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N153E has Assigned/Multiple Records

N-Number Entered: 153e Aircraft Description
Serial Number 2415 Status Valid
Manufacturer Name CIRRUS DESIGN CORP Certificate Issue Date 06/21/2023
Model SR22 Expiration Date 06/30/2030
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) 50152670
MFR Year 2007 Mode S Code (Base 16 / Hex) A0D5B8
Type Registration LLC Fractional Owner NO
Registered Owner
Name QUALITAIR LLC TRUSTEE
Street FLUGPLATZ MICHELSTADT
MOSSAUER STRASSE 17
City MICHELSTADT State
County Zip Code 64720
Country GERMANY
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 03/19/2007 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
Certificate Number T237404 Issue Date 06/22/2023 Expiration Date 07/22/2023
Fuel Modifications
Mod Code 28 Mod Date 20080820
MAJOR ALTERATION CONSISTS OF ONE TEMPORARY 100 GALLON EXTENDED RANGE FUEL SYSTEM TO INCORPORATE A TEMP. 100 GALLON EXTENDED RANGE FUEL TANKAND ASSOCIATED VALVES AND PLUMBING FOR FERRY OPERATIONS. SYSTEM ALSO INCORPORATES AN OIL REPLENISH SYSTEM. TANK MFR'D BY TDL AERO OF CALIFORNIA. TANK WILL BE LOCATED AT FUSELAGE STATION 175.0. TANK IS RECTANGULAR IN DESIGN AND CONSTRUCTED IAW ABYC H-24.18(2-12) AND 46 CFR SECTION 58.50(A)(4-6) FROM 5052 ALUM. .100" THICK IAW ABYC-H-24 18.1 TANK MATERIALS. TANK IS DESIGNED/WELDED TO MEET REQUIREMENTS OF FAR 23.963(A). TANK IS PRESSURE/LEAK CHECKED IAW FAR 23.965(A)(1). TEMP. TANK IS GROUNDED TO ACFT STRUCTURE. TANK IS VENTED TO POSITIVE AIR PRESSURE THROUGH A VENT SYSTEM FROM A SINGLE VENT FITTING MOUNTED ON A MODIFIED TEMP. REPLACEMENT INSPECTION PANEL CIRRUS P/N 20317-001,LOCATION ON R/H AFT SIDE OF FUSELAGE. SYSTEM INCORPORATES A FUEL JETTISON SYSTEM, CONTROLLED BY A VALVE WHICH PILOT OPERATES. REFER TO 337 FOR ADDITIONAL INFORMATION.

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