AD 67-30-04

AD Final Rules - DRS_67-30-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-30-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; HAWKER SIDDELEY Model DH-125 Series 1A and 1A-522 Airplanes
Subject:
Engine Mount Beam Failure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/11/1967
Make:
Textron Aviation Inc.
Model:
DH.125 Series 1A | DH.125 Series 1A-522
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Superseded AD: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Superseded By: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: 67-30-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-511

AD NUMBER:   67-30-04

SUBJECT HEADING:   Airworthiness Directives; HAWKER SIDDELEY Model DH-125 Series 1A and 1A-522 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 11, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-30-04 HAWKER SIDDELEY: Amdt. 39-511 Part 39 Federal Register November 10, 1967. Applies to Model DH-125 Series 1A and 1A-522 Airplanes, Serial Numbers 25013 through 25104.

Compliance required within the next 500 hours' time in service after the effective date of this AD, unless already accomplished.

To preclude the possibility of engine mount beam failure, modify the engine mount beam by removing the foam filler, reinforcing the lower flanges at the outboard ends with bar inserts and installing aluminum guard plates, in accordance with Hawker Siddeley Service Bulletin 53- 22-(1723). Revisions 1, dated April 10, 1967, or later ARB-approved revision or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region.

This amendment effective December 11, 1967.

FOOTER: