AD 75-24-06

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AD Number:
75-24-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Hawker Siddeley Aviation Limited Hawker Siddeley DH-104 "Dove" Airplanes
Subject:
Main Spar Joint
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/28/1975
Make:
de Havilland Aircraft Co., Ltd., The
Model:
D.H. 104 Dove Series 1A | D.H. 104 Dove Series 2A | D.H. 104 Dove Series 5A | D.H. 104 Dove Series 5...Show more
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Superseded AD: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Superseded By: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: 75-24-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2427

AD NUMBER:   75-24-06

SUBJECT HEADING:   Airworthiness Directives; Hawker Siddeley Aviation Limited Hawker Siddeley DH-104 "Dove" Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 28, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-24-06 HAWKER SIDDELEY AVIATION LIMITED: Amendment 39-2427. Applies to Hawker Siddeley DH-104 "Dove" airplanes, Serial Numbers 04465 and below certificated in all categories, except those that incorporate "Dove" Modification 870.

Compliance is required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished.

To detect spanwise cracks in the upper and lower wing main spar joint, accomplish the following:

(a) Inspect the upper and lower wing main spar joints for cracks in accordance with the X-ray technique specified in Appendix I, Issue 2 as amended June 16, 1975, of Hawker Siddeley Technical News Sheet (T.N.S.) No. 134, Issue 5, dated March 17, 1975, or an FAA- approved equivalent.

(b) If, during the inspection required by paragraph (a) of this AD, a crack is found in a wing main spar joint, before further flight modify the joint in accordance with Appendix 2 of Hawker Siddeley Technical News Sheet (T.N.S.) No. 134, Issue 5, dated March 17, 1975, or an FAA-approved equivalent.

This supersedes AD 57-05-02 that was contained in Supplement 2 to Part 507 of the Regulation of the Administrator (22 FR 6046) and that was transferred to Section 39.13 of the Federal Aviation Regulations upon the adoption of Part 39 (29 FR 14403).

NOTE: Copies of X-rays or of the results of the equivalent inspections as required by paragraph (a) of this AD are requested to be transmitted to DOT/FAA, Chief, Aircraft Certification Staff, Africa, and Middle East Region, c/o American Embassy, APO New York, N.Y. 09667.

(Reporting approved by the Bureau of the Budget under B.O.B. No. 04-R0174).

This amendment becomes effective November 28, 1975.

FOOTER: