# STC ST00118SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Panasonic Avionics Corporation, United States
- Description: Installation of Matsushita Avionics System 2000 (audio/visual).
- Applied: January 21, 1994
- Status date: June 5, 2006
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM)
- Certificate PDF: https://openairdocs.org/files/sha256/ab/9c/ab9c9bf85221ddd90221c769424227525926454aa12369c728dc7727071c452b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DF6495CD8F1A5AC2862579AD006ACB0E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00118SE

## 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 2001-14-04](https://openairdocs.org/ad/2001-14-04): Airplane Flight Manuals--In-Flight Entertainment (IFE) System · Boeing 767-300 Series with STC ST00118SE. Effective Aug 17, 2001. Named in the applicability

## Approved models (1)

- The Boeing Company 767-300 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate NumberST00118SE This certificate issued to: Panasonic Avionics Corporation 22333 29th Drive SE Bothell, WA 98021 Certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirement's of Part 25 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A1NM Make: Boeing Model: 767-300 Description of Type Design Change: Installation of Matsushita Avionics Systems (MAS) Co. System 2000 (Audio/Visual) in accordance to Master Drawing List DL 10065, Revision B, dated July 21, 1994, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. Any installations of this STC, amendments to this STC, or installation of this STC in conjunction with another STC installation involving MAS Systems 2000 components, shall insure that the maximum current draw on any Area Distribution Box does not exceed 10.5 Amps RMS. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

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.

Date of Application: January 21, 1994 Date Reissued: June 5, 2006 Date of Issuance: August 21, 1994 Date Amended: June 5, 2006

FEDERAL AVIATION (Signature)

TOMINIST RATIOD Acting Manager, Seattle Aircraft Certification Office (Title)

**FAA FORM S110-2(10-65)**

## Every issue (1)

- June 5, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ab/9c/ab9c9bf85221ddd90221c769424227525926454aa12369c728dc7727071c452b)

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