STC SA9198SC-D

Supplemental type certificate · L-3 Communications Integrated Systems LP

Holder
L-3 Communications Integrated Systems LP · United States
Status
Current · Amended
Status date
March 22, 2013
Applied
October 15, 2003
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 25, Part 121, Part 129
Data sheet
TCDSA20WE

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

What it approves

Installation of (4) channels of High Speed Data (HSD) for Aircraft Earth Station (AES) 1&2

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.

Number SA9198SC-D This Certificate issued to L-3 Communications Integrated Systems, L.P.

10001 Jack Finney Blvd.

Greenville, TX 75402 Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number: A20WE *SEE PAGE 3 Make : Boeing Model : 747-2G4B Description of Type Design Change: Installation of (4) channels of High Speed Data (HSD) for Aircraft Earth Station (AES) 1&2 in accordance with (1) L-3 Communications Integrated Systems Sealed Drawing List SDL 6528-2, Revision B dated 15 April 2005; (2) “Instructions for Continued Airworthiness VC-25 HST Status Upgrade” G6528B.28.41A, Revision NC dated 18 April 2005; or later FAA approved revisions of (1) or (2).

Date of application: 15 October 2003 Date reissued :

Date of issuance : 06 November 2003 Date amended : 21 April 2005;

22 March 2013 – Amdt 2 By direction of the Administrator

(Signature) Michael E. Hopper ODA-750173-SW Administrator, Alternate

(Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee) (Address of transferee) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SA9198SC-D Amendment 2 Date of Issuance: 22 March 2013

Limitations and Conditions: (Continued)

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

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. Based on 14 CFR §§ 21.115 and 21.101, the certification basis for the Boeing 747-2G4B aircraft is as follows:

a. The type certification basis fo r Boeing 747-2G4B series airplanes is shown on TCDS A20WE for parts not changed or not affected by the change.

b. The certification basis for parts changed or aff ected by the change since the reference date of application, 15 October 2003, is as shown in TCDS A20WE with the exception that 25.981(a)(3) is at amendment 25-102 and 25.1529 is at amendment 54.

4. When installed, airplanes with this STC are limited to operations excluding those of an Air Carrier.

Specifically, no operations under 14 CFR 121, 14 CFR 129 or any foreign Air Carrier are permitted.

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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 · 1

MakeModelData sheet
The Boeing Company747-200B SeriesA20WE