STC SA2119CE-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA2119CE-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 Type Certificate Data Sheet A20WE and Page 3 of 3 Continuation Sheet) Original Product --Type Certificate Number: A20WE Make: Boeing Model: 747-2G4B Description of Type Design Change:

Installation of an executive interior with support accommodations in accordance with Boeing Drawing Installation list shown in Boeing Document D3-8857, Section V, Appendix 27, Revision CJ or later FAA approved revision, which includes the Following:

1. Executive interior and related support systems 7. Addition of two lower lobe doors and airstairs

2. Mission Communication System (MCS) 8. Internal stairways from main deck to lower lobes

3. Secondary electrical power system 9. Additional avionics consisting of audio, navigation and

4. Self Defense System communication systems

5. Environmental control system for passenger areas and MCS 10. Replace Legacy Intercommunication System (ICS) with Digital ICS

6. Aerial Refueling System Limitations and Conditions: (See Page 2 of 3 Continuation Sheets)

1. This approval shall 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 aircraft.

Date of Application: February 20, 1987 Date Reissued:

Date of Issuance: August 15, 1990 Date Amended: July 11, 2007 (See Note 1 on Page 3 of 3 Continuation Sheet) FEDERAL AVIATION By Direction of the Administrator (Signature) TOMINSTRATO DAS-501296-CE Administrator David J. Horn (Title)

FAA Роки 8110-2 (10-68) PAGE 1 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA2119CE-D Limitations and Conditions: (Continued)

2. This modification requires FAA approved Boeing Commercial Airplane Group, Wichita Division, Airplane Flight Manual Supplement dated August 15, 1990 (S/N 23824) and December 10, 1990 (S/N 23825) or later FAA approved revision; DDS-33747.2G4-174.01 dated June 22, 2007 (SN's 23824, 23825) or later FAA approved revision.

3. This modification installs several features which are nonconformities to type design and have been accepted by the customer for mission requirements. These features are shown on FAA Forn 8130-2, Conformity Certificate - Military Aircraft, dated August 15, 1990 (S/N 23824) and December 17, 1990 (S/N 23825) or later dated forins and are for public use aircraft only. All nonconformities must be corrected prior to returning the aircraft to a standard airworthiness category.

Installation of HF3 and HF4 radio equipment using the provisions provided by this Supplemental Type Certificate is not approved.

5. Removal of deactivation components as shown on FAA Form 8130-2 dated August 15, 1990 (S/N 23824) and December 17, 1990 (S/N 23825) (Items 3 and 4 on both aircraft) which activates the aerial refueling system for operational use is not approved.

6. For carriage of passengers, two additional flight attendants are required during take-off and landing to occupy passenger seats designated as IPSS1 and IPSS9 as shown in Boeing Document D6-35692, Revision A or later FAA approved revision.

7. For carriage of passengers, one additional crew member is required who is trained to fight inflight fires in the lower lobe cargo compartments. This crew member may be one of the crew members specified in Number 6 above.

8. Equivalent safety findings exist with respect to regulation 25.1447(c).

9. This approval is limited to the airplanes listed on Page 3 of 3 of the Continuation Sheets.

10. This STC approval is for configuration as defined by the approved drawing list or later FAA approved minor changes.

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA2119CE-D Part 25 of the Federal Aviation Regulations: (Continued)

1. Equivalent safety finding with respect to FAR 25.1447(c); Reference FAA Wichita Aircraft Certification Office Letter to Boeing dated July 25, 1990.

2. Compliance has been shown with FAR part 36 through Amendment 36-17 (S/N 23824) and through Amendment 36-18 (S/N 23825) for Stage 3 noise level requirements.

3. Voluntary compliance has been shown with respect to the following Regulations:

14 CFR Amendment Original Post part Level STC STC

25.783(j) Amendment 25-54 effective October 14, 1980

25.812 (all except [h]) Amendment 25-58, effective November 26, 1984

25.853 Amendment 25-59, effective November 26, 1984 X

25.301; 25.303; 25.305(a)(b)(c); Amendment 25-23, effective April 8, 1970

25.471; 25.561; 25.607; 25.611,

25.773(a); 25.1321

25.787; 25.1359(đ) 25.1501(b) Amendment 25-32, effective May 1, 1972 Amendment 25-42, effective March 1, 1978 xxxxxx

25.603; 25.605; 25.789(a) Amendment 25-46, effective October 30, 1978

25.307(a)(c)(d) Amendment 25-54 effective October 14, 1980

25.853(a)(b) Amendment 25-59, effective November 26, 1984

25.29; 25.613(a)(b)(c)(d); Amendment 25-72, effective July 20, 1990

25.625(a)(b)(c); 25.869(a4);

25.1581(a2)(đ)

25.365(a)(b)(d)(e) (g) 25.1316(a)(b)(c4)(c5)(cб)(c7) Amendment 25-80, effective May 31, 1994 Amendment 25-87, effective June 5, 1996 xxxxx

25.981(a3) Amendment 25-102, effective June 6, 2001

25.1583(c1)(c2); 25.1585(a)(b) Amendment 25-105, effective June 26, 2001 25,856(a) Amendment 25-111, effective September 2, 2003 LIST OF APPLICABLE AIRPLANES Aircraft Variable Aircraft Model Aircraft Serial Number Tabulation Number 747-2G4B 23824 RD 166 747-2G4B 23825 RD167 NOTE 1: This STC has been previously amended on the following dates:

A. December 17, 1990 B. August 24, 1996 C. April 24, 2005 END July 11, 2007

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