# STC SR00078DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Paravion Technology Inc, United States
- Description: Installation of a swivel mount assembly to mount a flat design video monitor.
- Applied: January 8, 1993
- Status date: January 25, 1994
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS 4H12](https://openairdocs.org/tcds/4H12)
- Certificate PDF: https://openairdocs.org/files/sha256/e1/b3/e1b34b97a420cf6b1acd5f18c1be5f56b33b12cf4b863d9a461095decd77a6f2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/25CFA222A382F56885256CC20062246A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00078DE

## ADs that name it (0)

None.

## Approved models (4)

- Schweizer Aircraft Corporation 269A ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269A-1 ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269B ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269C ([TCDS 4H12](https://openairdocs.org/tcds/4H12))

## 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: SR00078DE This certificate issued to: Paravion Technology, Inc.

Part 6 of the Civil Air Regulations.

Original Product - Type Certificate Number: 4H12 Make: Schweizer Model: 269A, A-1, B, C Description of Type Design Change:

Installation of a Swivel Mount Assembly to mount a flat design Video Monitor per Paravion Technology, Inc.

Drawing List No. DL-269MM110, Rev. A, dated January 10, 1994, FAA approved January 25, 1994 or later FAA approved revision.

1. This approval is for the Swivel Mount only. The Video Monitor installation must be FAA approved and meet the requirements specified in Drawing 269MM-110, Rev. A dated 1/10/94 or later FAA approved revision.

2. This approval should not be extended to rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

3. A copy of this Certificate must maintained as part of the permanent records of the modified rotorcraft.

Date of Application: January 8, 1993 Date Reissued:

Date of Issuance: January 25, 1994 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Toqur Ca. Caldinell ROGER A. CALDWELL (Signature) Acting Manager NO MINIST RATION Denver Aircraft Certification Field Office Northwest Mountain Region, Denver, Colorado (Title)

## Every issue (1)

- January 25, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e1/b3/e1b34b97a420cf6b1acd5f18c1be5f56b33b12cf4b863d9a461095decd77a6f2)

---
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.