# STC SA00834SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Micro AeroDynamics Inc, United States
- Description: Installation of vortex generators on wings and tail surfaces.
- Applied: June 8, 2000
- Status date: August 11, 2000
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS A42EU](https://openairdocs.org/tcds/A42EU), [TCDS A18EU](https://openairdocs.org/tcds/A18EU), [TCDS 3A17](https://openairdocs.org/tcds/3A17)
- Certificate PDF: https://openairdocs.org/files/sha256/af/67/af671e92ce0670e005ff835af2b174a8cc899a315d88e5e43eea7012de2f4051
- Approved model list and other attachments: [AML SA00834SE.pdf](https://openairdocs.org/files/sha256/67/91/679189d26848bc0a39b33bd786dcfa6a4c6c34abd7d17d28bf5eb1e7a24c6286)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1631E648629344B885256CC1007E0174.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00834SE

## ADs that name it (0)

None.

## Approved models (33)

- Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182S ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company F182P ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Cessna Aircraft Company F182Q ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Cessna Aircraft Company FR172E ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR172F ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR172G ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR172H ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR172J ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR172K ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR182 ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Cessna Aircraft Company R172E ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172F ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172G ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172H ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172J ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R172K ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company T182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SA00834SE This certificate, issued to Micro AeroDynamics, Inc.

4000 Airport Road, Suite D Anacortes, WA 98221 Part * of the * Regulations.

Original ProductType Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA00834SE for a list of approved airplane Model: models and applicable airworthiness regulations.

Description of the Type Design Change: Installation of vortex generators on the wings and tail surfaces in accordance with the provisions of AML SA00834SE.

NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.

Limitations and Conditions: Approval of this change in type design applies to the aircraft listed on AML SA00834SE only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. NOTE: Compatibility of this modification with R/STOL Systems Supplemental Type Certificate SA1382WE has been demonstrated by flight testing. A copy of this Certificate and AML must be maintained as part of the permanent records for the modified 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.

Date of application: June 8, 2000 Date reissued:

Date of issuance: August 11, 2000 Date amended:

(Signature)

__ Acting Manager, Seattle AircraftCertification Office (Title)

### AML SA00834SE.pdf

**FAA APPROVED MODEL LIST NO. SA00834SE FOR**

INSTALLATION OF VORTEX GENERATORS ISSUED AUGUST 11, 2000 1 of 3

**ITEM AIRCRAFT MODEL**

**AIRCRAFT MAKE TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION BASIS FOR**

**ALTERATION**

**FAA SEALED**

DRAWING LIST _______________

**NUMBER REV**

**INSTALLATION**

**INSTRUCTIONS,**

**REVISION AND DATE AML**

**REVISION DATE**

1. R172E (USAF T-41B, C, & D) CESSNA 3A17 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

2. R172F (USAF T-41D) CESSNA 3A17 CAR 3 MA2138 REV A 5/12/00 IR MA2148, Rev IR 7/27/00

IR

3. R172G (USAF T-41C or D) CESSNA 3A17 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

4. R172H (USAF T41D) CESSNA 3A17 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

5. R172J CESSNA 3A17 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

6. R172K CESSNA 3A17 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

7. FR172E CESSNA A18EU FAR 21.29 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

8. FR172F CESSNA A18EU FAR 21.29 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

9. FR172G CESSNA A18EU FAR 21.29 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

10. FR172H CESSNA A18EU FAR 21.29 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

11. FR172J CESSNA A18EU FAR 21.29 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

12. FR172K CESSNA A18EU FAR 21.29 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

13. 182C CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

**FAA APPROVED MODEL LIST NO. SA00834SE FOR**

INSTALLATION OF VORTEX GENERATORS ISSUED AUGUST 11, 2000 2 of 3

**ITEM AIRCRAFT MODEL**

**AIRCRAFT MAKE TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION BASIS FOR**

**ALTERATION**

**FAA SEALED**

DRAWING LIST _______________

**NUMBER REV**

**INSTALLATION**

**INSTRUCTIONS,**

**REVISION AND DATE AML**

**REVISION DATE**

14. 182D CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

15. 182E CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

16. 182F CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

17. 182G CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

18. 182H CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

19. 182J CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

20. 182K CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

21. 182L CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

22. 182M CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

23. 182N CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

24. 182P CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

25. 182Q CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

26. R182 CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

27. TR182 CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

**FAA APPROVED MODEL LIST NO. SA00834SE FOR**

INSTALLATION OF VORTEX GENERATORS ISSUED AUGUST 11, 2000 3 of 3

**ITEM AIRCRAFT MODEL**

**AIRCRAFT MAKE TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION BASIS FOR**

**ALTERATION**

**FAA SEALED**

DRAWING LIST _______________

**NUMBER REV**

**INSTALLATION**

**INSTRUCTIONS,**

**REVISION AND DATE AML**

**REVISION DATE**

28. 182R CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

29. T182 CESSNA 3A13 CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

30. 182S CESSNA 3A13 FAR 23 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

31. F182P CESSNA A42EU CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

32. F182Q CESSNA A42EU CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

33. FR182 CESSNA A42EU CAR 3 MA2138 REV A 5/12/00 MA2148, Rev IR 7/27/00 IR

Approved ___________________________________ Acting Manager, Seattle Aircraft C e r t i f i c a t i o n O f f i c e

## Every issue (1)

- August 11, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/af/67/af671e92ce0670e005ff835af2b174a8cc899a315d88e5e43eea7012de2f4051), [AML SA00834SE.pdf](https://openairdocs.org/files/sha256/67/91/679189d26848bc0a39b33bd786dcfa6a4c6c34abd7d17d28bf5eb1e7a24c6286)

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