What it approves
Installation of Pilot and Copilot Main Windshield
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: SA04182AT
This certificate issued to: PPG Aerospace 1719 Highway 72 East Huntsville, AL 35811
Part 23 of Title 14 of the Federal Aviation Regulations.
Installation of Pilot and Copilot Main Windshield into eligible aircraft in accordance with PPG Aerospace Master Data List (MDL) documents as specified in the FAA Approved Model List (AML) SA04182AT Original Issue dated November 17, 2014, or later FAA approved revision. Instructions for Continued Airworthiness (ICA), PPG Aerospace PPG-2032-ICA Initial Release dated October 13, 2014, or later FAA approved revision, must be made available to the operator at the time of installation.
This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any other approved modifications will produce no adverse effect upon the airworthiness of that aircraft.
Continued on Page 3
Date of Application: January 31, 2014 Date Reissued:
Date of Issuance: November 17, 2014 Date Amended:
Signature
Title: Manager, Atlanta Aircraft Certification Office See attached Approved Model List (AML) SA04182AT Original Issue dated November 17, 2014, or later FAA approved revision
FAA Form 8110-2 (5/14) Page 2 of 3
Transfer the ownership of Supplemental Type Certificate Number: SA04182AT
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: ST04182AT Date of Issuance: November 17, 2014
FAA Form 8110-2 (5/14) Page 3 of 3
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101 and the FAA policy for significant changes in FAA Order 8110.48, the Certification Basis for each eligible model specified in the FAA Approved Model List (AML) SA04182 Original Issue dated November 17, 2014, or later FAA approved revision, is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown in the Type Certificate Data Sheet (TCDS) listed in the AML separately for each model.
b. The certification basis for parts changed or affected by the change since the reference date of application, January 31, 2014, is based upon part 23 as amended by amendment 23-62 and is determined to be:
- Regulations at the latest amendment: as listed in the AML separately for each model
- Regulations at the certification basis shown in the cited TCDS: as listed in the AML separately for each model
- Regulations at an intermediate basis: as listed in the AML separately for each model
--------------------------END---------------------------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 13
| Make | Model | Data sheet |
|---|---|---|
| M7 Aerospace LLC | SA226-AT | A5SW |
| M7 Aerospace LLC | SA226-T | A5SW |
| M7 Aerospace LLC | SA226-T(B) | A5SW |
| M7 Aerospace LLC | SA226-TC | A8SW |
| M7 Aerospace LLC | SA227-AC (C-26A) | A8SW |
| M7 Aerospace LLC | SA227-AT | A5SW |
| M7 Aerospace LLC | SA227-BC (C-26A) | A8SW |
| M7 Aerospace LLC | SA227-CC | A18SW |
| M7 Aerospace LLC | SA227-DC (C-26B) | A18SW |
| M7 Aerospace LLC | SA227-PC | A8SW |
| M7 Aerospace LLC | SA227-TT | A5SW |
| M7 Aerospace LLC | SA26-AT | A5SW |
| M7 Aerospace LLC | SA26-T | A5SW |
Every issue · 1
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| November 17, 2014 | Issued, current | CertificateApproved model list |