Federal Aviation Administration October 5, 2015 – Federal Register Recent Federal Regulation Documents
Results 1 - 4 of 4
Special Conditions: Gulfstream Model GVII-G500 Airplanes, Side-Stick Controllers; Controllability and Maneuverability
These special conditions are issued for the Gulfstream Model GVII-G500 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is side-stick controllers, instead of conventional-control wheel-and-column design, for pitch and roll control. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Special Conditions: Gulfstream Model GVII-G500 Airplanes, Automatic Speed Protection for Design Dive Speed
These special conditions are issued for the Gulfstream Model GVII-G500 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is associated with a reduced margin between design cruising speed, VC/MC, and design diving speed, VD/MD, based on the incorporation of a high-speed protection system that limits nose-down pilot authority at speeds above VC/MC. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Airworthiness Directives; Airbus Helicopters
We are publishing a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters, which was sent previously to all known U.S. owners and operators of these helicopters. This AD requires inspecting certain tail rotor (T/R) blades, replacing the set of T/R blades if there is damage, deactivating the rotor de-icing system, revising the rotorcraft flight manual (RFM), and installing a placard. This AD is prompted by a report of a T/R de-icing system power supply box stuck in a ``closed'' position providing an uncontrolled and un-annunciated power supply to the system. These actions are intended to detect and prevent structural damage to the T/R blades caused by overheating, and subsequent loss of control of the helicopter.
Change in EST Usage in Notice to Airmen (NOTAM)
This document provides clarity and guidance regarding the use of the contraction ``EST'', which stands for ``Estimated'', when appended to the end of validity time in a NOTAM. The FAA is taking this action to align NOTAM policy with International Civil Aviation Organization (ICAO) standards and recommended practices.
This site is protected by reCAPTCHA and the Google
Privacy Policy and
Terms of Service apply.
