STC SA01602SE

Historical

Supplemental type certificate · AeroMech Incorporated

Holder
AeroMech Incorporated · United States
Status
Historical · Amended
Status date
November 17, 2006
Applied
July 15, 2004
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDSA28CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed May 21, 2007.

What it approves

Group aircraft approval for Reduced Vertical Separation Minimum (RVSM).

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.

United States of America Department of Transportation _ Federal Aviation Administration Supplemental Type Certificate Number SA01602SE

This certificate, issued to: AeroMech Incorporated 1616 Hewitt Avenue, Suite 312 Everett, WA 98201

Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A28CE (Rev. 12) Make: Cessna Model: 441

Description of the Type Design Change: Group aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-CS-0422 Rev. “B," dated November 13, 2006, or latest FAA approved revision.

Limitations and Conditions: For Class 1 airframes, the Instructions for Initial and Continued Airworthiness, document AMI-IICA-CS-0438A, Rev. “A,” dated April 28, 2006, or latest FAA approved revision, is a required part of this STC.The Airplane Flight Manual Supplement (AFMS) for the Cessna Model 441, AeroMech Document AMI-AFMS-CS-0435A, Rev. “B,” FAA approved November 17, 2006, or latest FAA approved revision, is required on-board for operation of the Class 1 airframes.

For Class 2 airframes, the Instructions for Initial and Continued Airworthiness, document AMI-IICA-CS-0438B, Rev. “new,” dated November 13, 2006, or latest FAA approved revision, is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Cessna Model 441, AeroMech Document AMI-AFMS-CS-0435B, Rev. “new,” FAA approved November 17, 2006, or latest FAA approved revision, is required on-board for operation of the Class 2 airframes.

Descriptive data pertaining to this design change are considered inadequate for duplication on other products.

This approval is limited to Cessna Model 441aircraft only.

A copy of this certificate must be maintained as part of the permanent records of the aircraft. If the holder agrees to permit another person to use this certificate the holder shall give the other person written evidence of the permission.

Date of application: July 15, 2004 Date reissued:

Date of issuance: October 26, 2005 Date amended: May 4, 2006, November 17, 2006

This certificate may be transfe rred in accordance with FAR 21.47.

(Signature)

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 · 2

MakeModelData sheet
Cessna Aircraft Company441A28CE
The Cessna Aircraft Company441A28CE

Every issue · 2

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

DateStatusFiles
November 17, 2006Amended, earlier issueCertificate
May 4, 2006Amended, earlier issueCertificate