What it approves
Conversion of Teledyne Continental Motors (TCM) models IO-520-B, -BB to RAM model IO-550-B-RA engine, or conversion of TCM models IO-520-C, -CB to RAM model IO-550-C-RA engine
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.
United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project Number ST8603SC-E JEP
FAA Form 8110-2(10-68) Page 1 of 3 Number SE10746SC This Certificate issued to RAM Aircraft, Limited Partnership 7505 Karl May Drive Waco, TX 76708
Part 33 of the Federal Aviation Regulations.
Original Product Type Certificate Number : E5CE Make : Teledyne Continental Motors Model : IO-520-B, -BB, -C, or -CB
Description of Type Design Change: Conversion of Teledyne Continental Motors (TCM) models IO-520-B, -BB to RAM model IO-550-B-RA engine, or conversion of TCM models IO-520-C, -CB to RAM model IO-550-C-RA engine in accordance with RAM Master Drawing List 2691, Revision I.R. dated November 7, 2006, or later FAA approved revision.
Limitations and Conditions: The RAM model IO-550-B-RA engine is identical to and has the same ratings, limitations, and installation interfaces as TCM model IO-550-B engine. The RAM model IO-550-C-RA is identical to and has the same ratings, limitations, and installation interfaces as TCM model IO-550-C engine. The Instructions for Continued Airworthiness are contained in RAM Document number 2692, dated November 7, 2006, or later FAA approved revision.
Date of application : November 07, 2006
Date of issuance : November 20, 2007 Date reissued :
( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 3
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SE10746SC Date of Issuance: November 20, 2007
This approval should not be extended to other engines of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the inter-relationship between this change and any other previously approved modifications will produce no adverse affect on the airworthiness of that engine or aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
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