# STC SA494NE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Maple Leaf Aviation Ltd, Canada
- Description: Installation of nose gear strut fairing with Maple Leaf Aviation drawing numbers AD-182-1001, AD-182, AD-177-1002, all dated 3/22/84 and installation instruction amended 9/3/86. Eligible on aircraft equipped with 500 X 5 nose wheel and tire, and Cessna's standard nose wheel fairing only. Eligible on aircraft with fixed landing gear only.
- Applied: September 18, 1986
- Status date: May 9, 2001
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/56/fe/56fe89dad6f54e12d073c925c159868dd945905686c6761340ad337ed7af5072
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/129B00AAFF44D4A585256CC2000E3FE2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA494NE

## ADs that name it (0)

None.

## Approved models (1)

- The Cessna Aircraft Company 182 Series ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

PO Box 160 Brandon, Manitoba R7A 5YB Canada

Part 3 of the Civil Air Regulations.

Original Product -- Type Certificate Number : 3A13 Make : Cessna Aircraft Company

Model : 182 Series, 182S and 182T

Installation of nose gear strut fairing in accordance with Maple Leaf Aviation, Ltd. drawing numbers AD-182-1001, AD-182, AD-177-1002, all dated March 22, 1984 and Installation Instruction amended September 3, 1986.

1. Eligible on aircraft equipped with 500 X 5 nose wheel and tire, and Cessna’s standard nose wheel fairing only.

2. Eligible on aircraft with fixed landing gear only.

3. 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.

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

Date of application : September 18, 1986

Date of issuance : December 1, 1986 Date reissued :

Date amended : May 9, 2001

( Signature) Vito A. Pulera Manager New York Aircraft Certification Office

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

## Every issue (1)

- May 9, 2001: Amended, Current. [certificate](https://openairdocs.org/files/sha256/56/fe/56fe89dad6f54e12d073c925c159868dd945905686c6761340ad337ed7af5072)

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