AD 79-17-06

AD Final Rules - DRS_79-17-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
79-17-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BEECH Model 76 Airplanes
Subject:
Main Landing Gear Clevis Pin
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/27/1979
Make:
Textron Aviation Inc.
Model:
76
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 79-17-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3532

AD NUMBER:   79-17-06

SUBJECT HEADING:   Airworthiness Directives; BEECH Model 76 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 27, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-17-06 BEECH: Amendment 39-3532. Applies to Model 76 (Serial Numbers ME-1 through ME-228) Airplanes certificated in all categories.

COMPLIANCE: Required as indicated unless already accomplished.

To prevent possible collapse of the main landing gear, accomplish the following:

A) Within the next twenty-five (25) hours time-in-service after the effective date of this AD, install a new part number MS20392-2C67 clevis pin, common to the main landing gear fork and the fork pin, in the left and right main landing gear in accordance with procedures in Beechcraft Service Instructions Number 1073.

NOTE: Installation of the new larger clevis pins requires a 3/16 (.1875) inch diameter carbide tip drill bit, drill press and a suitable drill press vise or "V" blocks and clamps to hold the fork pin while enlarging the clevis pin hole.

B) Aircraft may be flown in accordance with Federal Aviation Regulation 21.197 to a location where this AD can be accomplished.

C) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective August 27, 1979.

FOOTER: