AD 74-17-02

AD Final Rules - DRS_74-17-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-17-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; VERTOL Model 107-II type Helicopters
Subject:
Rotor Blade Inspection System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/13/1974
Make:
Columbia Helicopters, Inc.
Model:
107-II
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Superseded AD: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Superseded By: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: 74-17-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1915

AD NUMBER:   74-17-02

SUBJECT HEADING:   Airworthiness Directives; VERTOL Model 107-II type Helicopters

ACTION:  

SUMMARY:  

DATES:   Effective August 13, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-17-02 VERTOL: Amendment 39-1915. Applies to Vertol Model 107-II type helicopters certificated in all categories.

1. Prior to the next flight after the effective date of this AD, unless already accomplished, an inspection program for the rotor blades which has been approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, subsequent to March 28, 1974 must be initiated.

2. An acceptable program is one afforded by forward and aft rotor blades altered, inspected and maintained in accordance with Boeing Vertol Service Bulletin 107-329 or later FAA approved revisions. The visual checks of the rotor blade pressure indicator required by paragraph 2 of this AD may be performed by the pilot.

This amendment is effective August 13, 1974.

FOOTER: