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N-Number Inquiry Results

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N30LP is Assigned

N-Number Entered: 30lp Aircraft Description
Serial Number 310R0995 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 10/10/2007
Model 310R Expiration Date 10/31/2028
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50617001
MFR Year 1977 Mode S Code (Base 16 / Hex) A31E01
Type Registration Corporation Fractional Owner NO
Registered Owner
Name DIALYSIS CLINIC INC
Street 1633 CHURCH ST STE 500
City NASHVILLE State TENNESSEE
County DAVIDSON Zip Code 37203-2948
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 3A10 Type Certificate Holder TEXTRON AVIATION INC
Engine Manufacturer CONT MOTOR Classification Standard
Engine Model IO 520 SERIES Category Normal
A/W Date 09/09/1977 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 20090812
UNINSTALLED A PREVIOUSLY INSTALLED LOCKER TANK INSTALLATION (AIR AMERICA STC SA2872SW). INSTALLED O&N AIRCRAFT MODIFICATIONS LOCKER TANK STC SA2504CE. IN ACCORDANCE WITH THE CURRENT STC HOLDER THE 18.5GALLON FUEL TANKS INSTALLED BY STC SA2872SW ARE SAME AS SUPPLIED WITH STC SA2504CE AND ARE USED IN THIS INSTALLATION AS IS THE PLUMBING ALONG LEADING EDGE FROM WS 100.50 RIGHT AND LEFT, TO MAIN (TIP) TANKS.THE CIRCUIT BREAKERS OCCUPY THE POSITION FORMERLY USED BY IN THE OPTIONAL CESSNA LOCKER TANK INSTALLATION. THE CONTROL SWITCHES ARE MOUNTED IN THE INSTRUMENT PANEL TO THE LEFT OF THE PILOT CONTROL YOKE IN VIEW OF THE PILOT. THIS SYSTEM, AS INSTALLED, CONFORMS TO STC SA2504CE IN FORM AND FUNCTION. THE AIRPLANE WAS WEIGHED AND A NEW WEIGHT AND BALANCE REPORT MADE. THE STC SA2504CE HAS NO SPECIFIC INSTRUCTIONS FOR CONTINUED AIRWORTHINESS. THE SYSTEM IS THEN REQUIREDTO BE MAINTAINED AND INSPECTED IN ACCORDANCE WITH FAR PART 43 APPENDIXD, INSTALLATION DRAWINGS SUPPLIED WITH STC SA2504CE, AND CESSNA 310R MAINTENANCE MANUAL ATA CHAPTER 5, ATA CHAPTER 20, AND FOR LIMITED GENERAL SYSTEM LAYOUT REFERENCE ATA CHAPTER 28.
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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