# STC ST09022AC-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: L3Harris Technologies Integrated Systems L.P., United States
- Description: Installation of executive interior and various electrical equipment.
- Applied: April 20, 1993
- Status date: May 4, 2023
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM)
- Certificate PDF: https://openairdocs.org/files/sha256/53/16/531614edf8b0bf7975eeba3cce24900d9343e921951f1892e03be1af82940d54
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141539167120231012160901.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST09022AC-D

## ADs that name it (2)

- [AD 2002-26-14](https://openairdocs.org/ad/2002-26-14): In-flight entertainment (IFE) systems · Boeing 767-300 Series with STC ST01869AT-D. Effective Jan 28, 2003. Cited in the text
- [AD 2001-14-13](https://openairdocs.org/ad/2001-14-13): Airplane Operations Manuals--Passenger Entertainment System (PES) · Boeing 767-200 Series with STC ST09022AC or ST09022AC-D. Effective Aug 16, 2001. Named in the applicability

## Approved models (1)

- The Boeing Company 767-200 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Supplemental Type Certificate Number ST09022AC-D

This certificate issued to: L3Harris Technologies Integrated Systems L.P.

7500 Maehr Road Waco, TX 76705

Part 25 of the Federal Aviation Regulations.

Original Product Make: The Boeing Company Type Certificate Number: A1NM Model: 767-200 Series

Installation of executive interior and various electrical equipment in accordance with L -3 Communications Sealed Drawing List 93030119, Rev R, dated August 10, 2007 or later FAA approved revision and L-3 Airplane Flight Manual Supplement dated August 10, 2007 or later FAA approved revision.

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

Items of this STC not complying with the appropriate certification basis are described in Report 93030117- 000.

(Limitations and Conditions continued on page 3 of 3)

Date of Application: April 20, 1993 Date Reissued: April 30, 2002; April 3, 2007 May 4, 2023 Date of Issuance: January 31, 1995 Date Amended: August 10, 2007 By Direction of the Administrator

Signature

Title Loyd R. Hamilton ODA-750173-SW Administrator

Supplemental Type Certificate Number ST09022AC-D

To (Name and address of transferee)

From (Name and address of grantor)

Number: ST09022AC-D Amendment 1 Date of Re-Issuance: May 4, 2023

Limitations and Conditions: (Continued)

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) dated August 9, 2007 or later FAA approved revision have been accepted by FAA Aircraft Evaluation Group (AEG).

Certification Basis:

The certification basis used for this STC is 14CFR25 Amendments 1 through 37 except where superseded as defined in FAA Type Certification Data Sheet (TCDS) and as follows:

• 14CFR25.869 Fire Protection Amdt 113

• 14CFR25.981 Fuel Tank Ignition Prevention Amdt 102

--------------------------------------------------END-----------------------------------------------

## Every issue (2)

- May 4, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/53/16/531614edf8b0bf7975eeba3cce24900d9343e921951f1892e03be1af82940d54)
- April 3, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b3/cc/b3cca208d9f6b274cc20c8634e72351c8b3c26a354d0c8fc0aa3638a9e5b28e7)

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