STC SA00412WI

Supplemental type certificate · Air Plains Services Corporation

Holder
Air Plains Services Corporation · United States
Status
Current · Reissued
Status date
September 22, 2005
Applied
April 12, 1995
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS3A24

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

What it approves

Installation of McCauley D3A34C401/90DFA -2, -4, -6, -8, -10 propeller with Teledyne Continental motors IO-550-D engines already installed, and associated changes.

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.

This certificate issued to: Air Plains Services Corporation Wellington Airport P. O. Box 541 Wellington, KS 67152

Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number : 3A24 Make : Cessna Model : 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F

Installation of McCauley D3A34C401/90DFA -2, -4, -6, -8, and -10 propeller on aircraft with Teledyne Continental Motors IO-550-D engines already previously approved and installed. Data Required: C S Industries Installation Instructions No. 401A, Rev. – , dated March 15, 1996, or later “FAA Approved” revisions.

The McCauley Propeller Model D3A34C401/90DFA-( ) should be installed on those Cessna Models with TCM IO-550-D engines installed. For the Models listed above, the installation of D3A34C401/90DFA-( ) propeller is limited to not over 88 inches and not under 80 inches diameter for land, float and amphibian planes. Placard is required to indicate the operating restrictions for continuous operation.

Date of application : April 12, 1995 Date of issuance : March 15, 1996 Date reissued : September 22, 2005

Date amended : March 09, 1998

Original signed by Dan Withers

(Signature) Dan Withers Program Manager Wichita Aircraft Certification Office (Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA00412WI

Date of Issuance: March 15, 1996 Date Amended: March 09, 1998 Date Reissued: September 22, 2005

The Operating Restrictions Placard should state: “Avoid Continuous Operation between the following RPM and manifold pressures at the stated diameters”:

Propeller Model Diameter Range (inches) RPM Inches MP C401/90DFA -2 88 to 86 1900 to 2100 26 and above C401/90DFA -4 86 to 84 1900 to 2100 26 and above C401/90DFA -6, -8, -10 84 to 80 No Placard required.

or later “FAA Approved” revision of any of these documents.

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

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.

--END--

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 · 8

MakeModelData sheet
The Cessna Aircraft Company1853A24
The Cessna Aircraft Company185A3A24
The Cessna Aircraft Company185B3A24
The Cessna Aircraft Company185C3A24
The Cessna Aircraft Company185D3A24
The Cessna Aircraft Company185E3A24
The Cessna Aircraft CompanyA185E3A24
The Cessna Aircraft CompanyA185F3A24