STC SA02118AK

Supplemental type certificate · Hageland Aviation Services, Inc.

Holder
Hageland Aviation Services, Inc. · United States
Status
Current · Reissued
Status date
August 3, 2018
Applied
June 19, 1998
Product
Aircraft · Small Multi-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDSA20SO

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

What it approves

Installation of damage protection plates to the inboard, lower side of the flaps.

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.

Part 3 of the Civil Air Regulations.

Original Product – Type Certificate Number: A20S0 Make: Piper Aircraft, Inc.

Model: PA-31, PA-31-300, PA-31-325, PA-31-350

Installation of Damage Protection Plates to the inboard, lower side of the flaps in accordance with Frontier Flying Service, Inc., Data List DL98-01, dated June 19, 1998 or Later FAA approved revision.

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, then the holder shall give that person written evidence of such permission.

June 19, 1998 June 30, 1998 August 3, 2018

(Signature) August A. Asay Manager, Anchorage ACO Branch

(Title)

Hageland Aviation Services, Inc.

4700 Old International Airport Road Anchorage, AK 99502

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 · 4

MakeModelData sheet
The New Piper Aircraft Inc.PA-31A20SO
The New Piper Aircraft Inc.PA-31-300A20SO
The New Piper Aircraft Inc.PA-31-325A20SO
The New Piper Aircraft Inc.PA-31-350A20SO