AD 2000-10-11 Airworthiness Directives; Gulfstream Model G-159 Series Airplanes

Models named: G-159 series. Read the applicability below — it usually turns on serial or part numbers too.

Model G-159 series airplanes equipped with pneumatic deicing boots, certificated in any category. To ensure that flightcrews activate the wing and tail pneumatic deicing boots at the first signs of ice accumulation on the airplane, accomplish the following: Note 1: For the purposes of this AD, the following definitions of “older” and “modern” apply: “Modern” pneumatic boot systems may be characterized by short segmented, small diameter tubes, which are operated at relatively high pressures [18-23 pounds per square inch (psi)] by excess bleed air that is provided by turbine engines. “Older” pneumatic boot systems may be characterized by long, uninterrupted, large diameter tubes, which were operated at low pressures by engine driven pneumatic pumps whose pressure varied with engine revolutions per minute (rpm). This low pressure coupled with long and large diameter tubes caused early de-ice systems to have very lengthy inflation and deflation cycles and dwell times. (Dwell time is the period of time that the boot remains fully expanded following the completion of the inflation cycle until the beginning of the deflation cycle.) (a) Within 10 days after the effective date of this AD: Perform a visual inspection to determine if the types of pneumatic deicing boots installed are either “older” or “modern” boots. (1) For those airplanes equipped with “older” pneumatic deicing boots, no further action is required by this AD. (2) For those airplanes equipped with “modern” pneumatic deicing boots: Within 10 days after the inspection required by paragraph (a) of this AD, revise the Limitations Section of the FAA-approved Airplane Flight Manual (AFM) to include the following requirements for activation of the ice protection systems. This may be accomplished by inserting a copy of this AD in the AFM. “• Except for certain phases of flight where the AFM specifies that deicing boots should not be used (e.g., take-off, final approach, and landing), compliance with the following is required. “• Wing and Tail Leading Edge Pneumatic Deicing Boot System, if installed, must be activated: —At the first sign of ice formation anywhere on the aircraft, or upon annunciation from an ice detector system, whichever occurs first; and —The system must either be continued to be operated in the automatic cycling mode, if available; or the system must be manually cycled as needed to minimize the ice accretions on the airframe. • The wing and tail leading edge pneumatic deicing boot system may be deactivated only after leaving icing conditions.” (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate. The request shall be forwarded through an appropriate FAA Operations Inspector, who may add comments and then send it to the Manager, Atlanta ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Atlanta ACO. (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (d) This amendment becomes effective on June 26, 2000. Issued in Renton, Washington, on May 15, 2000. Donald L. Riggin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-12672 Filed 5-19-00; 8:45 am] BILLING CODE 4910-13-U