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N277LS is Assigned

N-Number Entered: 277ls Aircraft Description
Serial Number 2312 Status Valid
Manufacturer Name BELL Certificate Issue Date 09/27/2022
Model 206B Expiration Date 09/30/2029
Type Aircraft Rotorcraft Type Engine Turbo-shaft
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50540610
MFR Year 1978 Mode S Code (Base 16 / Hex) A2C188
Type Registration LLC Fractional Owner NO
Registered Owner
Name G & G TRANSPORATION LLC
Street 21738 E ORION WAY
City QUEEN CREEK State ARIZONA
County MARICOPA Zip Code 85142-6448
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 H2SW Type Certificate Holder BELL HELICOPTER TEXTRON CANADA LTD
Engine Manufacturer ALLISON Classification Standard
Engine Model 250 SER 250HP Category Normal
A/W Date 01/09/1978 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 19910830
INSTALLATION OF TEMPORARY FERRY TANK SYSTEM. INSTALLED 55 GALLON CAPACITY, PRESSURE TESTED FUEL VESSEL, ON LOCALLY FABRICATED WOODEN CRADLE, WITH 2 EA. 1/8" CUSHIONED STEEL BRAIDED CABLES AND TURNBUCKLE ASSEMBLIES. CRADLE AND TANK ASSEMBLY IS STRAPPED ONTO AIRCRAFT AFT PASSENGER SEAT BULKHEAD WITH 2 EA. 1 3/4" X 1/9", 5000 LB. LOAD CAPACITY CARGO TIEDOWN STRAPS ATTACHED FROM SEATBELT FITTINGS, AROUND TANK, TO 2 EA. STAINLESS STEEL BRACKETS ATTACHED TO EXISTING AIRCRAFT CARGO HOOK FITTING BOLTS INSTALLED THROUGH FLOOR.

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