- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 28130
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- June 29, 1996
- Certificate issued
- September 8, 2022
- Expires
- September 30, 2029
- Mode S code
- A1C8C4
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CT7 model are included below.
On this page
Airworthiness directives that may apply · 48
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 | 2 |
| 1990 | 1 |
| 1994 | 3 |
| 1996 | 1 |
| 1997 | 6 |
| 1998 | 3 |
| 1999 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2013 | 3 |
| 2014 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 2 |
| 2025 | 2 |
See all 54 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Engine · GE CT7 series
SAIB ANE-98-31NTSB investigations
No NTSB investigations matched to N214EBMatched 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 Bell 214ST aircraft
FAA incident reports
No FAA accident or incident reports matched to N214EBMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JYDR20160225 053Ring Gear · crackedMGB REMOVED FOR OIL LEAKING FROM CRACK IN RING GEAR CASE. UPON DISASSEMBLY AT REPAIR STATION DISCOVERED A SECTION OF 13 SPLINE TEETH ON THE UPPER RING FRACTURED. 7 TEETH WERE COMPLETELY SEPARATED FROM THE CASE BUT HELD IN PLACE BY THE INNER RING GEAR ASSY. SDR 9EKA20160219001Stud · shearedTWO MAIN ROTOR TRANSMISSION MAST STUDS FOUND SHEARED OFF DURING 25 HOUR INSPECTION.SDR 9EKA20151201026Chip Detector · activatedPILOT REPORTED MOMENTARY TAIL ROTOR GEAR BOX CHIP LIGHT ON MASTER CAUTION PANEL.SDR 9EKA20151124025Fuel Filter · dirtyNUMBER 1 ENG FUEL FILTER MASTER CAUTION LIGHT CAME ON, INDICATING FUEL FLOW RESTRICTION.SDR 9EKA20150916024Engine · failedDURING CRUISE FLIGHT IN A SHALLOW RIGHT HAND TURN, NR 2 ENG EXPERIENCED HIGH SIDE FAILURE IMMEDIATELY, FOLLOWED BY UNCOMMANDED SHUTDOWN. ACFT RECOVERED 26 MILES BACK TO BASE IN SINGLE ENG CONFIGURATION.SDR 9EKA2015033013Case · crackedDURING PREFLIGHT OIL WAS NOTICED ON THE UPPER TRANSMISSION CASE. UPON FURTHER INVESTIGATION, PAINT WAS BUBBLED ON RING GEAR CASE. CLEANED PAINT & DYE PENETRANT WAS USED REVEALING A SUSPECTED CRACK. ACFT WAS RUN AT 100% NR & OIL WAS NOTICED COMING FROM A CRASDR 9EKA02162015001Skin · debondedTAIL BOOM, EMPENNAGE METALLIC SKIN, HONEYCOMB STRUCTURE ON RT SIDE JUST AFT OF THE FWD VOR ANTENNA MOUNT WL 74, BS 294 HAS DISBONDED. INSPECTION WAS PERFORMED IAW BHT ALL SRM 2-13. TAIL BOOM IS BEING REPLACED WITH REPAIRED SERVICE TAIL BOOM. DAMAGED TAIL BOSDR 9EKA20141114012Pump · failedON APPROACH, CREW NOTICED LOW PRESS ON NR 2 HYD SYS & THE MASTER CAUTION LIGHT, CONSULTED THE EMER CHECKLIST & SHUTOFF NR 2 HYD SYS. LANDED THE ACFT AT ANOTHER LOCATION.SDR 2014FA0000643Access Panel · missingAFTER A ROUTINE MISSION AN ACCESS PANEL LOCATED ON THE AFT PYLON FAIRING ON THE RT SIDE, WAS FOUND NOT INSTALLED ON THE ACFT. THE PANEL IS SECURED AT THE TOP BY A HINGE TO THE AFT PYLON FAIRING. THE HINGE CONSISTS OF 8 SECTIONS ATTACHED TO THE FAIRING AND HASSDR 9EKA20140809009Hydraulic Line · rupturedINFLIGHT CREW NOTED NR 1 HYD SYS FAIL LIGHT ILLUMINATED & PROCEEDED TO SHUT DOWN NR 1 SYS. EXECUTED UNEVENTFUL LANDING. VISUALLY FOUND NR 1 HYD SYS PRESSURE LINE PN 70-060T000Y4B4 TO LT CYCLIC SERVO RUPTURED.SDR 9EKA2013082300003Tab · missingWHILE CONDUCTING A "POST FLIGHT" INSPECTION, MECHANICS NOTICED THAT ONE OF THE MAIN ROTOR BLADES WAS MISSING A TRIM TAB.SDR LCFA2012F00073Attach Fitting · crackedWHILE PERFORMING AN URELATED MX WALK-AROUND INSPECTION, NOTED A CRACK ON THE UPPER LT MAIN FUSELAGE TO TAILBOOM ATTACHMENT FITTING. THIS IS A KNOWN ISSUE.SDR LCFA20110709001Spindle · brokenTHE TRANSMISSION WAS LIFTED TO FACILITATE CHANGING THE LT TRANSMISSION STOP FITTING. IT WAS NOTICED THAT THE LT NODAL BEAM WAS FREE TO ROTATE ON THE TRANSMISSION SPINDLE. IT WAS DISCOVERED THAT IT WAS NOT THE ELASTOMERIC, BUT THAT THE SPINDLE ASSY HAD CRACK
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