AD 67-20-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Pacific Propeller, Inc. | A6441FN-606 | ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers |
| propeller | Pacific Propeller, Inc. | A6441FN-606 | ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers |
Unsafe Condition
Retention bolts may fail, leading to serious overspeeds and reduced effectiveness of the propeller pitch lock under remote combinations of critical component failures.
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Required Actions
Install Part No. 6859637 restrictor in the increase pitch port of each hub island and replace the eight master gear retention bolts with P/N 6859881 bolts. Actions must be accomplished as outlined in specified Allison documents.
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Compliance Time
On or before November 1, 1967
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Affected Aircraft
Pacific Propeller, Inc. Models A6441FN-606 and A6441FN-606A Propellers
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Federal Register Abstract
Retention Bolts
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-20-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-20-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers Subject: Retention Bolts Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/23/1967 Make: Pacific Propeller, Inc. Model: A6441FN-606 Product Type: Propeller Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-20-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-466 AD NUMBER: 67-20-01 SUBJECT HEADING: ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers ACTION: SUMMARY: DATES: Effective August 23, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: 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. FOOTER:
Document Text
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AD Final Rules - DRS_67-20-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-20-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers Subject: Retention Bolts Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/23/1967 Make: Pacific Propeller, Inc. Model: A6441FN-606 Product Type: Propeller Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-20-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-466 AD NUMBER: 67-20-01 SUBJECT HEADING: ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers ACTION: SUMMARY: DATES: Effective August 23, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: 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. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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