AD 79-02-04

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AD Number:
79-02-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Costruzioni Aeronautiche Model A109 and A109A Helicopters
Subject:
Tail Rotor Drive Shaft
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/19/1979
Make:
Agusta S.p.A.
Model:
A109 | A109A
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Superseded AD: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Superseded By: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: 79-02-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3396

AD NUMBER:   79-02-04

SUBJECT HEADING:   Airworthiness Directives; Costruzioni Aeronautiche Model A109 and A109A Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective February 19, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-02-04 COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA: Amendment 39- 3396. Applies to Model A109 and A109A helicopters, serial numbers 7109 and below, certificated in all categories, incorporating tail rotor drive shaft hanger bearing support bracket, P/N 109-0370-02-1.

Compliance is required as indicated, unless already accomplished.

To prevent a possible tail rotor failure, accomplish the following:

(a) Within the next 10 hours time in service after the effective date of this AD, and thereafter following the last flight of each day in which the helicopter is operated, inspect the tail rotor drive shaft hanger bearing support bracket, P/N 109-0370-02-1, for cracks in accordance with Part I of the "Accomplishment" paragraph of Agusta Bollettino Tecnico No. 109-2, dated April 14, 1976, including Rev. A dated May 11, 1976, or an FAA-approved equivalent (hereinafter referred to as Service Bulletin).

(b) If a crack is found during an inspection required by this AD, before further flight, except as provided in paragraph (d) of this AD, replace the affected bracket with -

(1) A serviceable bracket of the same part number, and continue to inspect in accordance with paragraph (a) of this AD after the last flight of each day in which the helicopter is operated; or,

(2) A new support bracket, P/N 109-0370-12-1, in accordance with Part II of the "Accomplishment" paragraph of the Service Bulletin.

(c) Within the next 100 hours time in service after the effective date of this AD, replace the support bracket, P/N 109-0370-02-1 with a new bracket, P/N 109-0370-12-1, in accordance with Part II of the "Accomplishment" paragraph of the Service Bulletin. The repetitive inspections required by paragraphs (a) and (b)(1) of this AD may be discontinued upon installation of a support bracket, P/N 109-0370-12-1, in accordance with this AD.

(d) Helicopters may be flown in accordance with FAR's 21.197 and 21.199 to a base where the required work can be performed.

This amendment becomes effective February 19, 1979.

FOOTER: