AD 48-31-01

AD Final Rules - DRS_48-31-01.html
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AD Number:
48-31-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Grumman Model G-44 and G-44A Aircraft
Subject:
Stabilizer Strut
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Gulfstream American Corporation
Model:
G-44 | G-44A
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 48-31-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-31-01

SUBJECT HEADING:   Airworthiness Directives; Grumman Model G-44 and G-44A Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-31-01 GRUMMAN: Applies to G-44 and G-44A Aircraft.

To be accomplished by September 15, 1948.

Inspect upper terminal (P/N 17257-1) of stabilizer strut (P/N 17256) for cracks extending radially from the outside edge of the ears to the inside of the hole in which the shoulder bushings are pressed. Cracked terminals should be replaced with steel terminals. All terminals without cracks may be left in service if inspected every 100 hours.

(Grumman Aircraft Engineering Corp. Service Bulletin No. 22 dated July 1, 1948, covers this same subject.)

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