# STC SA4803NM

- 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 A-777](https://openairdocs.org/tcds/A-777)
- Certificate PDF: https://openairdocs.org/files/sha256/9b/f2/9bf2e2d2e93c05b99f4a71992b41ae29077226f6a1fd66c957359ce4ea1e727a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8B0B54A2B9C4E30285256CC2000E3EC3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4803NM

## ADs that name it (0)

None.

## Approved models (9)

- Raytheon Aircraft Company 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))

## What the certificate says

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

United States of America 4103 Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 571803NM This certificate issued to: ELT Engineering 14301 Flower Street Garden Grove, California 92643 Part 3 of the CiviI. Air Pegulation *see I.C.D.S. No. A-777 for complete certification basis Original Product - Type Certifioate Number: A~777 Make: Beech Model: 35, A35, B35, C35, D35, E35, F35, G35, 33R 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 confiquration will not introduce any adverse effect upon the airworthiness of the aircraft.

Date of Application: Apri1 24, 1989 Date Reissued: March 23, 1992, February 26, 1996 Date of Issuance: November 1, 1989 Date Amended:

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

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

## Every issue (1)

- February 26, 1996: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/9b/f2/9bf2e2d2e93c05b99f4a71992b41ae29077226f6a1fd66c957359ce4ea1e727a)

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