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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N58MS is Assigned

N-Number Entered: 58ms Aircraft Description
Serial Number E-2889 Status Cert Terminated
Manufacturer Name BEECH Certificate Issue Date None
Model A36 Expiration Date None
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) 51672263
MFR Year 1994 Mode S Code (Base 16 / Hex) A774B3
Type Registration Individual Fractional Owner NO
Registered Owner
Name REGISTRATION PENDING
Street 1634 SE 23RD ST
City OKLAHOMA CITY State OKLAHOMA
County OKLAHOMA Zip Code 73129-7661
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-550 SERIES Category Utility, Normal
A/W Date 08/24/1994 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
APPLICANT JM AERO LLC
APPLICATION DATED 051425
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 19950512
INSTALLED ONE 100.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FORFERRY 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 TD052, AND THE INSTALLATION WAS PER- FORMED PER NAI INSTALLATION INSTRUCTION A36-KIT. THE TEMPORARY TANK ISPLACED ON A WOODEN PLATFORM AT THE CENTER PASSENGER SEAT LOCATION. THETEMPORARY TANK IS SECURED TO THE AIRFRAME WITH 100 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 FITTINGS, AND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH THE 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 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. SEE 337 FOR FURTHER INFORMATION.
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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