- Registered owner
- Velocity Aviation LLC
- Location
- Kalispell, MT
- Owner type
- LLC
- Serial number
- 000144
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- May 18, 2026
- Certificate issued
- May 13, 2026
- Expires
- May 31, 2033
- Mode S code
- A649ED
Eclipse EA500TCDS A00002ACAirframe · Eclipse EA500TCDS E00074ENEngine · Pratt & Whitney Canada PW610F-A
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 7
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2007 | 2 |
|---|---|
| 2008 | 4 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N504MPMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eclipse EA500 aircraft
Investigations 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 investigation describes another aircraft.
FAA incident reports
No FAA accident or incident reports matched to N504MPMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eclipse EA500 aircraft
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.
Service difficulty reports
No reports matched to N504MPGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Eclipse EA500 aircraft
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 20000810SH002Blade · crackedPILOT 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, ONLY TWO SERIAL NUMBERS DIFFERENCE. (X)SDR 20000810SH003Blade · crackedCRACKED 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 LONG WITH A 90-DEGREE TURN FOR ANOTHER .5 INCH. (X)SDR 97ZZZX2038Switch · failedDURING 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 UNSUCCESSFUL FROM BOTH THE PILOTS AND COPILOTS POSITION (STICK). TRIM SYSTEM CIRCUIT BREAKER WAS PULLED
STCs that may be installed · 13
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Eclipse EA500
STC SA03275CHInstallation of an antiskid brake systemSTC SA09887ACInstallation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica
Cellular Module (avCMSTC ST02355CHIncorporation 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.STC SA02265SEInstallation of a camera housingSTC SA03359NYInstallation of STC Configuration 1 (Autothrottles, SDU, FMS updates) or of STC Configuration 2 (Autothrottles update, SVS)STC SA04514NYSingle/Dual Transponder System ADS-B UpgradeSTC SA04460CHREMOVAL OF AFMS GROUND POWER UNIT COLD START LIMITATION ON EA500 AIRCRAFTSTC SA04458CHIncorporation 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.STC SA04306CHIncorporation of RAS Instructions for Continued AirworthinessSTC SA04260CHINSTALL PPG WINDSHIELDSSTC SA04192CHAlternate inspection programSTC SA04166CH-ARemoval of the icephobic coating from the area surrounding static portsSTC SA02946NYInstallation 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.