DOT logo United States Department of Transportation
Aircraft Inquiry

FAA REGISTRY

N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N908SB is Assigned

N-Number Entered: 908sb Aircraft Description
Serial Number 81 Status Valid
Manufacturer Name DASSAULT Certificate Issue Date 08/18/2018
Model FALCON 900 EX Expiration Date 08/31/2028
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) 53107166
MFR Year 2000 Mode S Code (Base 16 / Hex) AC8E76
Type Registration LLC Fractional Owner NO
Registered Owner
Name FALCON HUNTER LLC
Street 1100 LOUISIANA ST STE 200
City HOUSTON State TEXAS
County HARRIS Zip Code 77002-5215
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 HONEYWELL Classification Standard
Engine Model TFE-731-SER Category Transport
A/W Date 04/27/2001 Exception Code Yes
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 19980302
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 6-11-93 AND ORIGINAL337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-CE-404-01, AF-CE-4040-FS, AF-CE-404-ID, AF-CE-404-II, AND AF-TYP(S) 100. NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PRO- VIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVAL-UATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FORACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE 3/26/98.

You are accessing a U.S. Government authorized information system, which includes (1) this computer, (2) this computer network, (3) all computers connected to this network, (4) all devices and storage media attached to this network or to a computer on this network, and (5) all cloud services and hosting environments supporting this information system. This information system is provided for U.S. Government-authorized use only.

Unauthorized or improper use of this system may result in disciplinary action, as well as civil and criminal penalties.

By logging in and using this information system, you understand and consent to the following:

  • You have no reasonable expectation of privacy regarding communications or data transiting or stored on this information system.
  • At any time, and for any lawful Government purpose, communication between the user and this information system, data transiting to/from the system, or stored on this system is subject to monitoring, interception, and search.
  • Any communications or data transiting or stored on this information system may be disclosed or used for any lawful Government purpose.


D O T Triskelion

U.S. Department of Transportation

Federal Aviation Administration

800 Independence Avenue, SW

Washington, DC 20591

(866) TELL-FAA | (866) 835-5322