AD 82-01-01

82-01-01 CANADAIR: Amendment 39-4288. Applies to Model CL-600 airplanes with serial number 1002 to 1050 inclusive. To prevent asymmetric spoiler deployment, accomplish the following within ten days after the effective date of this AD, unless already accomplished:

1. Visually inspect and adjust, if necessary, the left and right controlex cables (parts numbers 600-91305-5 and 600-91305-7) for compliance with the revised rigging procedure specified in Canadair Alert Service Bulletin A600-0024, Revision 1, dated November 6, 1981, or in a manner approved by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Mountain Region.

2. Airplanes may be flown in accordance with FAR 21.197 to a maintenance base for accomplishment of the inspection required by this AD.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the addresses listed above. These documents may also be examined at FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108.

This amendment becomes effective January 4, 1982.