OpenAirDocs.org

N390AL

Open the Markdown

1990 Bell 214ST · GE CT7 series

Open in FAA registry

© OpenStreetMap
Registered owner
Bank Of Utah Trustee
Location
Salt Lake City, UT
Owner type
Corporation
Serial number
28198
Year built
1990
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
April 5, 2024
Certificate issued
September 8, 2022
Expires
September 30, 2029
Mode S code
A482D4
Bell 214STAirframe model · 18 seats · 2 engines · 18 registeredTCDS H10SWAirframe · Bell 214STEngine modelGE CT7 series

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.

1981In forceSuperseded2026
See all 54 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

Engine · GE CT7 series

SAIB ANE-98-31Issued May 15, 1998

NTSB investigations

No NTSB investigations matched to N390ALMatched 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 · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 19951030041959IFcd/Prec Ldg From Cruise · Gulf Of Mexico, LANarrative: while in cruise flight over the Gulf Of Mexico with an indicated airspeed of 130 knots, the flight crew stated that they began to hear a "whooshing" noise followed by a severe vibration. The pilot stated that the vibration increased to a level that…Oct 30, 1995

Service difficulty reports · 20

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 9EKA20161029017Stud · brokenDURING SCHEDULED INSPECTION, FOUND BROKEN STUD FROM FORWARD RIGHT HAND OUTBOARD COMBINING GEARBOX MOUNT.Oct 29, 2016 · N390AL · Bell 214* · Main Rotor GearboxSDR 2017FA0000421Panel · crackedFUSELAGE LOWER PANEL BELOW LEFT FUEL BLADDER HAS A 30 INCHES LONGITUDINAL CRACK.Jul 2, 2016 · N390AL · Bell 214ST · Fuselage Main, Plate/SkinSDR 9EKA20160702009Skin Panel · crackedDURING A POST FLIGHT INSPECTION, FUSELAGE LOWER PANEL, BELOW LT FUEL BLADDER FOUND TO HAVE A 30" LONGITUDINAL CRACK.Jul 2, 2016 · N390AL · Bell 214ST · Fuselage Main, Plate/Skin
See all 20 reports

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