What it approves
Modification of aircraft fuselage to add 20" belly hole for camera or other aerial applications
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 N umber SA00515DE This certificate, issued to Straight Flight, Inc.
13251 E Control Tower Rd, Box K-12 Englewood, Colorado 80112 Part 23* of the Federal Aviation Regulations.
*Certification basis is set forth in Type Certificate Data Sheet A4CE Original ProductType Certificate Number: A4CE Make: Cessna Model: T206H, 206H Description of the Type Design Change:
Modification of aircraft fuselage to add 20" belly hole for camera or other aerial applications in accordance with Straight Flight Master Drawing List 0001-2328, Revision A, dated 08/27/03, FAA approved September 9,2003.
Revision B, dated 10/29/2005, FAA approved January 27,2006, or later FAA approved revision defines option group consisting of: A - 20" Camera Hole Modification; B - Retractable Belly Door; C - Exhaust Extension; D- 28VDC Power Provisions; E - Operator Seat; F - Quick-Release Bench Seat Hardware.
1. Instructions for Continued Airworthiness, Straight Flight Report 2328-905. Revision A. dated August 27, 2003, or later FAA accepted revision is required for this installation.
2. FAA Approved Flight Manual Supplement, AFM Supplement to Cessna 206H/T206H Airplane Flight Manual, No. 2328-908 Revision A, dated September 9, 2003, or later FAA approved revision is required.
3. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.
4. 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.
5. STC No. SA01782LA is a required installation with the 130 Amp alternator for the 50 Amp power port.
Date of application: February 7, 2002 Date reissued: 01/27/2006, 04/18/2007 Date of issuance: June 20, 2003 Date amended: 09/09/2003, 01/27/2006, 07/03/2013 12/27/2013
Roger Caldwell (Signature) Northwest Mountain Regional Acting Manager Denver Aircraft Certification Office (Title)
ADs that name this STC · 0
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Approved models · 2
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| December 27, 2013 | Amended, current | Certificate |
| July 3, 2013 | Amended, earlier issue | Certificate |
| April 18, 2007 | Reissued, earlier issue | Certificate |
| January 27, 2006 | Reissued, earlier issue | Certificate |