Owner type Corporation
Year built 1991
Type Rotorcraft
Engine Turbo-shaft
Airworthiness Standard, transport
Airworthiness date February 8, 2017
Certificate issued July 22, 2022
Expires July 31, 2029 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 Registration Potential ADs 48 Information bulletins 1 NTSB investigations 1 FAA incident reports 1 Difficulty reports 12 Potential STCs 50 Related links 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 2026 ADs by the year they took effect: 50 ADs 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.
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 · 1 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 12 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9EKA202004241002 Panel · corroded DURING A CORROSION INSPECTION, MULTIPLE LOCATIONS OF CORROSION FOUND ON THIS PANEL. Apr 21, 2020 · N746H · Bell 214ST · Fuselage Miscellaneous Structure SDR 9EKA201906075003 Blade · eroded DURING CRUISE, HEAVY VIBRATION FELT ON AIRCRAFT. THE AIRCRAFT MADE A PRECAUTIONARY LANDING OFF FIELD. ON INSPECTION, TIP CAP OF MAIN ROTOR BLADE SPLIT AND PEELED BACK. THERE APPEARED TO BE EROSION IN THE SANDY ENVIRONMENT. Jun 5, 2019 · N746H · Bell 214ST · Main Rotor Blades SDR 9EKA20190526005 Hydraulic Line · worn DURING CRUISE FLIGHT, OIL COOLER LIGHT ILLUMINATED. EMERGENCY PROCEDURES CARRIED OUT, SWITCHING THE FAN TO THE SECONDARY BLEED AIR FAN. OIL TEMP REMAINED IN THE GREEN AND THE AIRCRAFT LANDED SAFELY AT BASE. UPON ARRIVAL, IT WAS DETERMINED THAT A LEAK IN THE May 26, 2019 · N746H · Bell 214ST · Hydraulic System, Auxiliary SDR 96ZZZX987 Generator · defective GENERATOR DISENGAGES, LIGHT ON, NO AMP INDICATION. Sep 29, 1995 · N746H · Bell 214ST · DC Generator-Alternator SDR 96ZZZX989 Starter Swtich · defective STARTER SWITCH CUT OFF AT 15 PERCENT N1. Sep 24, 1995 · N746H · Bell 214ST · Engine Cranking SDR 96ZZZX985 Starter · failed STARTER WILL NOT DISENGAGE. Sep 20, 1995 · N746H · Bell 214ST · Starter-Generator SDR 96ZZZX988 Starter · defective STARTER SLOW DURING START, HIGH AMPS, LOW VOLTAGE. Sep 19, 1995 · N746H · Bell 214ST · Starter-Generator SDR 96ZZZX986 Generator · defective NR 2 GENERATOR WILL NOT COME ON LINE. Sep 2, 1995 · N746H · Bell 214ST · DC Generator-Alternator SDR 96ZZZX990 Stick Assy · loose AXIAL PLAY (END CHUCK) IN NR 1 THROTTLE GRIP. COLLECTIVE HEAD RIVETS LOOSE. Aug 20, 1995 · N746H · Bell 214ST · Main Rotor Control SDR 95ZZZX2974 Pa System · defective PA SYSTEM DEFECTIVE. BRIEFING CANNOT BE SELECTED OR TURNED OFF. Mar 13, 1995 · N746H · Bell 214ST · Entertainment System SDR 95ZZZX2973 Amplifier · inoperative AMPLIFIER FAILED. DF 88 DOES NOT POINT. NOTE: UNIT ORIGINALLY RECEIVED WITH NEW ACFT FROM BELL/USA. Mar 6, 1995 · N746H · Bell 214ST · Automatic Direction Finder (ADF) System SDR 95ZZZX2975 Link Assy · bearing worn LINK ASSY, BOTH RUBBER BEARINGS WORN. Jan 16, 1995 · N746H · Bell 214ST · Main Rotor System 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