AD 67-20-01

final rule

ALLISON - AERO PRODUCTS Models A6441FN-606 and A6441FN-606A Propellers

AD Number
67-20-01
Status
final_rule
Effective Date
Product Category
propeller
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

Applicability

TypeManufacturerModelDetails
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.

AI-generated summary from the source AD text. Verify against the official source before acting.

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

On or before November 1, 1967

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Pacific Propeller, Inc. Models A6441FN-606 and A6441FN-606A Propellers

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Retention Bolts

Applicability Source Text

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AD Final Rules - DRS_67-20-01.html
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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Superseded AD: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Superseded By: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

Show stored source text (verify against official source)
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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