FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N703JM is Assigned

N-Number Entered: 703jm Aircraft Description
Serial Number E-278 Status Valid
Manufacturer Name BEECH Certificate Issue Date 10/01/2012
Model A36 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) 52260207
MFR Year 1971 Mode S Code (Base 16 / Hex) A96087
Type Registration Individual Fractional Owner NO
Registered Owner
Name TOLLER KEVIN K
Street 1904 S DESERT PALM AVE
City BROKEN ARROW State OKLAHOMA
County TULSA Zip Code 74012-6133
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 520 SERIES Category Utility
A/W Date 08/12/1971 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 19980502
INSTALLED ONE 150.0 US GALLON ALUMINUM FUEL TANK IN CABIN AREA FOR FERRY PURPOSES ONLY. TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING FOLLOWING DRAWINGS:NAI M005, NAI SC001, NAI PS002, NAI TF001 NHAI TF002, NAI V012, NAI TD081, AND INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS A36-KIT. TEMPORARY TANK IS PLACED ON A WOODEN PLATFORM AT CENTER PASSENGER SEAT LOCATION. TEMPORARY TANK IS SECURED TO AIRFRAME WITH 1000 LBS LOAD HUGGER STRAPS. TEMPORARY TANK IS TEED INTO FUEL SUPPLY SYSTEM BETWEEN RH WING TANK AND AIRCRAFT FUELSELECTOR VALVE, BY ON-OFF VALVES, APPROPRIATE FITTINGS, AND LOW PRES- SURE HOSE. TANK IS VENTED OVERBOARD THROUGH MANUFACTURED VENT ATTACHEDTO A TEMPORARY PANEL SECURED IN THE STORM WINDOW OPENING WITH THE LINEFORWARD FOR POSITIVE TANK PRESSURE. TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION AND WAS DETERMINED TO BE SATISFACTORY. THIS FUEL SYSTEM 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 INSTRUCTIONARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 5/28/98.

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