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N9946M has Assigned/Multiple Records

N-Number Entered: 9946m Aircraft Description
Serial Number 20700588 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 01/09/2020
Model 207A Expiration Date 01/31/2030
Type Aircraft Fixed Wing Single-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 53362265
MFR Year 1980 Mode S Code (Base 16 / Hex) ADE4B5
Type Registration Corporation Fractional Owner NO
Registered Owner
Name GRANT AVIATION INC
Street 6420 KULIS DR
City ANCHORAGE State ALASKA
County ANCHORAGE DIV Zip Code 99502
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 CONT MOTOR Classification Restricted
Engine Model IO-520-F Category Aerial Surveying
A/W Date 10/05/2001 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 T215212 Issue Date 06/21/2021 Expiration Date 07/21/2021
Fuel Modifications
Mod Code 28 Mod Date 19990302
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 ON 9-2-97 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-207-OI, AF-CE-207-FS, AF-CE-207-ID-1, AF-CE-207-ID-2, AF-CE-207-II, AND AF-TYP(S) 150. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, STRUCTURAL EVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FULE SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO.EXPIRY DATE IS 4/2/99.

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