STC SH299NW

This Certificate issued to Siam Hiller Holdings, Inc.

925 M Street Firebaugh, California 93622 Part 6 of the Civil Air Regulations. effective January 15, 1951. See page 3 of this STC for certification basis.

4H10 Hiller UH-12D Description of Type Design Change: Installation of Soloy cargo racks in accordance with FAA approved Soloy Drawing List No. 560-201.

NOTE: Only those Hiller UH-12D rotorcraft, which have been converted to turbine power in accordance with STC SH177WE, are eligible for this modification.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this Certificate must be maintained as part of the permanent records for the modified rotorcraft. The limitations and conditions of Rotorcraft Type Certificate 4H10 and STC SH177WE apply except as outlined on page 3 of this STC. 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.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: January 8, 1976

Date of issuance: May 18, 1976

Date reissued: 05/28/91; 11/30/95; 08/19/05

Date amended: 05/28/91

( Signature)

Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

Number SH299NW

Limitations and Conditions: (Continued)

1. Rotorcraft Flight Manual Supplement

FAA approved Soloy Conversions, Ltd. Rotorcraft Flight Manual Supplement RFMS-4 for cargo racks is required together with the FAA approved Soloy Conversions, Ltd. Rotorcraft Flight Manual dated April 10, 1975, in lieu of that specified for the basic unmodified Model UH-12D. Refer to the applicable portions of this FAA approved Soloy Conversions, Ltd.

Rotorcraft Flight Manual Supplement RFMS-4 for the required placards.

2. Maximum Cargo Rack Load – 260 pounds per side.

3. Certification Basis

a. Civil Air Regulations Part 6 dated January 15, 1951, with Amendment 6-1 through 6-7 thereto.

b. The following paragraphs of Federal Avia tion Regulations Part 27 including Amendment 27-1 thereto.

27.45 through 27.79, 27.143, 27.361(a), 27.901 through 27.1193, 27.1305, 27.1337,

27.1351(c), 27.1353, 27.1505, 27.1509(c), 27.1521, 27.1549 through 27.1555, 27.1557,

27.1559, 27.1583(b), and (f), 27.1587, 27.1589.

c. Special Conditions 27-1-WE-1, dated August 6, 1968, and Amendment 1 thereto dated February 28, 1975.

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