STC SA2229CE

Supplemental type certificate · Northwest Propeller Services Inc.

Holder
Northwest Propeller Services Inc. · United States
Status
Current · Reissued
Status date
January 12, 2007
Applied
October 17, 1986
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS5A6

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

What it approves

Installation of McCauley 2A34C203/90DCA-2 or 2A34C203/90DCA-8 propeller. (THRU S/N 18052770)

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.

Number SA2229CE

This certificate, issued to Northwest Propeller Service Inc.

16709 Meridian Street E Unit #3 Pu yallup, WA 98375

Part 3 of the Civil Air Regulations.

Original Product⎯Type Certificate Number: 5A6 Make: Cessna Model: 180, 180A, B, C, D, E, F, G, H, and J through S/N 1805 2770

Description of the Type Design Change: Installation of McCauley 2A34C201/90DA-2 or 2A34C201/90DCA-8 or 2A34C203/90DCA-2 or 2A34C203/90DCA-8 propeller. Installation of C2A34C204/90DCB-2 or C2A34C204/90DCB-8 propeller. Data required: (1) CS Industries Installation Instructions No. 710 dated September 9, 1995, or later “FAA Approved” revision; and (2) a copy of this Certificate.

Limitations and Conditions: For the Model 180 equipped with the TCM 0-470-A engine: Installation to engine Serial Numbers 41000 and up. Engines with Serial Number below 41000 which incorporate one 5th and one 6th order crankshaft damper per TCM bulletin M89-24 are also approved. The 2A34C201/90DA-2, 2A34C203/90DCA-2 and C2A34C204/90DCB-2 propellers are for float, amphibian or land plane use. The 2A34C201/90DA-8, 2A34C203/90DCA-8 and C2A34C204/90DCB-8 propellers are for land plane use only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined 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. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

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.

Date of application: October 17, 1986 Date reissued: 3/4/96; 9/22/05; 1/12/07 Date of issuance: February 17, 1987 Date amended: 7/23/91; 1/11/93; 11/9/95; 1/12/07

Original signed by Mike Pasion (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 · 10

MakeModelData sheet
The Cessna Aircraft Company1805A6
The Cessna Aircraft Company180A5A6
The Cessna Aircraft Company180B5A6
The Cessna Aircraft Company180C5A6
The Cessna Aircraft Company180D5A6
The Cessna Aircraft Company180E5A6
The Cessna Aircraft Company180F5A6
The Cessna Aircraft Company180G5A6
The Cessna Aircraft Company180H5A6
The Cessna Aircraft Company180J5A6

Every issue · 2

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

DateStatusFiles
January 12, 2007Reissued, currentCertificate
September 22, 2005Reissued, earlier issueCertificate