# STC SA4804NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: ELT Engineering, United States
- Description: Installation of replacement storm window hinges and locking device.
- Applied: April 24, 1989
- Status date: February 26, 1996
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/3b/fd/3bfdfd05443125ea671f21083424ceb81d3ec08ea15b30aca3d5aa585ea92a07
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CC0576A66BF173BD85256CC2000E3EC4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4804NM

## ADs that name it (0)

None.

## Approved models (27)

- Hawker Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation E33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation G36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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: SA4804NM This certificate issued to: ELT Engineering 14301 Flower Street Garden Grove, California 92643 Certifies that the change in the type design for the following produd with the limitations and conditions therefor as speaified hereon meets the airworthiness requirement's of Part 3 of the civil Aix Poegulalions *see I.C.D.S. No. 3A15 for complete certification bas1s Original Product - Type Certificate Number: ЗА15 Make: Beech Model: see Continuation Sheet No. SA4804NM, page 3 Description of Type Design Change: Installation of replacement storm window hinges and locking device in accordance with FAA sealed E.L.T. Plastic Mold Installation Instructions Report 8965, dated 09/19/89 or later FAA approved revision.

Limitations and Conditions: This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

Date of Application: Apr11 24, 1989 Date Reissued: March 23, 1992, February 26, 1996 Date ofirmance: November 1, 1989 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) TOMINISTRATO Manager, Technical & Administrative Support Staff, ANM-1031 (Title)

FAA Form 8110-2-1(10-68) Page 1 of 3

Snitco Diates Di America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SAA804NM (I) November 1, 1989 (R) March 23, 1992 (R) February 26, 1996 Original Product - MODEL H35, J35, K35, M35, N35, ₽35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-833, 35-С33, 35-СЗЗА, Е33, ЕЗЗА, ЕЗ3С, Е33, F3ЗА, F3ЗС, G33, 36, А36, АЗ6TС,

- END -

FAA Form 8110-1(10-69) Page 3 of 3

## Every issue (1)

- February 26, 1996: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3b/fd/3bfdfd05443125ea671f21083424ceb81d3ec08ea15b30aca3d5aa585ea92a07)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.