DOT logo United States Department of Transportation
Aircraft Inquiry

FAA REGISTRY

N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N601PE is Assigned

N-Number Entered: 601pe Aircraft Description
Serial Number 61P-0421-153 Status Valid
Manufacturer Name SMITH Certificate Issue Date 06/19/2007
Model AEROSTAR 601P Expiration Date 07/31/2027
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) 51746100
MFR Year 1977 Mode S Code (Base 16 / Hex) A7CC40
Type Registration LLC Fractional Owner NO
Registered Owner
Name VCS TRANSPORTATION LLC
Street 703 HOWMET DR STE H
City HAMPTON State VIRGINIA
County HAMPTON Zip Code 23661-1093
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 Special Flight Permit
Engine Model IO 540 SER Category Operate Excess of Maximum Weight
A/W Date 07/01/2015 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 20110824
INSTALLATION OF COLLAPSIBLE FERRY FUEL TANK. FUEL TANK MANUFACTURED BYTURTLE-PAC PTY. LTD SPECIFICALLY FOR THIS AIRCRAFT. THIS ALTERATION IS APPROVED FOR INSTALLATION IN THIS AIRCRAFT BY J.R.G. DESIGN, INC. ENGINEERING ORDER NUMBER: JRG09-31-0706. (FAA FORM 8110-3 ATTACHED). AIRCRAFT WEIGHT AND BALANE HAS BEEN COMPUTED, AND IN THE FULLY LOADED CONFIGURATION FALLS WITHIN THE MANUFACTURERS APPROVED CG LIMITS. THE AIRCRAFT INSTRUMENT PANEL HAS BEEN PLACARDED WITH THE AIRSPEED LIMITATIONS AS OUTLINED IN FAA AUTHORIZATION LETTER.

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