# STC SA2543WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: BF Goodrich Aerospace, United States
- Description: Installation of Hoskins Model 700801Anti-Collision Light in accordance with FAA sealed Master Eligibility List No. SA2543WE.  While the requirements of FAR 23.1401(a), (c), (d), (e) and (f) are met by this installation, the requirements of FAR 23.1401(b) are not met.  Since the aircraft was type certificated under airworthiness regulations that contained no Anti-Collision Light Standards for intensity and field of coverage, this installation is accepted.  Hoskins FAA approved AFM Supplement (see MEL SA2543WE) is required with this modification.
- Applied: February 23, 1972
- Status date: September 30, 2011
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/02/f3/02f37d3b988c68be3fd06df5e5b09aefa0728e8436454d00fd7167baf4277760
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3166A5A96FE75F968625793E0062B9CF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2543WE

## ADs that name it (0)

None.

## Approved models (7)

- Hawker Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

## 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 3A16)

Original Product--Type Certificate Number: 3A16

Beech

See Master Eligibility List No. SA2543WE

Description of Type Design Change: Installation of Hoskins Model 700801Anti-Collision Light in accordance with FAA sealed Master Eligibility List No. SA2543WE. While the requirements of FAR 23.1401(a), (c),

(d), (e) and (f) are met by this installation, the requirements of FAR 23.1401(b) are not met. Since the aircraft was type certificated under airworthiness regulations that contained no Anti-Collision Light Standards for intensity and field of coverage, this installation is accepted. Hoskins FAA approved AFM Supplement (see MEL SA2543WE) is required with this modification.

Limitations and Conditions: The approval of this change in type design applied basically to Beech Models listed on MEL SA2543WE only. This approval should not be extended to other aircraft of these models on which previously approved modifications are incorporated unless it is determined by installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the airplanes. 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 : December 19, 1972 November 13, 1971

( Signature) Melvin Taylor Manager, Atlanta Aircraft Certification Office

( Title) Date of application : February 23, 1972

Date of issuance : June 05, 1972

## Every issue (1)

- September 30, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/02/f3/02f37d3b988c68be3fd06df5e5b09aefa0728e8436454d00fd7167baf4277760)

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