STC ST04435AT

Supplemental type certificate · Chippewa Aerospace Inc

Holder
Chippewa Aerospace Inc · United States
Status
Current · Issued
Status date
October 31, 2018
Applied
September 18, 2017
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 25, Part 26

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

What it approves

Installation of Astronics Passenger In-Seat Power in the Embraer ERJ-170-100, ERJ-170-200, ERJ-190-100 and ERJ-190-200 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor t o alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

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

Number: ST04435AT This certificate issued to: Chippewa Aerospace, Inc.

490 Allied Dr.

Conway, SC 29526

Part 25of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A56NM, A57NM Make: Embraer Model: ERJ 170-100/200, ERJ 190-100/200 Series

Description of Type Design:

Installation of Astronics Passenger In-Seat Power in the Embraer ERJ-170-100, ERJ-170-200, ERJ-190- 100 and ERJ-190-200 Series Aircraft in accordance with Chippewa Aerospace Master Drawing List (MDL) No. 170-2454-01-0001, Rev. 1, Dated August 23, 2018, or later FAA approved revision.

Limitations and Conditions: FAA Approved Airplane Flight Manual Supplement (AFMS) for the Embraer ERJ-170 (ERJ 170-100), ERJ-175 (ERJ 170-200), ERJ-190 (ERJ 190-100), ERJ-195 (ERJ 190-200) Series Aircraft for the Installation of the Passenger In-Seat Power System in accordance with Chippewa Aerospace Airplane Flight Manual Supplement No. 170-2454-01-1012, Rev. IR, Dated October 31, 2018, or later FAA approved revision, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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. (Limitations and Conditions continued on page 3 of 3.)

Date of Application: September 18, 2017 Date Reissued:

Date of Issuance: October 31, 2018 Date Amended:

Signature Title (for) Christina Underwood Manager, Atlanta ACO Branch

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

Transfer the ownership of Supplemental Type Certificate Number: ST04435AT

To (Name and address of transferee)

From (Name and address of grantor)

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

Number: ST04435AT Instructions for Continued Airworthiness (ICA), Chippewa Aerospace Inc.

Document No. 170-2454-01-0002B, Rev. 1, Dated October 01, 2018, or later FAA approved revision, must be made available to the operator at the time of installation.

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 the Embraer ERJ-170-100, ERJ-170-200, ERJ-190-100 and ERJ-190-200 Series aircraft is as follows:

a. The type certification basis for Embraer ERJ-170-100, ERJ-170-200, ERJ-190-100 and ERJ-190-200 airplane is shown on TCDS A56NM AND A57NM for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, September 18, 2017, is based upon part 25 as amended by Amendment 25-143. 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 this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-143 §§ 25.23 §§ 25.301 §§ 25.303 §§ 25.305 §§ 25.307 §§ 25.365 §§ 25.561 §§ 25.562 §§ 25.601 §§ 25.603 §§ 25.605 §§ 25.609 §§ 25.613 §§ 25.625 §§ 25.785 §§ 25.789 §§ 25.791 §§ 25.803 §§ 25.813 §§ 25.815 §§ 25.853 §§ 25.869 §§ 25.899 §§ 25.1301 §§ 25.1307 §§ 25.1309 §§ 25.1316 §§ 25.1317 §§ 25.1353 §§ 25.1357 §§ 25.1431 §§ 25.1525 §§ 25.1529 §§ 25.1541 §§ 25.1581 §§ 25.1583 §§ 25.1585 §§ 25.1587

Regulations at the amendment level in TCDS A56NM AND A57NM §§ 25.571 §§ 25.611

14 CFR Part 26 Regulations Based on 14 CFR §21.101 (g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For a future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of issuance date of this STC, compliance has been found for the following regulations: 14 CFR § 26.11 and 14 CFR § 26.47.

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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 · 15

MakeModelData sheet
Embraer S.A.ERJ 170-100 LRA56NM
Embraer S.A.ERJ 170-100 SEA56NM
Embraer S.A.ERJ 170-100 STDA56NM
Embraer S.A.ERJ 170-100 SUA56NM
Embraer S.A.ERJ 170-200 LLA56NM
Embraer S.A.ERJ 170-200 LRA56NM
Embraer S.A.ERJ 170-200 STDA56NM
Embraer S.A.ERJ 170-200 SUA56NM
Embraer S.A.ERJ 190-100 ECJA57NM
Embraer S.A.ERJ 190-100 IGWA57NM
Embraer S.A.ERJ 190-100 LRA57NM
Embraer S.A.ERJ 190-100 STDA57NM
Embraer S.A.ERJ 190-200 IGWA57NM
Embraer S.A.ERJ 190-200 LRA57NM
Embraer S.A.ERJ 190-200 STDA57NM