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N896AH is Assigned

N-Number Entered: 896ah Aircraft Description
Serial Number 20700732 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 03/08/2024
Model 207A Expiration Date 03/31/2031
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) 53055646
MFR Year 1981 Mode S Code (Base 16 / Hex) AC5BA6
Type Registration LLC Fractional Owner NO
Registered Owner
Name AEROSPACE ASSET HOLDINGS LLC
Street 704 N KING ST STE 500
City WILMINGTON State DELAWARE
County NEW CASTLE Zip Code 19801-3584
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 Standard
Engine Model IO-550-F Category Normal
A/W Date 03/13/2024 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 T242430 Issue Date 03/08/2024 Expiration Date 04/07/2024
Fuel Modifications
Mod Code 28 Mod Date 19980223
THIS DATA WAS FIELD APPROVED BY FAA, NE-FSDO-05 ON 9/2/97 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION, INC. (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION, INC. DRAWINGS AF-CE-207-0I, AF-CE-207-FS, AF-CE-207-ID-1, AF-CE-207-ID-2, AF-CE-207-II, AND AF-TYP(S) 150.60 A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS,OPERATES PROPERLY, AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. THE TANK IS PLACARDED FOR QUANTITY AND GRADE. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH STANDARD PRACTICES PERTAINING TO HARDWARE AND FITTINGS. THE TANK HAS BEEN PRESSURE CHECKED TO 3.5 PSI. PRIOR TO APPROVING THIS AIRCRAFT FOR A RETURNTO SERVICE IN IT'S STANDARD CATEGORY, THE FUEL SYSTEM MUST BE RETURNED TO IT'S ORIGINAL CONFIGURATION. THE MAGNETIC COMPASS CHECKED FOR ACCURACY. THE TEMPORARY EQUIPMENT AND PLACARDS REMOVED. THE AIRCRAFT CHECKED FOR DAMAGE WHILE IN THE OVERWEIGHT CONDITION. (EXPIRY 3/10/98)
Deregistered Aircraft
None
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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