STC ST00252WI-D

*Huitca Scates of Baserica Department of Transportation Federal Aviation Administration Supplemental Type Certificate Member This certificate issued to: Boeing Commercial Airplane Group, Wichita Division P.O. Box 7730 Wichita, Kansas 67277-7730 Certifies that the change in the type design for the following product with tho limitations and conditions thomfor as specified horeon meds the airworthiness requiremonts of Port 25 of the Federal Aviation Rogulations (See Type Certificate Data Sheet A2NM and Page 2 of 2 Continuation Sheet) Original Product _ Type Contificato Numbon: A2OWE Make: Boeing Model: 747-200B Series Description of Type Design Change: Conversion of a passonger Airplane to a Main Deck Side Cargo Door Dedicated Special Freighter as Defined by FAA Approved Boeing Document D800-10610-7, Revision New or Later FAA Approved Revision Limitations and Conditions: (See Page 2 of 2 Continuation Sheet)

1. Boeing Commercial Airplane Group, Wichita Division, Airplane Flight Manual Supplements, original or later FAA approved revisions, are required to support this modification of applicable airplanes as identified in Table I of FAA approved Bocing Document D800-10610-7, Revision New or later FAA approved revision.

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.

D1 (Signature) TOMINISTRAS Fred T. DeWinkler DAS-501296-CE Administrator (Tille )

FAA FoR 8110-2 (10-6B) Page 1 of 2

Baited States of Slucrica Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST00252WỊ-D Part 25 of the Federal Aviation Regulations: (Continued)

1. Voluntary Compliance has been shown with respect to the following Regulations:

25.783() • Amendment 25-72, effective August 20, 1990.

25.791 Amendment 25-72, effective August 20, 1990.

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

25,853(a)(b)(d)-(1) Amendment 25-59, effective November 26, 1984 (SN 23698).

25.855 Amendment 25-59, effective November 26, 1984 Amendment 25-59, effective November 26, 1984 Amendment 25-59, effective November 26, 1984 (SN 23698).

A finding of no acoustic change as a result of this modification and compliance with Stage 2 and 3 noise standard requirements of FAR 36 as amended by Amendment 36-20, effective September 11, 1992, was made by the FAA Wichita Aircraft Certification Office on October 6. 1995 (SINs 22304. 22442) and on March 27, 1998 (SNs 21833. 21832). A finding of no acoustic change as a result of this modification and compliance with Stage 2 and 3 noise standard requirements of FAR 36 as amended by Amendment 36-21, effective December 28. 1995, was made by the FAA Wichita Aircraft Certification Office on July 16, 1997 (SN 22579), September 17, 1998 (SNs 22447, 22446), November 30, 1998 (SN23698), and on May 9. 2000 (SN 23389).

Limitations and Conditions: (Continued) 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.

This approval is limited those airplanes listed in Table 1 of Boeing Document D800-10610-7, Revision new or later.

S. Jamco America galley per STC ST00240SE (SNs 22304, 22442) and STC ST00857SE (SN 23389) or Acronautical Engineers per STC SA23290SO (SNs 21833, 21832) has been installed on the upper deck using electrical, water and drain, and structural provisions of this STC.

6. Flight Structures upper deck crew rest bunks per FAA Field Approval (SNs 22447. 22446) has been installed using structural provisions of this STC The items that have not been approved by the FAA, but have been accepted by the JACB are listed in JAB Letters KU-KI-532 dated May 26.

1997 (SN 22579), and KU-K1-547 dated May 7, 1999 (SN 23698). These items have been installed using structural. electrical, and water provisions of this STC This STC approval is for the existing configuration as defined by the approved drawing list or Inter FAA approved minor change which has been reviewed and approved by the appropriate DAS-501296-CE (formly known as DAS2CE) staff member.

NOTE I.: This STC has been previously amended on the following dates:

January 25, 1996 C. October 22. 1997 July 14, 1998 G. May 11, 1999 I. February 8, 2000 B. July 31. 1997 D. Apol 30. 1998 F. February 3, 1999 H. May 24, 1999 END

PAA FORM 8110-2-1 (10-68) PAGE 2 OF 2 PAGES December 11, 2000 FAA AC 82-03578