STC SA485SW

Supplemental type certificate · Todd and Jo Peterson

Holder
Todd and Jo Peterson · United States
Status
Current · Reissued
Status date
July 3, 2001
Applied
January 19, 1965
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A13

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

What it approves

For 182H, 182J, 182K, 182L and 182M include (1) Full span double slotted flaps; (2) Drooped wing leading edge; (3) Aileron actuated drag plates; (4) Nose control surface; (5) Elevator down spring alteration; (6) Relocated pitot head. For 182N, 182P, and 182Q include nose control surface only.

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 is a scan without a text layerOpen the PDF to read it.

ADs that name this STC · 1

An AD can apply because an STC is installed, or mention one in its text.

Approved models · 8

MakeModelData sheet
The Cessna Aircraft Company182H3A13
The Cessna Aircraft Company182J3A13
The Cessna Aircraft Company182K3A13
The Cessna Aircraft Company182L3A13
The Cessna Aircraft Company182M3A13
The Cessna Aircraft Company182N3A13
The Cessna Aircraft Company182P3A13
The Cessna Aircraft Company182Q3A13