STC SA04741NY

Supplemental type certificate · Raisbeck Engineering Inc.

Holder
Raisbeck Engineering Inc. · United States
Status
Current · Reissued
Status date
December 9, 2024
Applied
July 18, 2023
Product
Aircraft · Small Airplane
Certification basis
Part 23
Data sheet
TCDSA37CE

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

What it approves

Installation of a Soot Shield

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.

SA04741NY Raisbeck Engineering, Inc.

2811 South 102nd Street, Suite 100 Tukwila WA, 98168 Part 23 Title 14 Code of Federal Regulations A37CE Textron Aviation Inc.

208B Installation of a Soot Shield in accordance with (1) Master Data List 22R0149-00-02, Rev A, dated November 4, 2024, or later FAA approved revision. (2) Instructions for Continued Airworthiness (ICA) 22R0149-50-02, Rev C, dated August 8, 2024, or later FAA accepted revision. The ICA must be made available to the operator at the time of installation. The ICA and its contents must be incorporated into the operator's maintenance program. (3) Aircraft Flight Manual Supplements (AFMS) 22R0149-50-03, Rev IR, dated October 31, 2024, or later FAA approved revision. The AFMS must be carried in the aircraft during all flights.

(1) The installer must determine whether this design change is compatible with previously approved modifications.

(2) If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission.

(Limitations and Conditions Continued on Page 3 of 3) July 18, 2023 December 9, 2024 November 4, 2024

for Manager, West Certification Branch 3

SA04741NY 3

SA04741NY Date of Issuance: November 4, 2024

Limitations and Conditions (continued from Page 1 of 3):

(3) This STC is applicable to Textron Aviation Inc, Model 208B S/N 208B0001 through 208B2196 and 208B2198 through 208B4999 with PT6A-114A series engine, and 208B2197 and 208B5000 and on with PT6A-140 Series engine.

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for Textron Aviation Inc, Model 208B is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A37CE.

b. The certification basis for parts changed or affected by the change since the reference application date, July 18, 2023, is based upon 14 CFR § 23 as amended by Amendments 23-1 through 23-28 except for those above amendment 23-28, listed below.

Regulations at later amendment than 23-28:

14 CFR Part 23.1557(a) amdt 23-45; 23.1583(a)(b)(c)(d)(e)(f)(g)(h)(i)(j)(k)(l)(m)(n)(o)(p) amdt 23-62.

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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 · 1

MakeModelData sheet
Textron Aviation Inc.208BA37CE

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
December 9, 2024Reissued, currentCertificate
November 4, 2024Issued, earlier issueCertificate