# STC SA2630WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: BF Goodrich Aerospace, United States
- Description: Installation of Hoskins (Pulstar TM) combined Position Anti-Collision Lighting System in accordance with FAA Sealed Hoskins Top Drawings No. 10-202186 or No. 10-202186-1.  These Anti-Collision Lighting Systems have been found to meet the Anti-Collision Light Standards of FAR 23.1401, in effect of August 11, 1972.  Hoskins FAA Approved AFM supplement dated December 27, 1972 or later FAA Approved Revision is required with this modification
- Applied: September 25, 1972
- Status date: September 30, 2011
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS 5A6](https://openairdocs.org/tcds/5A6)
- Certificate PDF: https://openairdocs.org/files/sha256/03/be/03beba3238d9a512d5db8b1ae38904a60457bd9d1313b4278681b9c6563a9bf1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/29DD69DAA494F3A98625795800633759.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2630WE

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part 3 of the Civil Air Regulations.

(See T.C. Data Sheet 5A6)

Original Product--Type Certificate Number: 5A6

Cessna

Description of Type Design Change: Installation of Hoskins (Pulstar TM) combined Position Anti-Collision Lighting System in accordance with FAA Sealed Hoskins Top Drawings No. 10-202186 or No. 10-202186-

1. These Anti-Collision Lighting Systems have been found to meet the Anti-Collision Light Standards of FAR 23.1401, in effect of August 11, 1972. Hoskins FAA Approved AFM supplement dated December 27, 1972 or later FAA Approved Revision is required with this modification. .

Limitations and Conditions: The approval of this change in type design applies basically to this model only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should not include considerations of significant changes in weight distribution such as an increase in fixed disposal weight in the fuselage.

BF Goodrich Aerospace Lighting Systems Division 3445 South 5th Street Phoenix, AZ 85040 Make :

Date reissued : April 01, 1990, September 25, 1995, January 31, 1996, September 30, 2011

Date amended : January 22, 1973, May 03, 1973 May 11, 1973

( Signature) Melvin Taylor Manager, Atlanta Aircraft Certification Office

( Title)

Date of application : September 25, 1972

Date of issuance : December 27, 1972

## Every issue (1)

- September 30, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/03/be/03beba3238d9a512d5db8b1ae38904a60457bd9d1313b4278681b9c6563a9bf1)

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