STC SA00199SE

Supplemental type certificate · Muffler and Exhaust System

Holder
Muffler and Exhaust System · United States
Status
Current · Amended
Status date
October 19, 1995
Applied
January 5, 1995
Product
Aircraft · Single-Engine
Certification basis
Part 21

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Modification of Beech 35-950116and/or 35-950118 exhaust stack assemblies by adding a slip joint to the middle riser of each exhaust stack assembly.

What the certificate saysOCR

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: SA00199SE This certificate issued to: Muffler and Exhaust System Remanufacturing 9616 South Cedar Rd.

Spokane, WA 99204 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requivements of Part 3 of the Civil Air Regulations. (See Type Certification Data Sheet for the complete certification basis.

Original Product - Type Certificate Number: A-777 3A15 Make: Beech Beech Model: 35 thru G35, 35R 35-33, 35-A33 thru C33, E33, F33 Description of Type Design Change: Modification of Beech 35-950116, 35-950118, 33-95001-5, and 33- 95001-7, exhaust stack assemblies by adding a slip joint to the middle riser of each exhaust stack assembly per Muffler and Exhaust System Remanufacturing Drawing 106-5500, Revision 1, dated July 20, 1995, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. This modification must be inspected for indications of leaking or cracking at each annual inspection of the modified airplane. A copy of this Certificate shall be maintained as part of the permanent records for the modified airplane.

Date of Application: January 5, 1995 Date Reissued:

Date of Issuance: June 22, 1995 Date Amended: October 19, 1995 FEDERAL AVIATION By Direction of the Administrator (Signature) ADMINIST RA T103 Acting Manager, Seattle Aircraft Certification Office (Title)

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 · 14

MakeModelData sheet
Hawker Beechcraft Corporation35A-777
Hawker Beechcraft Corporation35-A333A15
Hawker Beechcraft Corporation35-B333A15
Hawker Beechcraft Corporation35-C333A15
Hawker Beechcraft Corporation35RA-777
Hawker Beechcraft CorporationA35A-777
Hawker Beechcraft CorporationB35A-777
Hawker Beechcraft CorporationC35A-777
Hawker Beechcraft CorporationD35A-777
Hawker Beechcraft CorporationE333A15
Hawker Beechcraft CorporationE35A-777
Hawker Beechcraft CorporationF333A15
Hawker Beechcraft CorporationF35A-777
Hawker Beechcraft CorporationG35A-777