What it approves
Installation of full turning contoured engine exhaust stacks on Pratt & Whitney Canada PT6A-38, PT6A-41, or PT6A-42 engines
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.
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Original Product 7\SH&HUWLILFDWH1XPEHU Make:
SA8986SW Metrea Special Aerospace, ISR Inc.
1100 N. Broadway Ave, Suite 200 Oklahoma City, OK 73103 Part 23 Federal Aviation Regulations A24CE Textron Aviation (Beechcraft) A100-1, 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T Installation of full turning contoured engine exhaust stacks on Pratt & Whitney Canada PT6A-38, PT6A-41, or PT6A-42 engines. Data required:
1. STC Engineering Co., Drawing List No. DL93005, Rev. 3, dated July 1, 1994, or later FAA Approved revision.
1. Limited to Pratt & Whitney Canada PT6A-38, PT6A-41, or PT6A-42 engines.
2. Compatibility of this design change with previously approved modifications must be determined by the installer.
May 25, 1993 March 7, 1995, March 10, 2008, April 29, 2025 November 14, 1994 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 2
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Too (Name and address of transferee):
Date oI transfer:
SA8986SW 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 25
| Make | Model | Data sheet |
|---|---|---|
| Textron Aviation Inc. | 200 | A24CE |
| Textron Aviation Inc. | 200C | A24CE |
| Textron Aviation Inc. | 200CT | A24CE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 29, 2025 | Amended, current | Certificate |
| July 10, 2013 | Amended, earlier issue | Certificate |