# STC SA998WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Evans & Bailey Holdings LLC, United States
- Description: Installation of glass fiber reinforced plastic wing tips. (35R S/N D25R1 ONLY)
- Applied: June 15, 1965
- Status date: February 23, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS 5A4](https://openairdocs.org/tcds/5A4), [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/cb/e3/cbe3c2e4f650653e3c75a3aff4e08722d0dd84de5655d2fa8563dee30e9e2d41
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9B2CCD10F952E558862580D00060DC07.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA998WE

## ADs that name it (0)

None.

## Approved models (26)

- Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation B50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation C50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation D50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation D50A ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation D50B ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation E50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation F50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation G50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Textron Aviation Inc. 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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.

This Certificate issued to Evans & Bailey Holdings LLC 709 Airport Road Burlington, WI 53105 Part 3 of the Civil Air Regulations Original Product Type Certificate Number Make :

A-777, 3A15, 5A4 Beech B50, C50, D50, D50A, D50B, E50, F50, G50, 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, R35 (S/N D25R1 only), S35, 35-33, and 35-A33 Description of Type Design Change: Installation of glass fiber reinforced wing tips per FAA Sealed Met-Co-Aire Drawing number 11052, Revision N/C, dated June 9, 1965, and Installation Instruction SD 1024, Revision N/C, dated June 9, 1965, or later FAA approved drawings/instruction.

Limitations and Conditions: This approval of this change in type design applies basically to noted Models only. This approval should not be extended to other specific airplanes of these models on which other previous modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect on the airworthiness of that 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 15, 1965

Date of issuance : June 15, 1965

Date reissued : September 20, 1995;

February 23, 2017

Date amended : June 13, 1969; July 30, 1993

(Signature) Manager, Technical and Administrative Support Staff, ANM-103L (Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number (STC No.)

## Every issue (1)

- February 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/cb/e3/cbe3c2e4f650653e3c75a3aff4e08722d0dd84de5655d2fa8563dee30e9e2d41)

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