# STC SA04352CH

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Win Win Aviation Inc, United States
- Description: Installation of Wind Deflector, Bench, External Assist Handle, Internal Assist Handle, Jump Exit Control Light, External Step and Wind Block in accordance with Win Win Aviation Parts List, WA-PARTS-208-2088-JM, revision Original, dated Janua,y 02, 2018 or later FM approved revision.
- Applied: January 5, 2018
- Status date: October 24, 2018
- Product: Aircraft
- Certification basis: Part 21
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/f0/eb/f0eb5c1fa30304fc7e4c2606e297de365d6d9a9fb08ae16016f71cf9c5ef5249
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0E06EBDD0778574D862587C800179D8F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA04352CH

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- Textron Aviation Inc. 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA04352CH This certificate issued to: Win Win Aviation, Inc.

3210 Pleasant Street DeKalb, IL 60115 Surt. 23 of the Federal Aviation Pegulaliens. (See Type Certificate Data Sheet No. A37CE for complete certification basis) Original Product - Type Certificate Number: A37CE Ababe : Textron Aviation Inc.

Model: 208;208B Description of Type Design Change:

Installation of Wind Deflector, Bench, External Assist Handle, Internal Assist Handle, Jump Exit Control Light, External Step and Wind Block in accordance with Win Win Aviation Parts List, WA-PARTS-208-208B-JM, revision Original, dated January 02, 2018 or later FAA approved revision.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

3. This modification does not install Title 14 CFR part 23 compliant seating and is therefore zero occupancy.

Date of Application: January January 2018 Date Reissued:

Date of Issuance: October 24, 2018 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Monica L. Nemecek TOMNISTRATO Manager, Airframe and Administrative Section Chicago ACO Branch (Title)

FAR FORM 8110-2 (10-66) PAGE 1 Of 3 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) Extent of Authority (if licensing agreement):.

Signature of grantor (In ink): -

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01352CH Date of Issuance: October 24, 2018 Limitations and Conditions: (Continued):

4. The Left and Right Hand Benches are compliant as monuments and are not certified to carry any items of mass. Testing performed during certification would be sufficient for gust loading of seven evenly distributed masses of 215 pounds each. This is to assist in Sport Parachute Operations in accordance Title 14 CFR part 91, §91.107(a)(3)(ii) as interpreted by Advisory Circular 105- 2E, Sport Parachuting, dated December 4, 2013.

- END -

FAA FORM 8110-2-1 (10-69) PAGE 3 Of 3 PAGES

## Every issue (1)

- October 24, 2018: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f0/eb/f0eb5c1fa30304fc7e4c2606e297de365d6d9a9fb08ae16016f71cf9c5ef5249)

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