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N25BB has Assigned/Multiple Records

N-Number Entered: 25bb Aircraft Description
Serial Number 102 Status Valid
Manufacturer Name LEARJET INC Certificate Issue Date 04/25/2016
Model 31A Expiration Date 04/30/2029
Type Aircraft Fixed Wing Multi-Engine Type Engine Turbo-fan
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50452500
MFR Year 1995 Mode S Code (Base 16 / Hex) A25540
Type Registration LLC Fractional Owner NO
Registered Owner
Name PARK AIR LLC
Street PO BOX 3944
City GLENDALE State CALIFORNIA
County LOS ANGELES Zip Code 91221-0944
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 GARRETT Classification Standard
Engine Model TFE731-2-2B Category Transport
A/W Date 05/20/2013 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 20191004
THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL CONSISTING OF (3) ALUMINUM FERRY FUEL TANKS, MOUNTED IN THE CABIN OF THE AIRCRAFT, ALONG WITH ASSOCIATED FERRY FUEL SUPPLY LINE, SELECTOR VALVES AND VENTSYSTEM. THE FERRY FUEL SYSTEM SUPPLIES PRESSURE FEED FERRY FUEL DIRECTLY TO THE LEFT WING MAIN TANK SUM DRAIN. THE SYSTEM REQUIRES NO ELECTRICAL POWER. POSITIVE FUEL PRESSURE TO THE SYSTEM IS BY CABIN PRESSURE. THE SYSTEM IS REQUIRED TO EXTEND THE RANGE FOR A FLIGHT FROMHONOLULU HAWAII TO NORTH LAS VEGAS, NEVADA. DESCRIPTION: THIS MAJOR ALTERATION WILL CONSTIST OF REMOVING THE AIRCRAFT PASSENGER SEATS, FURNISHINGS AND EQUIPMENT, AS REQUIRED, FROM THE PASSENGER COMPARTMENTAND INSTALLNG A TEMPORARY FERRY FUELSYSTEM IN THE CABIN. THE TEMPORARYFERRY FUEL SYSTEM WILL BE CONNECTED TO THE AIRCRAFT LEFT MAIN WING TANK FUEL DRAIN. TANK NUMBER AND CAPACITY LOCATION IN INCHES: NUMBER ONE AND TWO, 150 GALLONS 400, FORE AND AFT PLACEMENT LEFT AND RIGHT SIDES. NUMBER THREE, 125 GALLONS 325 LATERAL PLACEMENT. THE TANKS ARE RECTANGULAR IN DESIGN AND CONSTRUCTED FROM 5052 ALUMINUM .100 INCHES THICK BY ROYALL MANUFACTURING OF PLACERVILLE, CALIFORNIA. THE TANKS ARE PRESSURE AND LEAKED CHECKED AS PER PERTINENT FARS. THE TANKS ARE ELECTRICLLY GROUNDED TO AIRCRAFT STRUCTURE. THE TANKS ARE VENTED BY ONE WAY CHECK VENT VALVES WITH 3.5 NEGATIVE PRESSURE RELIEF. THE CABINPRSSURE WILL PROVIDE POSITIVE FUEL FLOW TO THE LEFT MAIN TANK SUMP DRAIN. THE TANK IS MOUNTE ON 3/4 INCH PLYWOOD PALLET. THE TANK IS SECURED USING 4 2000 POUND STRAPS SECURED TO (8) POINTS OF THE CARGO TIE DOWN RINGS. LOCATED IN THE EXISTING FLOOR SEAT RAILS. THE FERRY

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