FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 26777 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 10/09/2012 |
| Model | 170B | Expiration Date | 10/31/2028 |
| 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) | 51254205 |
| MFR Year | 1955 | Mode S Code (Base 16 / Hex) | A55885 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | AIRCRAFT PARTNER N4433B DST | ||
| Street | C/O AIRCRAFT PARTNER 4U UG | ||
| BERLINER STR 84 | |||
| City | BERLIN | State | |
| County | Zip Code | 13189 | |
| Country | GERMANY | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | 0-300 SER | Category | None |
| A/W Date | 09/19/1956 | 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 |
| Certificate Number | T126658 | Issue Date | 10/09/2012 | Expiration Date | 11/08/2012 |
| Mod Code | 28 | Mod Date | 19940330 |
| INSTALLED ONE 100.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FORFERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI M023, NAI V009, NAI TD009, NAI TF001, NAI TF002, NAI SC001, NAI PS002, AND THE INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS 170B-KIT. THIS TANK IS PLACED ON A WOODEN PLATFORM AT THE REAR PASSENGER SEAT LOCATION. THE TANK IS SECURED TO THE AIRFRAME WITH TWO 1000 LBS LOAN HUGGER STRAPS TO REAR SEAT TRACK SUPPORT STRUCTURE FWD AND AFT. THE TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE AND IS PRESSURE CHECKEDTO 3/5 PSI. FUEL FROM THE TEMPORARY TANK IS TEED INTO THE FUEL SUPPLYSYSTEM BETWEEN THE AIRCRAFT FUEL SELECTOR AND THE AIRCRAFT FUEL STRAINER BY AN ON-OFF VALVE, APPROPRIATE FITTINGS, A PUMP, AND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH THE AIRCRAFT RH REAR FRESH AIR VENT HOSE WITH THE LINE FACING FORWARD FOR POSITIVE TANK PRESSURE. THIS TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION AND WAS DETERMINED TO BE SATISFACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1A CHAPTER 14, SECTION 2. WEIGHT AND BALANCE FOR THIS TEMPORARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TOTHE FLIGHT CREW. OPERATING INSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. | |||
