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N862K has Assigned/Multiple Records

N-Number Entered: 862k Aircraft Description
Serial Number 550-0257 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 04/22/2022
Model 550 Expiration Date 04/30/2029
Type Aircraft Fixed Wing Multi-Engine Type Engine Turbo-fan
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 52753446
MFR Year 1981 Mode S Code (Base 16 / Hex) ABD726
Type Registration LLC Fractional Owner NO
Registered Owner
Name N862K LLC
Street 10 PINEWOLD CIR
City HOUSTON State TEXAS
County HARRIS Zip Code 77056-1400
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 WILLIAMS Classification Standard
Engine Model FJ44-3A Category Transport
A/W Date 10/27/2017 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 20090108
INSTALLATION OF EXTENDEDC RANGE FUEL TANK AND RELOCATION OF AFT PRESSURE BULKHEAD, IN ACCORDANCE WITH BRANSON AIRCRAFT CORP LIST OF DRAWINGS AND DOCUMENTS NO. 91800, SHEETS 1 AND 2, REVISION A, DATED 09/10/1976, APPROVED 09/19/1976, OR LATER FAA APPROVED REVISION. APPROVED FAA AIRPLANE FLIGHT MANUAL SUPPLEMENT 09/16/1976 (FOR MODEL 500) OR 1/22/1979 (FOR MODEL 550) OR SUBSEQUENT FAA APPROVED REVISION REQUIRED. CESSNA SB 34-15 OR SB 34-23, REFERENCE NOTE 7 OF TCDS A22CELATEST REVISION, MUST BE INCORPORATED UNLESS MODIFIED AIRCRAFT WITH FULL CABIN TANK FUEL, MINIMUM CREW, AND REQUIRED BALLAST RESULTS IN ANAIRCRAFT WHICH IS WITHIN MAXIMUM ZERO FUEL WEIGHT AND C.G. LIMITS. REFERENCE REVISED WEIGHT AND BALANCE. PERTINENT DETAILS OF THIS ALTERATION ON FILE AT SIERRA INDUSTRIES LTD UNDER WO #1155-10-2007.

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