STC SA04364AT

Supplemental type certificate · JAARS Inc.

Holder
JAARS Inc. · United States
Status
Current · Issued
Status date
May 8, 2017
Applied
November 7, 2016
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDS7A15

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

What it approves

Introduction of alternative cargo tie down fittings for Pilatus PC-6 series aircraft

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.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SA04364AT

This certificate issued to: JAARS 7601 Radin Rd.

Waxhaw, NC 28173

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: 7A15 Make: Pilatus

Model: PC-6

Introduction of alternative cargo tie down fittings for Pilatus PC-6 series aircraft in accordance with JAARS Master Drawing List PC-6 001-20, Revision G, dated March 15, 2017, or later FAA- approved revisions.

1. For installation and inspection, apply JAARS Inc. Instructions for Continued Airworthiness PC-6 01-20-AW, Issue C, dated 18-APR-2017, or later FAA- approved revisions.

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

Date of Application: November 7, 2016 Date Reissued:

Date of Issuance: May 8, 2017 Date Amended:

Signature

Title Christina Underwood, Manager Atlanta Aircraft Certification Office

FAA Form 8110-2 (5/14) Page 2 of 3

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA04364AT

FAA Form 8110-2 (5/14) Page 3 of 3

Date of Issuance: May 8, 2017 Date Amended:

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, for the Pilatus PC-6, the Certification Basis is as follows:

 The type certification basis for the Pilatus PC-6 aircraft is shown on TCDS 7A15 for parts not changed or not affected by the change.

 The certification basis for parts changed or affected by the change since the reference date of application, November 7, 2016, is based upon part 23 as amended by amendment 23-62. Based on 14 CFR §§ 21.115 and 21.101, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 23-0 through 23-62

23.301 Amdt 23-48, 23.303 Amdt 23-0, 23.305 Amdt 23-45, 23.307 Amdt 23-0, 23.561 (a)(b)(c) Amdt 23-62, 23.601 Amdt

23.23, 23.603 Amdt 23-23, 23.605 Amdt 23-23, 23.607 Amdt 23-48, 23.609 Amdt 23-0, 23.611 Amdt 23-48, 23.613 Amdt 23-45, 23.625 Amdt 23-7, 23.1529 Amdt 23-26, 23.1581 Amdt 23-50, 23.1585 Amdt 23-62

Regulations at an intermediate amendment None

Regulations at the amendment level in TCDS 7A15 None

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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 · 1

MakeModelData sheet
Pilatus Aircraft LimitedPC-67A15