STC ST00260DE

FAA Form 8110-2 (5/14) Page 1 of 3

Number: ST00260DE

Fokker50Freighter STC Corporation 13394 East Control Tower Road Englewood, Colorado 80112 Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A-817 Make:

Fokker Services B.V.

F27 Mark 200 and Mark 050

Installation of Class E Cargo Interior, configuration 24E301-211, in accordance with Branson Aircraft Corporation Drawing List 24A300, revision B, dated November 5, 1996, FAA approved November 7, 1996 or later FAA approved revision. Also Configurations 24E301-901, -911 and -921 in accordance with FAA approved Fokker50Freighter STC Corporation Drawing list 24A300, revision F dated October 11, 2006, or later FAA approved revisions.

The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only.

(Continued on Page 3)

Date of Application: February 22, 1996 Date Reissued: December 22, 2004

Date of Issuance: November 7, 1996 Date Amended: January 28, 1998; December 07, 2006; July 21, 2009;

December 01, 2015; August 16, 2016

Signature Todd G. Dixon Title: Manager, Denver Aircraft Certification Office Northwest Mountain Region

FAA Form 8110-2 (5/14) Page 2 of 3

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00260DE Limitations and Conditions (Continued):

For the Mark 200 Configuration only:

• STC ST00354SE, installation of second main landing gear position indicating system, is required if gear down inspection light (24R304-021) is not installed.

• Maintenance Manual Supplement, MMS-231, dated November 7, 1996 or later revision is required. Cargo Loading Report, WB-2051, dated November 7, 1996 or later revision is required.

• A copy of the FAA Airplane Flight Manual Supplement, FMS-231, dated November 7, 1996, or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

For the Mark 050 Configuration only:

• Instructions for Continued Airworthiness, Maintenance Manual Supplement, MMS-232, Revision C, dated April 24, 2009, FAA accepted on May 1, 2009, or later FAA accepted revision is required.

• Cargo Loading Manual, WB-2052, revision D, dated January 16, 2009 or later revision is required.

• A copy of the FAA Airplane Flight Manual Supplement, FMS-232, revision B, dated February 20, 2009, or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

• Cargo Operating manual, COM-201, revision NC dated February 20, 2009, or later revision is required.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the design changes to Fokker Services B.V Model F27 Mark 050 is as follows:

• The type certification basis for Fokker Services B.V Model F27 Mark 050 airplanes is shown on TCDS A-817 for parts not changed or affected by the change.

• The certification basis for parts changed or affected by the change, is 14 CFR § 25 dated February 1, 1965 as amended by Amendment 25-1 through 25-112.

A copy of this STC 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.

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