STC SA184EA

United States of America 9A-219 Department of Transportation Federal Aviation Administration Supplemental Type Certificate EA 2976 EAS Number 511848A This certificate issued to: Wiggins Airways Inc.

Norwood Municipal Airport Norwood, Massachusetts 02062 Part 3 of the CI.VI.1 A ix Regulalions:

Original Product -TypeCertificate Number: AIEA Make: Piper Model: PA -30 Description of Type Design Change:

Installation of 13 quart alcoho propeller anti-icing kit utilizing either a Weldon pump (P/N 100B-6) or a Bendix pump (P/N 478360), in accordance wich:

(See STC continuation sheet page 2) Limitations and Conditions:

1. Wiggins Airways Inc. AFM Supplement WAP 503, revision 1, for Weldon pump kit or WAP 503-1 for the Bendix pump kit, both FAA approved 10/15/71, to the PA-30 Airplane Flight Manual is required with this installation.

2. Placard required in full view of the pilot: "This aircraft is not fully equipped for flight into icing conditions.

(See STC continuation sheet page 2)

Date of Application: 2 February 1964 Date Reissued:

Date of Issuance: 10 March 1964 Date Amended: 15 October 1971 FEDERAL AVIATION Pers didn t les Alministrator #. Oleksak (Signature) T MINISTRATO Chief, Engineering & Manufacturing Branch (Title)

U.S. GOVERNMEN Signature of grantor (In ink): - Date of Transfer: _ Extent of Authority (if licensing agreement): - (City, State, and ZIP code) (Number and street) (Address of grantor) from (Name of grantor) (Print or type) (City, State, and ZIP code) (Number and street) (Address of transferee) - to (Name of transferee) - Transfer the ownership of Supplemental Type Certificate Number

TRANSFER ENDORSEMENT The FAA will reissue the certificate in the name of the transferee and forward it to him.

the transfer of this Supplemental Type Certificate.

1 dated 3-18-71 Installation Drawing WAP 501, rev. 1 dated 3-18-71 Installation Instructions WAP 502, xev. 1 dated 3-18-71 Kit Description and Operation Install Bendix pump anti-ice kit according to:

WAP 500A, rev. 1 dated 3-18-71 Installation Drawing WAP 501-1, dated 3-18-71 Installation Instructions WAP 502-1, dated 3-18-71 Kit Description and Operation Limitations and Conditions: (continued) The installation of this equipment does not authorize the operation of Piper PA-30 Aircraft into known icing conditions.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined that the inter-relationship between this change and any of these other previously approved modifications will introduce no adverse affect upon the airworthiness of that airplane.

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