# STC SA399CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: BF Goodrich Aerospace, United States
- Description: Installation of Hoskins Supplemental Position Light  System which includes Model B (Dual) Wing Tip Light, Model C, D, or K Tail Light with or without Model 2 Fuselage Lights.
- Applied: September 19, 1962
- Status date: September 30, 2011
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-807](https://openairdocs.org/tcds/A-807)
- Certificate PDF: https://openairdocs.org/files/sha256/99/74/99741aa3d9eb75b98177fab4f4dff000fd38e1241779cc3ad47e6d557b2a262e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/07358C2F71BA392B86257958006337E5.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA399CE

## ADs that name it (0)

None.

## Approved models (10)

- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 1A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 2A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 5A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 5BA ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 6A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 6BA ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 7A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 7AXC ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 8A ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 8AXC ([TCDS A-807](https://openairdocs.org/tcds/A-807))

## 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 10 of the Civil Air Regulations.

Description of Type Design Change: Installation of Hoskins Supplemental Position Light System which includes Model B (Dual) Wing Tip Light, Model C, D, or K Tail Light with or without Model 2 Fuselage Lights.

Data Required: (1) General installation instructions as amended February 18, 1996 Hoskins Specification Sheets, 6 pages Dated February 18, 1966. (2) Hoskins drawings DH-104, Sheets 1 and 2: 30-0028 Sheets 1 & 2; 22-1-B or 30-0108; 30-0021 or 30-0022, Specifications Sheet P/N 65-0035-1 dated June 03, 1968.

Limitations and Conditions: LIMITATION OF APPLICABILITY. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of the airplane.

BF Goodrich Aerospace Lighting Systems Division 3445 South 5th Street Phoenix, AZ 85040 A-807 DeHavilland Make :

104 Model :

Date reissued : October 17, 1974, April 1, 1990, September 25, 1995, January 31, 1996, September 30, 2011

Date amended : June 26, 1968

( Signature) Melvin D. Taylor Manager, Atlanta Aircraft Certification Office

( Title) Date of application : September 19, 1962

Date of issuance : February 18, 1966

## Every issue (1)

- September 30, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/99/74/99741aa3d9eb75b98177fab4f4dff000fd38e1241779cc3ad47e6d557b2a262e)

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