FAA REGISTRY
N-Number Inquiry Results
| Serial Number | E2513 | Status | Valid |
| Manufacturer Name | BEECH | Certificate Issue Date | 03/15/2007 |
| Model | A36 | Expiration Date | 11/30/2029 |
| 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) | 52222250 |
| MFR Year | None | Mode S Code (Base 16 / Hex) | A924A8 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | CHARNEY AIR INC | ||
| Street | 3511 SILVERSIDE RD STE 105 | ||
| City | WILMINGTON | State | DELAWARE |
| County | NEW CASTLE | Zip Code | 19810-4902 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | Unknown | Classification | Unknown |
| Engine Model | Unknown | Category | None |
| A/W Date | None | 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 |
| None |
| Mod Code | 28 | Mod Date | 19951027 |
| INSTALLED ONE 100.0 GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FOR FERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIRUSING THE FOLLOWING DRAWINGS: NAI M005, NAI SC001, NAI PS002, NAI TF001, NAI TF002, NAI V012, NAI TD009, AND THE INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS A36-KIT. THE TEMPORARY TANK IS PLACED ON A WOODEN PLATFORM AT THE CENTER PASSENGER SEAT LOCATION. THETEMPORARY TANK IS SECURED TO THE AIRFRAME WITH 1000 LBS LOAD HUGGER STRAPS. THE TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE AND IS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM THE TEMPORARY TANK IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE RH WING TANK AND THE AIRCRAFT FUEL SELECTOR VALVE BY ON-OFF VALVES, APPROPRIATE FITTINGAND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH A MANUFACTURED VENT ATTACHED TO A TEMPORARY PANEL SECURED IN THE STORM WINDOW OPENING WITH THE LINE 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 STANDARD PRACTICES FOUND IN AC 43.13-1A CHAPTER 14, SECTION 2 AND ACCEPTED INDUSTRY PRACTICES. WEIGHT AND BALANCE FOR THIS TEMPORARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATING INSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. | |||
