STC SA01982WI

Supplemental type certificate · BLR Aerospace LLC.

Holder
BLR Aerospace LLC. · United States
Status
Current · Reissued
Status date
March 28, 2023
Applied
April 29, 2021
Product
Aircraft · Small Airplane
Certification basis
Part 23
Data sheet
TCDSA24CE

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

What it approves

Removal of the Ground Idle Solenoid on the Textron Aviation Inc. Model B200C serial numbers BL-73 thru BL-123 that had a Ground Idle Solenoid installed

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.

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Original Product 7\SH&HUWLILFDWH1XPEHU Make:

SA01982WI BLR Aerospace LLC 11002 29th Ave W Everett, WA 98204 23 the Code of Federal Regulations A24CE Textron Aviation Inc.

B200C Removal of the Ground Idle Solenoid on the Textron Aviation Inc. model B200C.

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

2) Limited to serial numbers BL-73 thru BL-123 that had a Ground Idle Solenoid installed in accordance with “Master Data List,” document number 3S21-001-1001, Revision 1.0, dated January 24, 2022, or later FAA approved revision.

April 29, 2021 February 22, 2022, March 28, 2023 January 25, 2022 Steven K Simpson ODA Administrator ODA-833355-CE 3

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Too (Name and address of transferee):

Date oI transfer:

SA01982WI 3

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3) The following STC is required to be installed as prerequisites:

a) STC SA03209NY - Installation of Model MTV-27-1-E-C_F_R(P)/CFR225-55f full feathering and reversing 5-bladed propellers.

4) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

5) Approval of this type design change applies to the aircraft model shown on this STC.

6) A copy of this certificate shall be maintained as part of the permanent records for the modified aircraft.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and the FAA policy for significant changes in FAA order 8110.48A, the certification basis for the applicable 14 CFR Part 23 aircraft is as follows:

a. As specified on the applicable Type Certificate Data Sheet (TCDS) of the aircraft for parts not changed or not affected by this STC.

b. Regulations at the amendment levels defined within the below table for parts changed or affected by the STC since the reference date of STC application.

Regulations at the amendment level in TCDS A24CE:

23.29(b) [Amdt. 23-0], 23.601 [Amdt. 23-0], 23.609 [Amdt. 23-0],

23.901(a)(2) [Amdt. 23-7], 23.905(b) [Amdt. 23-0], 23.907(b) [Amdt. 23-0],

23.1141(e) [Amdt. 23-7], 23.1351(b)(1)(i) [Amdt. 23-7], 23.1351(b)(1)(ii) [Amdt. 23-7].

Regulations with amendment level exceptions defined in TCDS A24CE:

23.1301(a) [Amdt. 23-20], 23.1301(d) [Amdt. 23-20], 23.1309(a)(1)(i) [Amdt. 23-49],

23.1309(a)(3) [Amdt. 23-49], 23.1309(b)(2)(3)(4) [Amdt. 23-49].

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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.B200CA24CE

Every issue · 2

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

DateStatusFiles
March 28, 2023Reissued, currentCertificate
February 22, 2022Reissued, earlier issueCertificate