STC SA01390WI

Supplemental type certificate · McCauley Propeller Systems

Holder
McCauley Propeller Systems · United States
Status
Current · Amended
Status date
March 21, 2008
Applied
October 3, 2005
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA00003SE

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

What it approves

Installation of McCauley Propeller Model D3A34C444/78MLA-0 and E-7819 spinner.

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.

FAA FORM 8110-2(10-69) Sheet 1 of 2 Number SA01390WI This certificate issued to: McCauley Propeller Systems 7751 E. Pawnee Wichita, KS 67207

FAR 23 of the Regulations.

Original Product Type Certificate Number: A00003SE

Make: Cessna Aircraft Company (formerly Columbia Aircraft Manufacturing) (formerly the Lancair Company)

Model: LC40-550FG, LC42-550FG

Installation of McCauley Propeller Model D3A34C444/78MLA-0 and E-7819 spinner. Installation of this STC is approved by the Wichita Aircraft Certification Office in coordination with the Seattle Aircraft Certification Office, as an Alternative Method of Compliance (AMOC) to Airworthiness Directive (AD) 2005-02-01.

Required Data:

1. A copy of this certificate.

2. Installation Instructions, Technical Report No. 969, Rev. (-), dated April 17, 2006 or later FAA approved revision.

3. FAA Approved Airplane Flight Manual Supplement, Technical Report No. 970, Rev. (IR), dated May 25, 2006 or later FAA approved revision.

4. Maintenance Manual Supplement–Instructions for Continued Airworthiness, Technical Report No. 975, Rev. (A), dated May 4, 2006 or later FAA approved revision.

1. The Limitations and Conditions are as defined on this certificate and in the Required Data.

2. Later FAA Approved revisions to the above data may be incorporated without further revision to this certificate.

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

4. If the STC 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 change in type design applies to the above model airplanes only.

6. A copy of the Required Data shall be maintained in the airplane permanent records and included in the operator’s Aircraft Maintenance Manual and the operator’s Aircraft Scheduled Maintenance Program.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: October 3, 2005

Date of issuance: June 2, 2006 Date reissued:

Date amended: March 21, 2008

Original Signed by Robert D. Adamson

( Signature) Robert D. Adamson FAA Program Manager Wichita Aircraft Certification Office

( Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor ( In ink):

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 · 2

MakeModelData sheet
Cessna Aircraft CompanyLC40-550FGA00003SE
Cessna Aircraft CompanyLC42-550FGA00003SE

Every issue · 2

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

DateStatusFiles
March 21, 2008Amended, currentCertificate
June 2, 2006Issued, earlier issueCertificate