FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 401-0064 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 01/28/2022 |
| Model | 401 | Expiration Date | 01/31/2029 |
| 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) | 50703615 |
| MFR Year | 1967 | Mode S Code (Base 16 / Hex) | A3878D |
| Type Registration | Individual | Fractional Owner | NO |
| Name | WILTON WILLIAM H | ||
| Street | PO BOX 415 | ||
| City | KAILUA KONA | State | HAWAII |
| County | HONOLULU | Zip Code | 96745-0415 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | IO 520 SERIES | Category | Normal |
| A/W Date | 04/04/1967 | Exception Code | No |
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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/ |
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| None |
| Mod Code | 28 | Mod Date | 20120517 |
| REMOVED FLOOR CAPET & SEATS IN POSTIONS 3 & 4 FROM AIRCRAFT TO MAKE ROOM FOR TEMPORARY FERRY FUEL SYSTEM INSTALLATION. INSTALLED TEMPORARYFERRY FUEL SYSTEM RESTING ON 3/8" THICK PLYWOOD BASE SUPPORTING ON EXISTING AIRCRAFT STUCTURE. PLYWOOD BASE IS INSTALLED TO FACILITATE EVEN LOAD DISTRIBUTION AND AIRCRAFT FLOOR LOADING LIMITS ARE NOT EXCEEDED. THE FERRY FUEL SYSTEM CONSISTS OF A TURTLEPAC FERRY TANK WITH CAPACITY OF 300 U.S. GALLONS, TWO 24 VDC FACET ELECTRIC PUMPS (P/N: 40164), SHUT-OFF VALVES, FUEL HOSES (SAE 100R6), HOSE FITTINGS AND HOSE CLAMPS. THE FERRY FUEL TANK MAY BE FILLED UP TO 300 U.S. GALLONS AND IS LOCATED IN THE AIRCRAFT CABIN BEHIND THE PILOTS SEATS. TANKS IS PRESSURE AND LEAK TESTED IN ACCORDANCE FAR 23.965(A)(1) AT POINT OF MANUFACTURE. THE FERRY TANK IS SECURED TO SEATS/TRACKS WITH CARGO TIE DOWN STAPS, TIE DOWN STRAPS ARE RATED 2,100 LBS EACH. FERRY FUEL TANK IS ELECTICALLY BONDED TO THE AIRFRAME TO FACILITATE STATIC ELECTRICITY DISCHARGE AS OUTLINED IN AC 43.13-1B. THE FERRY FUEL SYSTEM IS PLUMBED INTO LH AND RH MAIN FUEL TANKS AT THE FUEL RETURN LINES UTILIZING AN824 (TEE FITTINGS) AND THRU FUEL HOSES, MANUALLY CONTROLLED ELECTRIC FUEL PUMPS AND/OR MANUAL FUEL PUMP AND SELECTOR VALVES. FERRY FUEL PUMP, FUEL SELECTOR VALVE AND FUEL PUMP OPERATING SWITCH ARE LOCATED ON FLOOR BETWEEN THE PILOT AND CO-PILOT SEATS. THE TRANSFER OF THE FUEL FROM THE FERRY TANK TO LH AND RH MAIN TANKS IS TOBE UNDERTAKEN DURING NORMAL LEVEL CRUISE FLIGHT ONLY. SCHEMATIC OF THEFERRY SYSTEM IS ON ATTACHMENTS 1 & 2. REMOVED ELT ANTENNA TO MAKE ROOMFOR THE INSTALLATION OF LONG-WIRE HF ANTENNA. WEIGHT AND BALANCE IS CALCULATED AND ENTERED INTO THE AIRCRAFT RECORD. TEMPORARY FUEL SYSTEM | |||
