- Registered owner
- N222be Inc Trustee
- Location
- Cheyenne, WY
- Owner type
- Corporation
- Serial number
- 000186
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- May 5, 2008
- Certificate issued
- August 17, 2018
- Expires
- August 31, 2028
- Mode S code
- A1E88D
Eclipse EA500TCDS A00002ACAirframe · Eclipse EA500TCDS E00074ENEngine · Pratt & Whitney Canada PW610F-A
From the FAA registry file of October 24, 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 N222BEMatched 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
FAA incident reports
No FAA accident or incident reports matched to N222BEMatched 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
Service difficulty reports
No reports matched to N222BEGeneral 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 N222BE not matched to an aircraft · 14
They name N222BE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR CIEA200600007Check Valve · failedDURING MAINTENANCE OF THE BLEED AIR DISTRIBUTION SYSTEM DUCTING IN THE AFTER EQUIPMENT BAY AREA OF THE AIRCRAFT, SPECIFICALLY REMOVAL OF THE 3 WAY VALVE IN ORDER TO REPLACE SOME LEAKING SEALS, THE CHECK VALVE FOR THE RT ENGINE BLEED AIR SOURCE AIR WAS FOUND TOSDR CIEA200500004Connector · brokenTHE STALL WARNING ACCELEROMETER WAS BEING USED TO TROUBLESHOOT A PROBLEM ON ANOTHER AIRCRAFT. DURING THE REMOVAL OF THE ACCELEROMETER, THE WIRE BROKE ON PIN B OF THE CANNON PLUG. AS PART OF THE TROUBLESHOOTING IT WAS DETERMINED THE PROBLEM ON THE OTHER AIRCRSDR 0041Pressure Switch · out of limitsDURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHAS
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.