STC SA816SW

Supplemental type certificate · Peterson Aircraft Repair

Holder
Peterson Aircraft Repair · United States
Status
Current · Reissued
Status date
September 16, 1977
Applied
September 6, 1967
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS5A6

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

What it approves

Installation of Hartzell BHC-A2VF-3/V8833 reversible pitch propeller.

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.

linted States of amtrica Bepartment of 'Transportation -jfetol atiiation administration Supplemental 'Cgpe Certificate SA816SW Peteraon Aircraft Repair 5104 Rector Fort Worth, Texas 76133 'W^^^^x24^^A-.<^^*^^ <^foMs/>*w(™^.</n^^/><e<jpu*4^nj!v^ 3 j>#j&e, Civil Air 5A6 Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H ^-taA^np*; Installation of a Hartzell BHC-A2VF-3/V8833 reversible pitch propeller in accordance with Wren Aircraft Corporation Drawing 200-100"E" dated 3/12/68, and MASA Drawing No. 9000 dated 4/16/73.

!•• Wren Beta MMWuil Ho. 2 dated 7/17/67 i» required for amphibian or seaplane. 2. Aircraft must be placarded: BETA CONTROL. Use inaccordance with Operator's Manual. Lock for Take-Off. 3* Wren Beta ManualNo. 6 dated 1/29/68 is required for Land Plane, Standard or Cross Wind Gear.4. Aircraft with 0-470-A, or 0-470- J engines HartBell BHC-A2VF-3/V8833 PropellerDia. Limits 88" - 86"; with 0-470-K, or 0-470- L engines Dia. limits 88" only.No additional reduction for repairs allowed. Not eligible on aircraft with 0-470-R engine.

September 6, 1967 ^^^^ 3/20/70; 5/11/72; 5/14/73;

3lW4Tl/10/75i 2/28/75; 9/16/77 J«ly 21, 1967 c* , // Revision 7~ * ""* »^»»» ^/'Mit'Mrn&ndea' • Don P. Watson (Slgmture) Chief, Engineering and Manufacturing Branch

FAAFORM 81 10-2 (10-68)

tinted States of America Btpartmcnt of ^Transportation -federal aoiation administration Supplemental t:gpe Certificate(Continuation &heet) jVum^ SA8163( K4Vlalon 7 Limitations and Conditions!

A. Aircraft must be placarded! BETA CONTROL. Use in accordance with Operator's Manual. Lock for Take-Off.

B. Aircraft with 0-470-A, or 0-A70-J engines Hartzell BHC-A2VF-3/V8833 propeller dia. limits 88" - 86"} with 0-470-K, or 0-470-L engines dia. limits 88" only* Ho additional reduction for repairs allowed.

Eligible on aircraft with 0-470-R engine with 84 - 80" dia. only.

C, For installation per Wren data Wren Beta Manual No. 2 dated 7/16/67 is required for amphibian or seaplane. Wren Beta Manual No. 6 dated 1/29/68 is required for Land Plane, Standard, or Cross Wind Gear.

D. For installation per Aero Accessories, Inc. data AeroSTOL Company Operator's Manual dated July 24, 1975, is required.

FAA FORM 8110-2-1 (1O-69) This certificate may bt transferred in accordance with FAR 21.47.

PAGE OF PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, Stair, and .£//> code) from (Name of grantor) (Print or type) (Address of grantor) {Number and street] ( C.ilr, Slnle. and ~JT code) Extent of Authority (if licensing agreement): __ Date of Transfer:.

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 · 9

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