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AD 67-20-01 ACTIVE

Retention Bolts
Key Information
AD Number 67-20-01 Status Active
Effective Date August 23, 1967 Issue Date Not specified
Docket Number Unknown Amendment 39-466
Product Type ["Propeller"] Product Subtype Not specified
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Pacific Propeller, Inc.
Model(s) A6441FN-606
Regulatory Text

67-20-01 ALLISON - AERO PRODUCTS: Amdt. No. 39-439 as revised Amdt. 39-466, Part 39, Federal Register June 29, 1967. Applies to Models A6441FN-606 and A6441FN-606A Propellers.

Compliance required as indicated, unless already accomplished.

To prevent serious overspeeds and to make the propeller pitch lock more effective under remote combinations of critical component failures, accomplish the following:

(a) On or before November 1, 1967, install Part No. 6859637 restrictor in the increase pitch port of each hub island, as outlined in Allison Commercial Service Letter CSL 189, Pages 14 and 15, Paragraph C2b(1)(2)(3) and (4), entitled "Hub Assembly - Preparation for Assembly."

(b) On or before November 1, 1967, remove the eight master gear retention bolts and install eight P/N 6859881 bolts as replacements, as outlined in Allison's Commercial Propeller Bulletin, CPB No. 63-317.

This amendment effective August 23, 1967.

Revised August 23, 1967.