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N9147N has Assigned/Multiple Records

N-Number Entered: 9147n Aircraft Description
Serial Number 602-0623 Status Valid
Manufacturer Name AIR TRACTOR INC Certificate Issue Date 04/12/2018
Model AT-602 Expiration Date 04/30/2028
Type Aircraft Fixed Wing Single-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 53124341
MFR Year 2001 Mode S Code (Base 16 / Hex) ACA8E1
Type Registration Corporation Fractional Owner NO
Registered Owner
Name 1 LOWFLYER INC
Street 310 S INDEPENDENCE ST
City HARRISONVILLE State MISSOURI
County CASS Zip Code 64701-2352
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 P&W CANADA Classification Standard-Restricted
Engine Model PT6A-60A Category Forest, Agriculture and Pest Control, Aerial Advertising, Agriculture and Pest Control
A/W Date 01/09/2001 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 19951122
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 9-1-93 AND ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-CE-100/200 II, AF-CE-100/200-2, AF-CE-100-2, AF-CE-100/200-3-ID, AF-C-100/200-2-ID, AND THE FOLLOWING FUEL TANK DRAWINGS AF-TYP: 205,205. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT IS WITHIN THE 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 THE ABOVE NAMED DRAWINGS, OPERATED PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGMENT INSTRUCTIONS.

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