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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N38GW is Assigned

N-Number Entered: 38gw Aircraft Description
Serial Number 1015 Status Valid
Manufacturer Name CIRRUS DESIGN CORP Certificate Issue Date 02/02/2019
Model SR22 Expiration Date 02/28/2029
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) 51054634
MFR Year 2004 Mode S Code (Base 16 / Hex) A4599C
Type Registration Corporation Fractional Owner NO
Registered Owner
Name AIRCRAFT PARTNER N38GW DST
Street C/O AIRCRAFT PARTNER 4U UG
BERLINGER STRASSE 84
City BERLIN State
County Zip Code 13189
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 Special Flight Permit
Engine Model IO-550 SERIES Category Operate Excess of Maximum Weight
A/W Date 03/05/2008 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
Certificate Number T190858 Issue Date 02/06/2019 Expiration Date 03/08/2019
Fuel Modifications
Mod Code 28 Mod Date 20080307
MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE ACFT FUEL SYSTEM TO INCORPORATE A TEMP. 100 GAL. EXTENDED RANGE FUEL TANK & ASSOCIATED VALVES AND PLUMBING FOR FERRY OPERATIONS. SYSTEM ALSO INCORPORATES ANOIL REPLENISH SYSTEM. MAJOR ALTERATION WILL CONSIST OF ONE TEMPORARY 100 GAL. EXTENDED RANGE FUEL TANK MFR'D BY TDL AERO OF CALIFORNIA. TANK WILL BE LOCATED AT FUSELAGE STATION 175.0. THE TANK IS RECTANGULRIN DESIGN AND CONSTRUCTED IAW ABYC H-24.18(2-12) & 46 CFR SEC. 58.50A (4-6) FROM 5052 ALUMINUM .100 INCHES THICK IAW ABYC H-24 18.1 TANK MATERIALS. THE TANK IS DESIGNED AND WELDED TO MEET THE REQUIREMENTS OF FAR 23.963(A). THE TANK IS PRESSURE AND LEAK CHECKED IAW FAR 23.965(A)(1). THE TEMP. EXTENDED RANGE FUEL 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 REPLACE- MENT INSPECTIOIN PANEL CIRRUS P/N 20317-001, LOCATION OF R/H AFT SIDE OF FUSELAGE. SYSTEM INCORPORATES A FUEL JETTISON SYSTEM, CONTROLLED BY A VALVE WHICH THE PILOT OPERATES. FUEL IS JETTISONED THROUGH PLUMBING EXITING THE ACFT FROM THE MODIFIED TEMP INSPECTION PANEL CIRRUS P/N 20317-001 LOCATION RE3 ON R/H AFT SIDE OF FUSELAGE. CABIN FLOOR IS REINFORCED WITH 3/4 INCH PLYWOOD. TANK RESTS IN A WELDED ALUMINUM TRAY BY THE USE OF 1/8 INCH ACFT CABLE AND TURNBUCKLES ATTACHED BY A BRACKET WHICH IS MOUNTED TO THE ACFT SEAT TRACK ASSEMBLYAND 222 BULKHEAD CROSS MEMBER. TEMP 100 GAL. FERRY TANK FEEDS TO THE FERRY FUEL SELECTOR VALVE THROUGH A NO. 8 HOSE. SELECTOR VALVE FEEDS THROUGH A BULKHEAD FITTING TO A 1/2 INCH AEROQUIP BRAIDED FUEL LINE & T-FITTINGS INSTALLED BETWEEN THE ACFT FUEL SELECTOR VALVE AND THE
Deregistered Aircraft
None
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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