What it approves
Modification of DeHavilland piston P/N 2200-25/2.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
This Certificate issued to MOTH AIRCRAFT COMPANY 21807 SOUTH EMBASSY AVENUE LONG BEACH, CA 90810-1738 Part 21* of the Federal Aviation Regulations. *Certification Basis is set forth in Type Certificate Data Sheet A44EU Original Product Type Certificate Number :
A44EU
DeHavilland
DH.CL Chipmunk 21, 22, 22A Description of Type Design Change: This approval authorizes the modification of the DeHavilland Aircraft Co. LTD piston, Part No. 2200- 25/2 in accordance with FAA Approved Moth Aircraft Co. Drawing No. 216, Revision N/C, dated 3/3/75, or l ater FAA approved revisions. This modification is applicable to the Bristol Siddeley (DeHavilland) or (Rolls -Royce) (1971) Gipsy Major Engine Model 10MK2.
Limitations and Conditions: NOTE: This STC specifies the DeHavilland Model DH.CL Chipmunk 21, 22, 22A aircraft since the propeller and Gipsy Major Engine were certificated as part of the aircraft. Ref. FAA Letter ANE -140 to ANM -179W dated 11/7/84. This approval should not be extended to other aircraft of this model on which other previously approve d modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any previously approved modifications will not introduce any adverse effect upon the airworthiness of that aircraft.
This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date of application: April 13, 1984
Date of issuance: December 27, 1985
Date reissued: June 16, 2015
(Signature)
Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)
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Number (STC No.)
ADs that name this STC · 0
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