25 AT PVC, CREW FEATHERED ENGINE AND LANDED. LATER INSPECTION ON 5-27-07 FOUND INTERNAL FAILURE IN THE RIGHT ENGINE. ENGINE REMOVED AND REPLACED ON 5-28-07. A/C RETURNED TO SERVICE AND ENG TO BE SENT TO MANUFMay 27, 2007 · N2611X · Cessna 402C · Engine Emergency Shutdown SystemSDR HYI2005F00004Seat · brokenPILOT REPORTED FIXED BACK DOUBLE PASSENGER SEAT BROKEN. MAINTENANCE FOUND SEAT SEPARATED FROM PEDASTAL. REMOVED AND REPLACED SEAT AND SENT BACK TO ORIGINAL MFG FOR REPAIR. SEAT WAS INSTALLED UNDER AVIATION FABRICATOR STC SA2716CE. (K)Mar 7, 2005 · N2611X · Cessna 402C · Passenger Compartment EquipmentSDR HYI2003F00012Master Switch · burnedCLIMBING THROUGH 1000 FEET, CREW NOTICED SMOKE COMING FROM AVIONICS MASTER SWITCH, TURNED OFF SWITCH, TURNED ON ALTERNATE AVIONICS SWITCH, LANDED WITHOUT INCIDENT. MECHANIC REMOVED OLD, REPLACED SWITCH.Aug 18, 2003 · N2611X · Cessna 402C · Central WarningSDR 20001204SH015Seal · leakingAFTER DEPARTURE, CREW SMELLED FUEL AND RETURNED TO LAND, LANDING WITHOUT INCIDENT. MAINTENANCE FOUND HEATER FUEL FILTERS LEAKING. REMOVED AND REPLACED GASKET. OPS AND LEAK CHECKED OK. AIRCRAFT RELEASED FOR RETURN TO SERVICE. (X)Oct 18, 2000 · N2611X · Cessna 402C · Heating System
Back to N2611X