AD 65-08-01

AD Final Rules - DRS_65-08-01.html
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AD Number:
65-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hawker Siddeley Model 114 Heron Aircraft
Subject:
Main Ground Assembly
Status:
Current
Citation:
Federal Register: April 2, 1965
Citation Publish Date:
04/02/1965
Effective Date:
05/03/1965
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Superseded AD: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Superseded By: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: 65-08-01
CITATION:   [Federal Register: April 2, 1965]

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-52

AD NUMBER:   65-08-01

SUBJECT HEADING:   Airworthiness Directives; Hawker Siddeley Model 114 Heron Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective May 3, 1965.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
65-08-01 HAWKER SIDDELEY: Amdt. 39-52 Part 39 Federal Register April 2, 1965. Applies to de Havilland Model 114 "Heron" Aircraft.

Compliance required as indicated.

To prevent further cases of overheating of electric cables in the cockpit and fuselage nose area, accomplish the following:

Within the next 25 hours' time in service after the effective date of this AD, unless already accomplished, dismantle, clean, inspect, replace and modify as required, the main ground (earth) assembly in the forward fuselage in accordance with Hawker Siddeley Technical News Sheet Heron (114) No. N.4, Issue 1, dated July 20, 1964.

(Hawker Siddeley Aviation, de Havilland Division, Technical News Sheet Heron (114) No. N.4, Issue 1, dated July 20, 1964, covers this same subject.)

This directive effective May 3, 1965.

FOOTER: