# N504MP: 2008 Eclipse EA500 - Status: Valid registration - Airframe: [Eclipse EA500](https://openairdocs.org/model/eclipse-ea500) (registry code 3350000, 6 seats) - Engine: [Pratt & Whitney Canada PW610F-A](https://openairdocs.org/engine/pratt-whitney-canada-pw610f-a) (registry code 52267) - Data sheets: [TCDS A00002AC](https://openairdocs.org/tcds/A00002AC) (Eclipse Aerospace Inc.), [TCDS E00074EN](https://openairdocs.org/tcds/E00074EN) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 000144 - Year built: 2008 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, normal - Airworthiness date: May 18, 2026 - Certificate issued: May 13, 2026 - Expires: May 31, 2033 - Mode S code: A649ED - Registered owner: [Velocity Aviation LLC](https://openairdocs.org/faa-owner/VELOCITY%20AVIATION%20LLC) - Location: [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell) - Owner type: LLC - Owner's area on the map: 48.2306° N, 114.4033° W: Placed by OpenAirDocs at the center of ZIP code 59901, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=504MP - Page: https://openairdocs.org/aircraft/N504MP From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 7 in force ### Matched by airframe (Eclipse EA500) - [AD 2013-16-04](https://openairdocs.org/ad/2013-16-04): Communications · Eclipse Aerospace EA500. Effective Sep 20, 2013 - [AD 2011-06-06 R1](https://openairdocs.org/ad/2011-06-06-R1): Engine · Eclipse Aerospace EA500. Effective Jan 23, 2012 - [AD 2010-20-24](https://openairdocs.org/ad/2010-20-24): Communications · Eclipse Aerospace EA500. Effective Nov 9, 2010 - [AD 2008-19-01](https://openairdocs.org/ad/2008-19-01): Airplane flight manual (AFM) · Eclipse Aerospace EA500. Effective Sep 29, 2008 - [AD 2008-16-15](https://openairdocs.org/ad/2008-16-15): Throttle lever · Eclipse Aerospace EA500. Effective Aug 7, 2008 - [AD 2008-02-04](https://openairdocs.org/ad/2008-02-04): Pitot system · Eclipse Aerospace EA500. Effective Feb 26, 2008 - [AD 2007-24-12](https://openairdocs.org/ad/2007-24-12): Inspect the fuel filler adapters for primer and/or paint in the surround · Eclipse Aerospace EA500. Effective Nov 27, 2007 ### Matched by engine (Pratt & Whitney Canada PW610F-A) None in force. ### Historical (superseded or no longer in force) - [AD 2011-06-06](https://openairdocs.org/ad/2011-06-06) (historical): Engine · Eclipse Aerospace EA500. Effective Mar 21, 2011 - [AD 2008-24-07](https://openairdocs.org/ad/2008-24-07) (historical): Airplane flight manual (AFM) · Eclipse Aerospace EA500. Effective Dec 4, 2008 - [AD 2008-13-51](https://openairdocs.org/ad/2008-13-51) (historical): Throttle · Eclipse Aerospace EA500 - [AD 2007-13-11](https://openairdocs.org/ad/2007-13-11) (historical): Airplane flight manual (AFM) · Eclipse Aerospace EA500. Effective Jun 27, 2007 ## Information bulletins (advisory) (4 in force) - [SAIB CE-12-30](https://openairdocs.org/saib/CE-12-30): Wing, Fuselage Attach Fittings. Issued May 8, 2012 - [SAIB CE-12-28](https://openairdocs.org/saib/CE-12-28): Battery/Charger System. Issued Apr 17, 2012 - [SAIB CE-12-13](https://openairdocs.org/saib/CE-12-13): Ailerons. Issued Jan 24, 2012 - [SAIB CE-09-14](https://openairdocs.org/saib/CE-09-14): Eclipse EA500. Issued Feb 27, 2009 ## NTSB investigations None matched to N504MP. ## NTSB investigations on N504MP not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR14TA236](https://openairdocs.org/ntsb/WPR14TA236), Jun 8, 2014: Mcdonnell Douglas Helicopter 369E (N504MP), Mesa, AZ, substantial damage. Probable cause: The loss of engine power during cruise flight due to the decoupling of the engine’s turbine and compressor sections. Contributing to the decoupling was the excessive wear of the turbine-to-compressor… ## FAA accident and incident reports None matched to N504MP. ## Reports on N504MP not matched to an aircraft (1) They name N504MP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 20140608010449A](https://openairdocs.org/incident/20140608010449A), Jun 8, 2014: Mcdonnell Douglas Helicopter 369E (N504MP), Gilbert, AZ, Substantial damage. On 06/08/2014 at 0105 local time, mesa police dept helicopter N504MP experienced a loss of power during flight. Pilot reports engine began to slowly "spin… ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N504MP not matched to an aircraft (4) They name N504MP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 20000810SH002](https://openairdocs.org/sdr/20000810SH002), Jul 12, 2000: BLADE. CRACKED. PILOT FOUND TAIL ROTOR BLADE ROOT FITTING CRACKED ON A PRE-FLIGHT INSPECTION. THIS IS THE SECOND OCCURRENCE ON THIS AIRCRAFT. THE LAST BLADE, S/N 009999-1489, O - [SDR 20000810SH003](https://openairdocs.org/sdr/20000810SH003), Mar 9, 2000: BLADE. CRACKED. CRACKED BLADE WAS FOUND ON POST-FLIGHT AFTER THE PILOT FELT AN IN-FLIGHT VIBRATION. THE TAIL ROTOR BLADE WAS CRACKED FROM THE INBOARD ROOT FITTING, 1.5 INCHES L - [SDR 97ZZZX2038](https://openairdocs.org/sdr/97ZZZX2038), Mar 5, 1997: SWITCH. FAILED. DURING NORMAL OPERATIONS, THE TRIM SYSTEM CONTINUED TO DRIVE TO THE LEFT LATERAL CYCLIC STOP. ATTEMPTS TO BRING THE TRIM BACK TO THE NEUTRAL POSITION WERE UNSUC - [SDR 96ZZZX4278](https://openairdocs.org/sdr/96ZZZX4278), Aug 13, 1996: SWITCH. FAILED. PILOT REPORTED NO TRIM IN FORE/AFT DIRECTION. DURATION OF FLIGHT HAD TO FIGHT HIGH FORE/AFT STICK FORCES. SUBMITTER STATED A COMMON PROBLEM, SWITCH IS TOO LIGHT ## STCs that may be installed (OpenAirDocs) (13) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Eclipse EA500) - [STC SA03275CH](https://openairdocs.org/stc/SA03275CH): Installation of an antiskid brake system. Lee Air Inc - [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc - [STC ST02355CH](https://openairdocs.org/stc/ST02355CH): Incorporation of Aircraft Maintenance Manual sections listed on Resurgent Aviation Solutions Master Data List E50-MDL-0005-020, Rev. 1 dated November 9, 2021 or later FAA Approved revision. Resurgent Aviation Solutions LLC - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA03359NY](https://openairdocs.org/stc/SA03359NY): Installation of STC Configuration 1 (Autothrottles, SDU, FMS updates) or of STC Configuration 2 (Autothrottles update, SVS). Innovative Solutions & Support Inc - [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS - [STC SA04460CH](https://openairdocs.org/stc/SA04460CH): REMOVAL OF AFMS GROUND POWER UNIT COLD START LIMITATION ON EA500 AIRCRAFT. RESURGENT AVIATION SOLUTIONS LLC - [STC SA04458CH](https://openairdocs.org/stc/SA04458CH): Incorporation of an Alternate Maintenance Program on EA500 aircraft per Resurgent Aviation Solutions Instructions for Continued Airworthiness, Document E50-ICA-0405-010 Rev. 1, dated May 4, 2020 or later FAA Approved Revision. Resurgent Aviation Solutions LLC - [STC SA04306CH](https://openairdocs.org/stc/SA04306CH): Incorporation of RAS Instructions for Continued Airworthiness. Resurgent Aviation Solutions LLC - [STC SA04260CH](https://openairdocs.org/stc/SA04260CH): INSTALL PPG WINDSHIELDS. RESURGENT AVIATION SOLUTIONS LLC - [STC SA04192CH](https://openairdocs.org/stc/SA04192CH): Alternate inspection program. Resurgent Aviation Solutions LLC - [STC SA04166CH-A](https://openairdocs.org/stc/SA04166CH-A): Removal of the icephobic coating from the area surrounding static ports. Cary Winter Resurgent Aviation Solutions, LLC - [STC SA02946NY](https://openairdocs.org/stc/SA02946NY): Installation of Innovative Solutions & Support - (IS&S) Operational Class Gamma 3 Flight Management System (FMS) Option and dual Beta 3 Global Positioning System (GPS) receivers in accordance with IS&S Master Drawing List, 1D-08570 Revision 4, dated March 18, 2011. Innovative Solutions & Support Inc ## Related - Other Eclipse EA500 aircraft: https://openairdocs.org/model/eclipse-ea500/aircraft.md - The Pratt & Whitney Canada PW610F-A engine: https://openairdocs.org/engine/pratt-whitney-canada-pw610f-a.md --- 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.