FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N517CP is Assigned

N-Number Entered: 517cp Aircraft Description
Serial Number 3323 Status Valid
Manufacturer Name CIRRUS DESIGN CORP Certificate Issue Date 08/13/2021
Model SR22 Expiration Date 08/31/2028
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) 51475660
MFR Year 2008 Mode S Code (Base 16 / Hex) A67BB0
Type Registration Corporation Fractional Owner NO
Registered Owner
Name INFORMATION MANAGEMENT SYSTEMS INC
Street 541 COUNTRYSIDE PL
City MADISON State MISSISSIPPI
County MADISON Zip Code 39110-8387
Country UNITED STATES
Airworthiness INFORMATION PROVIDED HERE SHOULD NOT BE USED TO DETERMINE THE AIRWORTHINESS OF AN AIRCRAFT.
Refer to 14 CFR Parts 39, 43, 91, and FAA Order 8130.2 for airworthiness regulations and guidance.
Type Certificate Data Sheet A00009CH Type Certificate Holder CIRRUS DESIGN CORP
Engine Manufacturer CONT MOTOR Classification Standard
Engine Model IO-550-N Category Normal
A/W Date 10/24/2008 Exception Code No
The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis for a determination regarding the
airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/
Other Owner Names
None
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 20160825
THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY 100 GALLON AND 40 GALLON EXTENDED RANGE FUEL TANKS, AND ASSOCIATED VALVES AND PLUMBIN FOR FERRY OPERA TIONS. THE 100 GALLON TANK WILL BE LOCATED AT FUSELAGE STATION 171.5 AND THE 40 GALLON TANK WILL BE LOCATED AT STATION 145.0. THE TEMPORARYEXTENDED RANGE FUEL TANKS ARE GROUNDED TO AIRCRAFT STRUCTURE. THE TANKS ARE VENTED TO POSITIVE AIR PRESSURE. THE CABIN FLOOR IS REIN FORCED WITH 1/2 INCH PLYWOOD. THE FUEL TANKS ARE MOUNTED ON 1/2 INCH PLYWOOD, AND SECURED USING RATCHED STRAPS. THE TEMPORARY 100/40 GALLONFERRY TANK FEED THROUGH NO. 8 HOSE, CONNECTED TO LHS FUEL TANK AT THE CDC SUPPLIED FILLER FITTING. INSTALLATION COMPLETED USING TDL AERO ENTERRPRISES, SR2X INSTALLATION DRAWINGS AND INSTRUCTIONS. REMOVAL OF FORWARD TANK PER OPERATION LIMITATIONS COMPLETED IAW TDL AERO ENTER PRISES, SR2X INSTALLATION DRAWINGS AND INSTRUCTIONS. SEE ATTACHED SHEET WITH WEIGHT AND BALANCE DATA. OPEN ALL DOORES PRIOR TO FUELING. FILL AIRCRAFT WING TANKS FIRST PRIOR TO FUELING FERRY TANK. FUEL FERRYTANK BY SPECIFIC METERING OF FUEL TO CAPACITIES PLACARDED ON FERRY TANK. DURING FUELING INSPECT SYSTEM FOR LEAKS, STOP FUELING IF LEAKS ARE DETECTED AND CORRECT ANY DEFECTS. INSTALL FERRY TANK CAP AND ASSURE IT IS TIGHT. AIRCRAFT MUST BE OPERATED PER A SPECIAL FLIGHT PERMIT AND OPERATIONS LIMITATIONS WHILE FERRY FUEL SYSTEM IS INSTALLEDFERRY SYSTEM SHALL BE REMOVED UPON REACHING DESTINATION IN THE OPERATIONS LIMITATIONS.

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