Rosoboronexport, a member of Rostec, expects a heightened interest of foreign customers in Russian aircraft and AD systems at the International Paris Air Show 2017. This largest aviation show in the world is to take place in Le Bourget, France, on June 19-25. “Rosoboronexport witnesses heightened interest in modern aviation equipment on the world market…. Read more »
Source: State Corporation Rostec, 20-Jun-17
Updated placarding required. Applicable to _ALL_ Bell models, plus Eurocopter EC135 and Bo105
Source: FAA, 14-Dec-11
Main Rotor Blades – Inspection and Replacement
Source: NZ CAA, 01-Dec-11
Non-conformities on adjustment of some hydromechanical units (HMUs) have been reported by a Turbomeca repair centre. The technical investigations carried out by Turbomeca are showing that only a limited number of HMUs are potentially affected by this non-conformity to HMU adjustment.
Source: FAA, 29-Nov-11
N2 (power turbine speed) sensor harness wire crimping discrepancy
Source: FAA, 22-Nov-11
Number 2 Modular Avionic Unit (MAU) ventilation duct
Source: FAA, 21-Nov-11
Monitor the power display when a generator is deactivated
Source: FAA, 21-Nov-11
Supercedes AD 2003-22-06. Tail rotor pitch control rod
Source: FAA, 10-Nov-11
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2011-1188; Directorate Identifier 2008-SW-46-AD] RIN 2120-AA64 Airworthiness Directives; Bell Helicopter Textron, Inc. (Bell) Model 204B, 205A, 205A-1, 205B, and 212 Helicopters Preamble Information AGENCY: Federal Aviation Administration, DOT. ACTION: Notice of proposed rulemaking (NPRM). ———————————————————————– SUMMARY: This document proposes superseding four existing airworthiness… Read more »
Source: FAA, 04-Nov-11
Upper end fitting ball joints of the main rotor servocontrols
Source: FAA, 27-Oct-11
Side mounting of pilot and co pilot seats
Source: FAA, 27-Oct-11
Rotorcraft Flight Manual, Limitations section
Source: FAA, 27-Oct-11
Vertical Stabilizer Control System tube adaptors
Source: FAA, 18-Oct-11
Actions to be taken when a generator is deactivated
Source: FAA, 29-Sep-11
Main rotor scissor fitting assembly
Source: FAA, 26-Aug-11
This AD supersedes and cancels EASA AD No. 2006-0252 dated 22 August 2006
Source: EASA, 27-Jan-10
This AD revises EASA Emergency AD 2009-0230-E dated 23 October 2009
Source: EASA, 07-Jan-10
The EASA, which is the Technical Agent for the Member States of the European Community, has issued EASA AD No. 2008-0142-E, dated July 30, 2008, to correct an unsafe condition associated with hoist cable assemblies installed on Agusta Model AB412 and AB412 EP helicopters.
Source: FAA, 04-Sep-09
