- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 28105
- Year built
- 1982
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Multiple
- Airworthiness date
- July 14, 2025
- Certificate issued
- September 8, 2022
- Expires
- September 30, 2029
- Mode S code
- A6659E
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 29
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1982 | 1 |
| 1984 | 2 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 1 |
| 1990 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 5 |
| 1998 | 2 |
| 1999 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2013 | 3 |
| 2014 | 1 |
| 2020 | 1 |
See all 31 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N511EVMatched 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 Bell 214ST aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9EKA20160224002Blade · crackedMAIN ROTOR BLADE HAS A 2 INCH CRACK IN THE CHORD DIRECTION OF THE TIP SHOE, CAUSED FROM EROSION, AS A RESULT FROM UNIMPROVED LANDING ZONES.SDR 9EKA2015FA0000414Chip Detector · damagedON RETURN TO BASE, NR 2 ENGINE CHIP DETECTOR CAUTION LIGHT ILLUMINATED AND STAYED ON, EMERGENCY PROCEDURES IAW THE RFM WERE C/W BY THE PIC, CONDUCTED TROUBLESHOOTING AND FOUND ELECTRICAL CHIP DETECTOR HOUSING DAMAGED CAUSING FALSE CAUTION LIGHT, REPLACED WITH SDR 9EKA2015052720Case · cracked90 DEGREE TAIL ROTOR GEAR BOX LOWER LT CASE AROUND MOUNTING STUD BROKEN.SDR 9EKA0514201518Structure · delaminatedRIGHT ENG SERVICE DECK HONEYCOMB PANEL HAS DELAMINATION OF APPROX 3" DIAMETER, STATION 298, BL 25, WL 65.SDR 9EKA2015050517Bulkhead · crackedCRACK 2.75 INCHES FOUND ON AFT LT PYLON BULKHEAD AREA, PREVIOUS HELICOPTER REPAIR COMPLETED.SDR 9EKA02162015002Hose · chafedWHILE IN STEADY STATE CRUISE FLIGHT AT 70% TQ, MAIN TRANSMISSION OIL CAUTION LIGHT ILLUMINATED & THE OIL PRESS GAUGE FOR THE TRANSMISSION WAS OBSERVED DECREASING RAPIDLY. PRECAUTIONARY EMER LANDING WAS MADE IN LESS THAN 1 MIN & THE ACFT SAFELY TOUCHED DOWN.
STCs that may be installed · 50
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 50 STCs