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N552HF is Assigned

N-Number Entered: 552hf Aircraft Description
Serial Number 208B2205 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 10/01/2022
Model 208B Expiration Date 10/31/2029
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) 51603616
MFR Year 2010 Mode S Code (Base 16 / Hex) A7078E
Type Registration Corporation Fractional Owner NO
Registered Owner
Name MISSION AVIATION FELLOWSHIP
Street 112 N PILATUS LN
City NAMPA State IDAHO
County CANYON Zip Code 83687-9635
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
Engine Model PT6A-114A Category Normal
A/W Date 04/25/2018 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 20190507
INSTALLED RANGEFLYERS, INC LONG RANG SUPPLEMENTAL FUEL SYSTEM, IN ACCORDANCE WITH THE APPROVED MANUAL, DESIGN, FABRICATION, INSTALLATIONAND LONG RANGE SUPPLEMENTAL FUEL SYSTEM, CESSNA 208 SERIES AIRCRAFT. DRAWING NUMBER 208, 208A, 208B, ADDENDUM NUMBER 9, DATED 06 AUG 2017. THIS FERRY FUEL TANK APPLICATION IF FOR THE CESSNA 208, 208A AND 208B ONLY. ALL PARTS, INSTALLATION AND MAINTENANCE AND OPERATION ARE CONTAINED IN DRAWING NUMBER: 208, 208A, 208B. EXTENED RANGE TANKS ARE CONNECTED TO THE AIRCRAFT FUEL SYSTEM AND ELECTRICAL SYSTEMS PER SECTION 6. OPERATION IS PER SECTION 8. INSPECTION/MAINTENANCE: CHECK ALL FITTINGS FOR LEAKAGE AND STRAPS FOR TIGHTNESS AT EACH REFUELING OPERATION. TIGHTEN AS NECESSARY. VERIFY PUMPS ARE OPERATIONAL AND FUELTRANSFERS APPROPRIATELY PER VALVE SELECTION. REMOVE IN REVERSE ORDER OF INSTALLATION. LEAK CHECK SYSTEMS AFTER REMOVAL AND RETURN OF AIR CRAFT SYSTEM TO NORMAL.DIAGRAMS ARE ALL CONTAINED IN DRAWING NUMBER 208, 208A, 208B. ALL MATERIAL SPEXIFICATIONS (DATA) IS CONTAINED IN DRAWING NUMBER 208, 208A, 208B. NO SPECIAL TOOLS REQUIRED. ALL SUPPLEMENTAL FUEL SYSTEMS COMPONENTS MUST BE REMOVED AT DESTINATION ORAT EXPIRATION OF SPECIAL FLIGHT PERMIT. NO PERSON MAY OPERATE THIS AIRCRAFT, AS ALTERED HEREIN, UNLESS IT HAS WITHIN IT AN APPROPRIATE AND CURRENT SPECIAL FLIGHT PERMIT ISSUED UNDER PART 21. AIRCRAFT WAS WEIGHED AND NEW WEIGHT AND BALANCE IN AIRCRAFT.
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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