# STC SH1414NM

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Wesscam Camera systems, United States
- Description: Installation of "Wesscam" Camera Control Console in place of left front seat, Servotec AGL-8098 camera mount outriggers, left and right, Canadian Westinghouse "Wesscam" gyro stabilized HC32 or 33 camera assembly contained within a plastic sphere, and associated hardware
- Applied: October 22, 1981
- Status date: January 13, 1982
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1IN](https://openairdocs.org/tcds/H1IN)
- Certificate PDF: https://openairdocs.org/files/sha256/56/a6/56a697dee3a38a74d1628f58d1c9c026a36494c3c527e0ba4c958b8d34b11abd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A20F535EDAF2474086257A150068D8B2.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH1414NM

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter France SA.315B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))

## 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: SH1 4140M This certificate issued to: Wesscam Camera Systems 717 Hampshire San Francisco, CA Part 10 of the CIVi1 AiT Regulations.

Original Product -TypeCertificate Number: HIIN Make: Aerospatiale Model: SA315B " Camera Control Console and right; Canadian Westinghouse "Wesscam" gyro stabilized HC32 or 33 camera assembly contained within a plastic sphere, and associated hardware in accordance with Servotec Report No. AGL-TR-269.

Limitations and Conditions: Approval of this change in type design applies to the above model helicopter only. This approval should not be extended to helicopters of this model on which other previously approved modifications are incorporated unless it is determined that the relationship 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 helicopter. A copy of this Certificate, Addendum and Rotorcraft Flight Manual Supplement shall be maintained as part of the permanent records for the modified aircraft. (See Addendum Page 3, attached) This certificate and the supporting data which is the basis for approval shall remain in effect until sur rendered, suspended, revoked, or a termination date is therwise established by the Administrator of the Federal Aviation Administration Date of Application: October 22, 1981 Date Reissued:

Date of Issuance: January 13, 1982 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Scanacu (Signature ) TOMINIST RATO Chief, Seattle Area Aircraft Certification Office, ANM-100S (Title)

## Every issue (1)

- January 13, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/56/a6/56a697dee3a38a74d1628f58d1c9c026a36494c3c527e0ba4c958b8d34b11abd)

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