# STC SA3170NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bruce Aerospace Inc., United States
- Description: Installation of Floor Proximity Emergency Escape Path Marking System
- Applied: June 12, 2008
- Status date: June 12, 2008
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A5EU](https://openairdocs.org/tcds/A5EU)
- Certificate PDF: https://openairdocs.org/files/sha256/64/52/6452b2439d07fd940c2ebc0a765f9bce381991790d1259badb13bbccb872c41b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/298C056608DDC581862574710077B668.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3170NM

## ADs that name it (0)

None.

## Approved models (2)

- British Aerospace Airbus Limited BAC 1-11 200 Series ([TCDS A5EU](https://openairdocs.org/tcds/A5EU))
- British Aerospace Airbus Limited BAC 1-11 400 Series ([TCDS A5EU](https://openairdocs.org/tcds/A5EU))

## 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: SA3170NM This certificate issued to: Bruce Aerospace Inc.

101 Evans Ave.

Dayton, NV 89403 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of Part 4b* of the Civil Abir Foegulations.

*Certification basis is set forth in Type Certificate Data Sheet ASEU. In addition, compliance has been demonstrated with Federal Aviation Regulations, Part 25, FAR 25.812(e), Amendment 25-58.

Original Product Type Certificate Number ASEV Make: British Aerospace Model: BAC 1-11, 200 Series, 400 Series Description of Type Design Change: Installation of Floor Proximity Emergency Escape Path Marking System in accordance with FAA approved Bruce Industries, Inc. Master Drawing List MDL-111, Revision D, dated May 30, 1986 or later FAA approved revisions.

Limitations and Conditions: This system should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. This system has been determined to comply with the applicable airworthiness requirements with the following operative light assemblies: exit identifiers and/or flood lights - 2 bulbs operative, light track red modules - 50% operative (1 bulb in each 2 bulb group or 2 bulbs in each 4 bulb group), and light track clear and/or directional arrow modules - 50% operative with a maximum of 2 bulbs in a row out. 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.

suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration Date of Application: January 20, 1986 Date Reissued: June 12, 2008 Date of Issuance: June 9, 1986 Date Amended:

FEDERAL AVIATION Ae Jodministrator (Signature) Mausour Rafat TOMINSTRATO Manager, Cabin Safety/Mechanical and Environmental System Branch Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- June 12, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/64/52/6452b2439d07fd940c2ebc0a765f9bce381991790d1259badb13bbccb872c41b)

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