AD 68-21-04

Active

Ice Damage to Engine

Key Information
68-21-04
Active
October 17, 1968
Not specified
Unknown
39-668
Applicability
["Aircraft"]
["Small Airplane"]
Textron Aviation Inc.
65-90 65-A90 65-A90-1 B90
Regulatory Text

68-21-04 BEECHCRAFT: Amendment 39-668. Applies to Models 65-90, 65-A90 and 65-B90 aircraft (Serial Numbers LJ-1 through LJ-406) and 65-A90-1 aircraft (Serial Numbers LM-1 through LM-129).

Compliance required as indicated.

To reduce the possibility of engine damage and malfunction while operating in icing conditions above 15,000 feet MSL, within one year after the effective date of this Airworthiness Directive, unless already accomplished, accomplish the following:

(A) Install seal strips and a spring lockdown assembly on the Inertial Separator Vane and an automatic ignition (re-light) system in accordance with the method outlined in Beechcraft Service Instructions #0115-010 dated October 1, 1968.

(B) Equip the airplane with the applicable FAA Flight Manual as set forth in Beechcraft Service Instructions #0115-010 dated October 1, 1968.

(C) The Emergency Order Amending Type Certificate No. 3A20 dated May 24, 1968, as amended September 19, 1968, shall remainin force and effect as to each individual aircraft covered by this Airworthiness Directive until paragraphs (A) and (B) have been accomplished.

This amendment becomes effective October 17, 1968.

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References
This information is not available.
--- - Part 39
FAA Documents