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N941DS has Assigned/Multiple Records

N-Number Entered: 941ds Aircraft Description
Serial Number 3246050 Status Valid
Manufacturer Name PIPER Certificate Issue Date 01/23/2023
Model PA-32R-301 Expiration Date 01/31/2030
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) 53210473
MFR Year 1996 Mode S Code (Base 16 / Hex) AD113B
Type Registration LLC Fractional Owner NO
Registered Owner
Name MIRROR INVINCIBLE LLC
Street 106 LADY LANE
City ROTONDA State FLORIDA
County CHARLOTTE Zip Code 33947
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 None Type Certificate Holder None
Engine Manufacturer LYCOMING Classification Standard
Engine Model IO-540-K1G5 Category Normal
A/W Date 08/03/2022 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 T230895 Issue Date 01/23/2023 Expiration Date 02/22/2023
Fuel Modifications
Mod Code 28 Mod Date 19961009
INSTALLED ONE 150.0 US GALLONG ALUMINUM FUEL TANK IN CABIN AREA FOR FERRY PURPOSES ONLY. TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI PS002, NAI TF001, NAI TF002, NAI M007, NAI V021, NAI SC002, NAI BTD055, AND THE INSTALLATION WAS PERFORMEDPER NAI INSTALLATION INSTRUCTIONS PA32R-301 KIT. TANK IS PLACED ON A WOODEN PLATFORM AT THE REAR PASSENGER SEAT LOCATION. TANK IS SECURED TO THE AIRFRAME WITH TWO 1000 LB LOAD HUGGER STRAPS, ATTACHED TO THE FWD SEAT TRACKS AND THE REAR SEAT BELT ATTACH POINTS. TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE, AND WAS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM TEMPORARY TANK IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE AIRCRAFT SELECTOR VALVE AND THE AIRCRAFT ELECTRIC FUEL PUMP, BY AN ON-OFF VALVE, APPROPRIATE FITTINGS AND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH THE PILOTS VENT WINDOW WITH A PITOT FACING FORWARD FOR POSITIVE TANK PRESSURE. THIS TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION AND WAS DETERMINED TO BE SATISFACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1A, CHAPTER 14, SECTION 2. WEIGHT AND BALANCE FOR THIS TEMPO-RARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATING INSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO.
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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