FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N36LH is Assigned

N-Number Entered: 36lh Aircraft Description
Serial Number E-614 Status Valid
Manufacturer Name BEECH Certificate Issue Date 05/16/2003
Model A36 Expiration Date 07/31/2027
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) 51005365
MFR Year 1974 Mode S Code (Base 16 / Hex) A40AF5
Type Registration LLC Fractional Owner NO
Registered Owner
Name JACKSON AVIATORS LLC
Street 301 DEMONBREUN ST UNIT 1809
City NASHVILLE State TENNESSEE
County DAVIDSON Zip Code 37201-2248
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 None
A/W Date None 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 19980914
INSTALLED ONE 70.0 US GALLON ALUMINUM FUEL TANK IN CABIN AREA FOR FERRY PURPOSES ONLY. TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI M005, NAI SC001, NAI PS002, NAI TF001, NAI TF002, NAI V012, ANI TD077 AND INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS A36-KIT. TEMPORARY TANK PLACED ON A WOODEN PLATFORM AT CENTER PASSENGER SEAT LOCATION. TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE AND IS PRESSURE CHECKED TO3.5 PSI. FUEL FROM TEMPORARY TANK IS PLUMBED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE RH WING TANK AND AIRCRAFT FUEL SELECTOR VALVE, BY ON-OFF VALVES, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. 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 SATIS-FACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE 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. OPERATINGINSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 10-13-98.

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