STC ST04574AT

Supplemental type certificate · Avionics Support Group Inc.

Holder
Avionics Support Group Inc. · United States
Status
Current · Issued
Status date
November 20, 2023
Applied
March 4, 2022
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDST00021SE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of the Avionics Support Group Constant Friction Mount (cfMount) and Cradle

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.

Title: (for) Christina M. Underwood Manager, East Certificate Branch Compliance and Airworthiness Division Aircraft Certification Service ST04574AT Avionics Support Group, Inc.

13155 SW 132 Avenue Miami, FL 33186 25 the Federal Aviation Regulations T00021SE The Boeing Company 787-8, 787-9 & 787-10 Series Installation of the Avionics Support Group Constant Friction Mount (cfMount) and Cradle in accordance with Master Data List (MDL) 219274-MDL, Rev IR, dated March 14, 2022, or later FAA approved revision.

(See Continuation Sheet 3 of 4) March 4, 2022 November 20, 2023 4

ST04574AT 4

ST04574AT Limitations and Conditions - cont.:

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

2. 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.

3. Instructions for Continued Airworthiness (ICA) document 219274-ICA Rev IR, dated March 14, 2022 or later FAA Approved revision must be made available to the operator at the time of installation.

ST04574AT 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 Boeing 787-8/-9/-10 series aircraft is as follows:

a. The type certification basis for Boeing 787-8/-9/-10 airplane is shown on TCDS T00021SE 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, March 4, 2022, 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 § 25.29 § 25.301 § 25.303 § 25.305 § 25.307 § 25.561 § 25.601 § 25.603 § 25.605 § 25.609 § 25.611 § 25.613 § 25.773 § 25.789 § 25.853 § 25.1301 § 25.1309 § 25.1529 § 25.1541

Regulations at an intermediate amendment None

Regulations at the amendment level in TCDS T00021SE None

--------------------------END--------------------------- 4 4

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 · 3

MakeModelData sheet
The Boeing Company787-10T00021SE
The Boeing Company787-8T00021SE
The Boeing Company787-9T00021SE