STC ST10396SC-D

FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES Number ST10396SC-D This certificate, issued to The Boeing Company, Wichita Division P. O. Box 7730 Wichita, Kansas 67277-7730

Part 25 of the Federal Aviation Regulations. (See Page 2 of 2 Continuation Sheet)

A20WE Original Product--Type Certificate Number:

Make : Boeing Model : 747-200B (E-4A, E-4B)

Description of Type Design Change: Installation of Phase II Global Air Traffic Management (GATM) System [Honeywell Communication Management System with Aircraft Communication Addressing and Reporting System, VHF Data Link System, Cockpit Thermal Printer, Selcal Decoder System, and Update the Flight Interphone System] in accordance with Boeing Master Data List D226-38759-1, Revision G, dated April 22, 2005, and Boeing Document D3-8857, Section V, Appendix 102, Revision HH; or later FAA approved revisions. Airplane Flight Manual Supplement D226-38931-1, dated April 21, 2005, or later FAA approved revision, is required.

Limitations and Conditions: (See Page 2 of 2 Continuation Sheet)

1. This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the airplane.

Date of application : June 18, 2001

Date of issuance : August 23, 2005 Date reissued : April 17, 2006

Date amended : April 17, 2006

(Signature on File)

( Signature)

JR Brownell

DAS-501296-CE Administrator (Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

Number ST10396SC-D

Part 25 of the Federal Aviation Regulations: (Continued)

1. As defined in Type Certificate Data Sheet No. A20WE, Revision 35, starting on Page 11.

2. Voluntary compliance has been found relative to the following regulations:

a. Amendment 25-23, effective May 8, 1970 [25.301(a)(b)(c); 25.303; 25.471; 25.607; 25.611]

b. Amendment 25-41, effective September 1, 1977 [25.1309(a)(b)(c)(d)(e)(g); 25.1321(e)]

c. Amendment 25-42, effective March 1, 1978 [25.1353(a)(b)]

d. Amendment 25-46, effective December 1, 1978 [25.603; 25.605; 25.777(a)(b)(c); 25.789(a)]

e. Amendment 25-51, effective March 6, 1980 [25.787(a)(b)]

f. Amendment 25-54, effective September 11, 1988 [25.365(a)(d)(e)(g); 25.571(a)(c); 25.1529]

g. Amendment 25-59, effective November 26, 1984 [25.853(a)(b)]

h. Amendment 25-72, effective August 20, 1990 [25.21(a)(d); 25.29; 25.307(a); 25.613(a)(b)(c)(d)(f);

25.625; 25.869(a); 25.1351(a); 25.1381(a)(b); 25.1581(a)(b)(d)]

i. Amendment 25-80, effective May 1, 1994 [25.1316]

j. Amendment 25-86, effective March 6, 1996 [25.305(a)(b)]

k. Amendment 25-91, effective July 29, 1997 [25.561(a)(b3)(c)(d)]

l. Amendment 25-102, effective June 6, 2001 [25.981]

m. Amendment 25-105, effective July 26, 2001 [25.1583(c1)(c2); 25.1585(a)]

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. Other military modifications may have been installed on the aircraft which are not part of this Supplemental Type Certificate. These installations do not conform to FAA Approved type design, but may have been accepted by the military Airworthiness Authority for operation by the United States Department of Defense.

These installations are shown on FAA Form 8130-2, Conformity Certificate – Military Aircraft, dated April 26, 2005 or later. All non-conformances to FAA approved type design must be removed, or FAA approved, prior to returning the aircraft to civil registration with a standard airworthiness certificate.

4. This approval is limited to Boeing Models 747-E4A (Serial Numbers 20682, 20683, and 20684) and 747- E4B(Serial Number 20949).

5. Prior installations are required of the following Supplemental Type Certificates:

a. STC ST00529WI-D, INMARSAT

b. STC ST09661SC, FMS; EFIS; GPS

c. STC ST09504SC, VHF Com Upgrade

d. STC ST09662SC, TCAS; TA/VSI; IFF Mode S

e. STC ST09663SC, TAWS

6. This STC approval is for the existing configurati on as defined by the approved drawing list and later FAA approved minor change which have been reviewed and approved by the appropriate DAS-501296-CE staff members.

7. Installation of this STC modification must be acco mplished at the Boeing Wichita Repair Station PI2R084L utilizing Boeing Planning Paper as Installation Instructions. FAA approved changes to this STC may be installed at locations other than Boeing Wichita Repair Station if the changes are prepared in the form of kit engineering and include adequate installation instructions.

April 17, 2006