STC SA02380CH

Transfined to ATc AcO United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA02380CHi This certificate issued to: Piaggio America, Inc.

1515 Perimeter Rd.

West Palm Beach, FL 33406 Purt 23 of the Federal Aviation Pegulations.

Original Product Type Certificate Number : A59EU Make: Piaggio Model: P-180 Description of Type Design Change: Installation of a Rockwell Collins TCAS-4000 Traffic Alert and Collision Avoidance System (TCAS II) in accordance with Envoy Aerospace Master Data List JW2368A-3445-01, Rev. A, dated January 30, 2007, or later FAA approved revision.

Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. 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.

Date of Application: November 05, 2006 Date Reissued: December 28, 2007; November 02, 2009; January 7, 2011 Date of Issuance: February 05, 2007 Date Amended:

FEDERAL AVIATION By Direction of the Administrator * Jany A s havo (Signature) TOMINSTRATO S. Frances Cox Manager, Special Certification Office Southwest Region (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02380CH Date of Issuance: January 7, 2011 Limitations and Conditions: (Continued):

1. FAA Approved Flight Manual Supplement, Jet Works Air Center Document JW2368A-3445-100, Revision-, dated February 05, 2007 or later FAA approved revision is required onboard the modified aircraft.

The aircraft must be maintained in accordance with Airworthiness Limitations contained in Jet Works Air Center Document JW2368A-3445-200, Chapter 10, Revision -, approved February 05, 2007 or later FAA approved revision, in addition to the basic aircraft maintenance manuals.

Cerlification Busis: The certification basis for the Piaggio P-180 is as follows:

The type certification basis for the Piaggio P-180 is shown on TCDS A59EU for parts not changed or not affected by this change.

The type certification basis for the parts changed or affected by this change since the reference date of application, November 05, 2006, is shown on TCDS A59EU. Additionally, the applicant has voluntarily complied with 14 CFR part 23 as amended by Amendment 23-55.

Applicable Regulations at the latest amendment 23-0 through 23-55

23.301(a), (b); 23.303; 23.305(a), (b); 23.307(a); 23.365(a), (b), (d); 23.561 (a), (b), (e); 23.571(c); 23.573(b);

23.575; 23.603(a); 23.605(a); 23.607(b); 23.609(a), (b); 23.611; 23.613(a), (b), (d); 23.619; 23.625(a); 23.867(a),

(b); 23.1301(a), (b), (c), (d); 23.1309(a), (b), (c), (d), (e); 23.1322 (a), (b), (d), (€); 23.1327(a); 23.1351(a);

23.1357(a), (b), (c), (d); 23.1359(b); 23.1365(a), (b), (d), (e), (f); 23.1367(a), (b), (c), (d); 23.1431 (a), (b);

23.1501; 23.1529; 23.1581(a), (b), (c), (d), (f); 23.1583(m); 23.1585(a), (i).

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FAA Form 8110-2-1(10-69) Page 3 of 3