STC SA01054LA

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01054LA This certificate issued to: Department of the Navy NAVAIRSYSCOM PMA-207 • 469900 Hinkle Circle, Bldg. 419 Patuxent River, MD 20670 Part 23 the Federal Aviation Poegulations.

Original Product Type Bertificate Number: A18SW Make: Fairchild Aircraft, Inc.

Model: SA227-DC (C-26B) Description of Type Design Change: Modification for external aft belly radome, radar mounting assembly, and electrical power interface for Litton search radar P/N 10-36400-02 in accordance with FAA approved ATS Master Data List 2056, Revision J, dated May 1, 2001 or later FAA approved revision. ATS FAA Approved Airplane Flight Manual Supplement Number 2037 to the Fairchild SA227-DC (C-26B) Flight Manual, dated July 13, 2001 or latter approved revision is required with this installation.

Limitations and Conditions: The installation defines modification for external aft belly radome, radar mounting assembly, and electrical power interface for Litton search radar P/N 10-36400-02 and 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. 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. (See Continuation Sheet 3 for applicable operating limitations).

30, 2003 Date Amended:

Call nine (Signature) Manager, Tech. and Administrative Support TOMNISTRATIO Staff, Los Angeles Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01054LA Date of Application: June 7, 1999 Date of Issuance: August 8, 2001 Date Amended:

Date Reissued: Aprl 15, 2002 Jan. 30, 2003 Limitations and Conditions: (Cont'd):

Center of Gravity Limits Aft Limit: 273.0 inches aft of datum at all weights.

Kinds of Operation Flight into known icing not permitted.

Maximum crosswind component 18 knots.

Flight with missing vortex generators prohibited.

Note:

This modification has been determined/demonstrated not to increase the noise level and is not considered an "acoustical change" as defined in Paragraph 21.93(b), Amendment 21-75 of the Federal Aviation Regulations.

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