AD 49-15-02

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AD Number:
49-15-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Martin Model 202 Aircraft
Subject:
Wing Modifications
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Martin-Marietta Corporation
Model:
202
Product Type:
Aircraft
Product Subtype:
Large 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Superseded AD: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Superseded By: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: 49-15-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   49-15-02

SUBJECT HEADING:   Martin Model 202 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
49-15-02 MARTIN: Applies to All Model 202 Aircraft.

I. To be accomplished prior to return to service.

The wing splice attachment fitting, Station 187, must be inspected and reworked in accordance with the procedures outlined in Martin Service Bulletin No. 73, revised May 10, 1949, including the following amendments; Amendment 1, revised October 14, 1948; Amendment 2, revised May 10, 1949; Amendment 3, dated October 5, 1948; Amendment 4, dated October 15, 1948; Amendment 5, dated December 27, 1948; Amendment 6, dated May 10, 1949.

II. Compliance required as indicated.

The inspections outlined in the above Service Bulletin No. 73 must be conducted on all aircraft as follows:

1. Conduct the inspections outlined above in Service Bulletin 73 at maximum intervals of 900 hours and beginning with the last inspection conducted at approximately 1,500 hours total flight time, the succeeding intervals shall not exceed 600 hours.

2. Conduct the inspections of amendments 2 and 6 of Service Bulletin 73 between 1,500 and 1,700 total flight hours and at maximum intervals of 200 hours thereafter.

As an added precautionary measure do not operate the aircraft in excess of 90 percent of the Placard Vne and Vno speeds as shown in Aircraft Specification A-795. In the event any turbulence is encountered in flight, immediately reduce the speed to a maximum of 170 m.p.h. and further reduce the speed to a maximum of 150 m.p.h. dependent upon the severity of the turbulence. (Suitable revisions to the operating manual will be provided.)

III. Compliance required as indicated.

1. Compliance with the Glenn L. Martin Schedule No. 202-87-1, calling for the return of 202 aircraft to the Glenn L. Martin Co. factory during 1949 for incorporation of modifications described in Martin Service Bulletin No. 87 is hereby directed.

2. After this has been accomplished on each airplane, items I and II are no longer applicable to that airplane.

This supersedes AD 49-09-01.

FOOTER: