AD 80-03-07

AD Final Rules - DRS_80-03-07.html
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AD Number:
80-03-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BELL Model 205A-1, Helicopters
Subject:
Fuselage Main Beams Splice
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/05/1980
Make:
Bell Helicopter Textron, Inc.
Model:
205A-1
Product Type:
Aircraft
Product Subtype:
Rotorcraft
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 80-03-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3681

AD NUMBER:   80-03-07

SUBJECT HEADING:   Airworthiness Directives; BELL Model 205A-1, Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective February 5, 1980.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-03-07 BELL: Amendment 39-3681. Applies to Bell Model 205A-1 helicopters, S/N 30001 through 30287 and S/N 30289 through 30296, certificated in all categories.

Compliance required prior to further flight after March 4, 1980, unless already accomplished.

To assure fuselage structural integrity by installing Monel rivets in the fuselage main beams splice, in place of improper aluminum rivets, accomplish the following:

a. Inspect right and left main beam splice (BL14), WL54 from station 127.5 to 154 as specified in Bell Helicopter Textron Technical Bulletin No. 205-79-34.

b. Equivalent means of compliance with this AD may be approved by the Chief, Administration, Southwest Region.

c. The helicopters may be flown in accordance with FAR 21.197 to a base where inspections and repairs can be performed.

This amendment becomes effective February 5, 1980.

FOOTER: