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N56GF is Assigned

N-Number Entered: 56gf Aircraft Description
Serial Number TG-29 Status Valid
Manufacturer Name BEECH Certificate Issue Date 07/10/2023
Model 56TC Expiration Date 07/31/2030
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 51622455
MFR Year 1967 Mode S Code (Base 16 / Hex) A7252D
Type Registration Corporation Fractional Owner NO
Registered Owner
Name INTERNATIONAL AIR SERVICES INC TRUSTEE
Street 701 S CARSON ST STE 200
City CARSON CITY State NEVADA
County CARSON CITY Zip Code 89701-5239
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 TI0-540 SER Category Normal
A/W Date 03/07/1995 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 T238057 Issue Date 07/10/2023 Expiration Date 08/09/2023
Fuel Modifications
Mod Code 28 Mod Date 19950315
INSTALLED 2 100.0 US GALLON ALUMINUM TEMPORARY FUEL SYSTEMS IN THE CABIN AREA FOR FERRY PURPOSES ONLY. THE TEMPORARY SYSTEM WAS INSTALLEDBY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI BTD029, NAI M035, NAI TF001, NAI TF002, NAI PS002, NAI V012 NAI AND THE INSTALLATION WASPERFORMED PER NAI INSTALLATION INSTRUCTIONS B56-KIT. THE TANKS ARE PLACED ON A WOODEN PLATFORM AT THE CENTER CABIN SEAT LOCATIONA ND AFT SEAT LOCATION. THE TANKS ARE SECURED TO THE AIRFRAME WITH TWO 1000 LBSLOAD HUGGER STRAPS TO THE 2 FRONT AND REAR SEAT TRACK SUPPORT STRUCT- URES. THE TEMPORARY TANKS ARE PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE AND WERE PRESSURE CHECKED TO 3.5 PSI. FUEL FROM THE TEMPORARY TANKS IS TEED INTO THE FUEL SUPPLY SYSTEM DOWN STREAM OF THE SELECTOR.THIS CONNECTION WAS MADE BY ON-OFF VALVES, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH THE PILOTS STORM WINDOW. WITH THE LINE FACING FORWARD FOR POSITIVE TANK PRESSURE.SEE FILE FOR COMPLETE INFO.

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