CIRRUS DESIGN CORP (2066)

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Aircraft Description
Serial Number	2066	Status	Valid
Manufacturer Name	CIRRUS DESIGN CORP	Certificate Issue Date	06/02/2014
Model	SR20	Expiration Date	06/30/2017
Type Aircraft	Fixed Wing Single-Engine	Type Engine	Reciprocating
Pending Number Change	None	Dealer	No
Date Change Authorized	None	Mode S Code (base 8 / oct)	51423512
MFR Year	2010	Mode S Code (base 16 / hex)	A6274A
Type Registration	Corporation	Fractional Owner	NO

Registered Owner
Name	CAREFREE CIRRUS LLC
Street	PO BOX 5608
City	CAREFREE	State	ARIZONA
County	MARICOPA	Zip Code	85377-5608
Country	UNITED STATES

Airworthiness
Engine Manufacturer	CONT MOTOR	Classification	Standard
Engine Model	IO-360-ES	Category	Normal
A/W Date	10/22/2010

Temporary Certificates
None

Fuel Modifications
Modification 1 of 1
04/18/2014
INSTALLED TEMPORARY FUEL SYSTEM RESTING ON PLYWOOD SUPPORTING ON EXISTING AIRCRAFT STRUCTURE. PLYWOOD BASE IS INSTALLED TO FACILITATE EVEN LOAD DISTRIBUTION. AIRCRAFT FLOOR LOADING LIMITS ARE NOT EXCEEDED FERRY SYSTEM CONSISTS OF 2 ALUMINUM TANK. THE TANKING SYSTEM TOTAL CAPACITY IS 140 U.S. GALLONS. TANKS ARE CONSTRUCTED FROM .090 5052-H34 ALUMINUM WELDED AT ALL SEAMS, INTERNAL BAFFLES ARE INSTALLED AND WELDED INTO PLACE. CONSTRUCTION OF TANKS MEETS THE STANDARDS OF U.S. COAST GUARD 33 C.F.R. 183.580 SPECIFICATIONS. TANKS ARE PRESSURE AND LEAK TESTED IN ACCORDANCE WITH IAW FAR 23.965A(1). ALL TANKS ARE SECURED TO SEAT TRACKS WITH CARGO TIE DOWNS. THESE TIE DOWN AND 1/8' STEEL CABLES. THESE TIE DOWN STRAPS ARE OF IDENTICAL TYPE THAT HAVE BEEN UTILIZED IN PREVIOUSLY FAA APPROVED TANKING SYSTEMS. STRAPS, (2 PER TANK) SECURE THE TANKS BOTH LONGITUDINALLY AND LATERALLY. FERRY FUEL TANKS ARE ELECTRICALLY BONDED TO THE AIRFRAME TO FACILITATE STATI DISCHARGE, AND ARE VENTED TO THE ATMOSPHERE IAW AC43-13-1B. LEAK TEST OF ALL COMPONENTS FOLLOWING INSTALLATION FOUND SATISFACTORY. FERRY TANKING SYSTEM IS PLUMBED INTO THE AIRCRAFT FUEL SYSTEM AS NOTED ON THE AIRCRAFT FUEL SYSTEM SCHEMATIC ATTACHMENT 1. FERRY FUEL SYSTEM OPERATION AND MANAGEMENT DETAILS IS OUTLINED IN ATTACHMENT 2. CONTINUOUS AIRWORTHINESS COMPLIANCE NOT APPLICABLE DUE TO TEMPORARY INSTALLATION.

Complete data for this aircraft is available from the Federal Aviation Administration.