# Service difficulty reports: N2714M, cancelled May 27, 2023 A list on [N2714M, cancelled May 27, 2023](https://openairdocs.org/deregistered/N2714M-2023-05-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20171027001](https://openairdocs.org/sdr/HYIA20171027001.md): Resistor · burned · Oct 23, 2017 · N2714M · Cessna 402C · Light System Wiring > DURING APPROACH, THE CAPTAINS OVERHEAD LIGHT SWITCH WAS ACTUATED AND THE LIGHT DID NOT ILLUMINATED. THE CREW SUBSEQUENTLY ACTUATED THE COPILOT'S OVERHEAD LIGHT SWITCH WHICH ILLUMINATED AND WAS ACCOMPANIED BY AN ODOR OF SMOKE. THE CAPTAIN SHUTDOWN ALL ELECTR - [SDR HYIA20170828006](https://openairdocs.org/sdr/HYIA20170828006.md): Fitting · cracked · Mar 3, 2017 · N2714M · Cessna 402C · Nacelle/Pylon, Attach Fittings > DURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THERE WAS ONE CRACK IN THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS.108 IN LENGTH. THE OTHER CRACK WAS DISCOVERED ON THE OUTBOARD SIDE O - [SDR HYIA20170828005](https://openairdocs.org/sdr/HYIA20170828005.md): Fitting · cracked · Mar 3, 2017 · N2714M · Cessna 402C · Nacelle/Pylon, Attach Fittings > DURING A ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS MEASURED AT.191 IN LENGTH. - [SDR HYIA20161010167](https://openairdocs.org/sdr/HYIA20161010167.md): Exhaust Valve · damaged · Sep 29, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010166](https://openairdocs.org/sdr/HYIA20161010166.md): Exhaust Valve · damaged · Sep 29, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010165](https://openairdocs.org/sdr/HYIA20161010165.md): Exhaust Valve · damaged · Sep 29, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010164](https://openairdocs.org/sdr/HYIA20161010164.md): Exhaust Valve · damaged · Sep 29, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010163](https://openairdocs.org/sdr/HYIA20161010163.md): Exhaust Valve · damaged · Sep 29, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818082](https://openairdocs.org/sdr/HYIA20160818082.md): Exhaust Valve · damaged · Aug 17, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818081](https://openairdocs.org/sdr/HYIA20160818081.md): Exhaust Valve · damaged · Aug 17, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818080](https://openairdocs.org/sdr/HYIA20160818080.md): Exhaust Valve · damaged · Aug 17, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803051](https://openairdocs.org/sdr/HYIA20160803051.md): Exhaust Valve · damaged · Jul 20, 2016 · N2714M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20150107001](https://openairdocs.org/sdr/HYIA20150107001.md): Spar Cap · mechanic error · Jan 7, 2015 · N2714M · Cessna 402C · Wing Spar > UPON DISASSEMBLY OF RT NACELLE LOWER FAIRING FOR INSPECTION OF RT WING SPAR STRAP IAW SID 57-10-16, UNINTENTIONAL DRILL DAMAGE AT WING SPAR STRAP WAS FOUND BY VISUAL INSPECTION. THE DAMAGE EXISTS JUST OTBD OF THE INBD NACELLE FITTING WITH FWD FACE OF RT WING - [SDR HYIA20140905116](https://openairdocs.org/sdr/HYIA20140905116.md): Transducer · inaccurate · Sep 1, 2014 · N2714M · Cessna 402C · Fuel Flow Indicating > ON INITIAL CLIMB, THE PILOT REPORTED FUEL FLOW OF 160PPH. AFTER REACHING CRUISING ALTITUDE THE FUEL FLOW WENT TO 0 & THE PILOT REPORTED TEMP POWER LOSS. THE PILOT WENT THROUGH THE ENG FAILURE CHECKLIST & PLACED THE AUXILIARY BOOST PUMP ON IN THE HIGH SETTING - [SDR HYIA20140414020](https://openairdocs.org/sdr/HYIA20140414020.md): Drag Brace · cracked · Sep 11, 2012 · N2714M · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 - [SDR HYIA201205170005](https://openairdocs.org/sdr/HYIA201205170005.md): Spar · damaged · May 16, 2012 · N2714M · Cessna 402C · Fuselage Main, Frame > DURING A MX EVENT, DAMAGE WAS DISCOVERED ON THE FORWARD CARRY THROUGH SPAR ASSY. DAMAGE INCLUDES FWD LOWER SPAR WEB FLANGE CRACK AND CORRESPONDING VERTICAL STIFFENER CRACKED AT SAME LOCATION. UPON DISCOVERY OF DAMAGE ACFT WAS SUBMITTED TO MRO. MRO REQUESTED - [SDR HYIA20140415075](https://openairdocs.org/sdr/HYIA20140415075.md): Drag Brace · cracked · Dec 8, 2011 · N2714M · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 IAW - [SDR HYIA20140415043](https://openairdocs.org/sdr/HYIA20140415043.md): Drag Brace · cracked · Apr 5, 2011 · N2714M · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 - [SDR HYIA20140415025](https://openairdocs.org/sdr/HYIA20140415025.md): Drag Brace · cracked · Feb 8, 2011 · N2714M · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 O - [SDR HYIA2714MAVMSTR](https://openairdocs.org/sdr/HYIA2714MAVMSTR.md): Circuit Breaker · unserviceable · Jan 3, 2010 · N2714M · Cessna 402C · DC Power Distribution System > CREW REPORTED AVIONICS BUSS FAILURE. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE. - [SDR HYIA2714M](https://openairdocs.org/sdr/HYIA2714M.md): Unknown · unknown · Feb 7, 2009 · N2714M · Cessna 402C · Nacelle/Pylon Structure > RT ENG SURGING AT CRUISE POWER. RESHAPED LEFT NOSE BOWL DUE TO PROP CABLE ROD END CLEARANCE. - [SDR 1357141120307](https://openairdocs.org/sdr/1357141120307.md): Turbocharger · failed · Dec 3, 2007 · N2714M · Cessna 402C · Exhaust Turbocharger > PILOT LOG READS THE FOLLOWING: LEFT ENG SMOKES ON APPROACH. MAINTENANCE INSPECTED AND FOUND TURBO TO HAVE FAILED. MAINTENANCE REMOVED AND REPLACED THE TURBO. - [SDR HYI2003F00022](https://openairdocs.org/sdr/HYI2003F00022.md): Rheostat · unserviceable · Sep 30, 2003 · N2714M · Cessna 402C · Flight Compartment Lighting > AFTER REACHING CRUISE ALTITUDE, CREW NOTICED SMOKE FROM PEDESTAL LIGHTING RHEOSTATS. DAY/NIGHT SWITCH TURNED OFF, CIRCUIT BREAKERS PULLED, SMOKE STOPPED. DIVERTED TO MECHANIC BASE. MECHANIC REMOVED AND REPLACED DIMMER ASSY AND RETURNED AIRCRAFT TO SERVICE. - [SDR HYI2003F00011](https://openairdocs.org/sdr/HYI2003F00011.md): Computer · failed · Sep 3, 2003 · N2714M · Cessna 402C · Autopilot System > 5 MINUTES INTO CLIMB, CREW REPORTED SMOKE FROM AVIONICS RACK, RETURNED W/O INCIDENT. MECHANIC FOUND A/P PITCH SERVO HARNESS SHORTED, CAUSING A/P COMPUTER TO FAIL INTERNALLY, (TRANSISTORS OVERHEATED AND BURNED) REPAIRED SHORTED HARNESS. REPAIRED A/P COMPUTER, - [SDR HYI2003F00014](https://openairdocs.org/sdr/HYI2003F00014.md): Line · loose · Aug 29, 2003 · N2714M · Cessna 402C · Fuel Storage > ON CLIMB OUT, AFTER FIRST POWER REDUCTION, RIGHT ENGINE COST POWER, ATTEMPTED AUX FUEL PUMP, CROSSFEED, NO HELP. SECURED ENGINE AND FEATHERED PROP. RETURNED W/O INCIDENT. MECHANIC FOUND MAIN FUEL LINE TO ENGINE PUMP LOOSE. TIGHTENED LINE, RETURNED A/C TO S - [SDR HYI2003F00015](https://openairdocs.org/sdr/HYI2003F00015.md): Pump · failed · Aug 27, 2003 · N2714M · Cessna 402C · Fuel Boost Pump > ON CLIMB OUT, TOWER REPORTED SMOKE FROM LT ENGINE, CREW REPORTED LOSS OF POWER AFTER AUX BOOST PUMP WAS TURNED ON, ENGINE SHUT DOWN, RETURNED W/O INCIDENT. MECHANIC REMOVED AND REPLACED LT ENGINE DRIVEN FUEL PUMP. RETURNED AC TO SERVICE. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N2714M' AND deregistration_id = 'N2714M-2023-05-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N2714M-2023-05-27/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.