AD 63-15-02

AD Final Rules - DRS_63-15-02.html
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AD Number:
63-15-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; de Havilland Model DH 114 Series Aircraft
Subject:
Bolt Attaching Flap Jack to Wing
Status:
Current
Citation:
Federal Register: July 23, 1963
Citation Publish Date:
07/23/1963
Effective Date:
08/22/1963
Make:
de Havilland Aircraft Co., Ltd., The
Model:
D.H.114 Heron Series 2A | D.H.114 Heron Series 2DA | D.H.114 Heron Series 2X
Product Type:
Aircraft
Product Subtype:
Small/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Superseded AD: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Superseded By: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: 63-15-02
CITATION:   [Federal Register: July 23, 1963]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   63-15-02

SUBJECT HEADING:   Airworthiness Directives; de Havilland Model DH 114 Series Aircraft

ACTION:   Final Rule

SUMMARY:  

DATES:   Effective August 22, 1963.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
63-15-02 DE HAVILLAND: Amdt. 588 Part 507 Federal Register July 23, 1963. Applies to All Model DH 114 Aircraft.

Compliance required within 200 hours' time in service after the effective date of this AD.

Because of instances of fatigue failure of the bolt, P/N 4W.1121, which attaches the flap jack attachment shackle to the wing, replace the bolt with a new special bolt P/N 14W.5835 in accordance with a de Havilland Heron Modification No. 1498.

(de Havilland TNS Series Heron (114) No. C.F.7 Issue 1 dated December 31, 1962, and de Havilland Modification News Sheet No. Heron 1498 dated January 1, 1963, cover this subject.)

This directive effective August 22, 1963.

FOOTER: