AD 73-13-06

AD Final Rules - DRS_73-13-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
73-13-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hawker Siddeley Model DH-114 "Heron" Airplanes
Subject:
Aileron and Rudder Trim
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/23/1973
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Superseded AD: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Superseded By: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: 73-13-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1671

AD NUMBER:   73-13-06

SUBJECT HEADING:   Airworthiness Directives; Hawker Siddeley Model DH-114 "Heron" Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 23, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
73-13-06 HAWKER SIDDELEY: Amdt. 39-1671. Applies to Hawker Siddeley deHavilland Model DH-114 "Heron" Airplanes, having Modifications 496 installed.

Compliance is required as indicated.

To prevent possible inadvertent actuation of aileron and rudder trim in a direction other than that desired and to prevent possible interference by the aileron trim jack with the aileron when in its full down position, accomplish the following:

Prior to September 21, 1973, unless already accomplished, incorporate Hawker Siddeley Modifications Nos. 1006 and 1053, or FAA-approved equivalents.

This amendment becomes effective June 23, 1973.

FOOTER: