STC SA2543WE

Supplemental type certificate · BF Goodrich Aerospace

Holder
BF Goodrich Aerospace · United States
Status
Current · Reissued
Status date
September 30, 2011
Applied
February 23, 1972
Product
Aircraft · Small Multi-Engine
Certification basis
Part 3, Part 21, Part 23
Data sheet
TCDS3A16

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

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.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 7

MakeModelData sheet
Hawker Beechcraft Corporation583A16
Hawker Beechcraft Corporation95-553A16
Hawker Beechcraft Corporation95-A553A16
Hawker Beechcraft Corporation95-B553A16
Hawker Beechcraft Corporation95-C553A16
Hawker Beechcraft CorporationD553A16
Hawker Beechcraft CorporationE553A16