AD 50-52-01

AD Final Rules - DRS_50-52-01.html
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AD Number:
50-52-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
HAMILTON STANDARD Models Hamilton Standard 2H17 Series Propellers
Subject:
Blades
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company | Hamilton Standard | Kelowna Flightcraft R & D Ltd. | Martin-Marietta Corporation
Model:
DC-6 | DC-6A | DC-6B | Propeller Blades | 240 Series | 202 | 202A
Product Type:
Appliance
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Superseded AD: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Superseded By: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: 50-52-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   50-52-01

SUBJECT HEADING:   HAMILTON STANDARD Models Hamilton Standard 2H17 Series Propellers

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
50-52-01 HAMILTON STANDARD: Applies to All Convair Model 240 Series, Douglas DC-6 and Martin Models 202 and 202A Aircraft Equipped With Hamilton Standard 2H17 Series Blades.

Compliance required daily until further notice.

There have been several cases in which a crack has been detected in Hamilton Standard 2H17 blades during routine ground inspections and recently there was a case in which a section of the blade tip shell was lost in flight requiring an unscheduled landing. In order to eliminate the possibility of other blade failures, the following precautionary measures must be taken:

(1) Thoroughly clean the entire surface of each blade to remove oil, grease, dirt, etc., so that an adequate inspection of the entire blade surface can be made.

(2) Carefully examine visually at close range (12 inches-14 inches) and in detail, the entire surface of each blade for cracks and surface defects in accordance with Hamilton Standard Service Bulletins Nos. 177 and 193. Any suspected areas should then be more closely examined by using a suitable magnifying glass, permanent magnet or any other suitable means as required.

(3) If any cracks are found in the blade surface, it must be retired immediately from service. All doubtful cases should be referred to the propeller manufacturer.

This directive supplements previous Hamilton Standard information on the same subject to all affected operators.

FOOTER: