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N400BS is Assigned

N-Number Entered: 400bs Aircraft Description
Serial Number 421C1089 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 12/13/2023
Model 421C Expiration Date 12/31/2030
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) 51126313
MFR Year None Mode S Code (Base 16 / Hex) A4ACCB
Type Registration Corporation Fractional Owner NO
Registered Owner
Name MB AVIATION INC
Street 8800 STRIPER CV
City LARUE State TEXAS
County HENDERSON Zip Code 75770-4975
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 Unknown Classification Standard
Engine Model Unknown Category Normal
A/W Date 07/23/1981 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
Certificate Number T234093 Issue Date 12/13/2023 Expiration Date 01/12/2024
Fuel Modifications
Mod Code 28 Mod Date 19900616
INSTALLED A TEMPORARY FERRY FUEL TRANSFER SYSTEM PER VKV-CESSNA 421 DATA. CABIN INSTALLATION FEEDS INTO PREVIOUSILY INSTALLED FUEL PROVISIONS AS SHOWN IN AIRCRAFT LOG BOOK. CABIN FUEL TRANSFER SYSTEM SUPPLIES FERRY FUEL INTO WING MAIN TANKS. SYSTEM TRANSFERS BY CABIN PRESSURIZATION. A BACK UP PUMP IS PROVIDED IN EVENT OF ELECTRICAL FAILURE OR PRESSURIZATION PROBLEMS. INSTALLATION COMPLIES WITH AC 43.13-1A TECHNIQUES SHOWN FOR FUEL SYSTEM AND ATTACH POINT REQUIREMENTS. MIL-E-1605K, MIL-0E-15997A, AND QQR-566 SPERCIFICATIONS ADHERED TO. SYSTEM PRESSURE TESTED. SYSTEM TO BE FLIGHT TESTED AND RESULTS ENTERED INTO AIRCRAFT RECORDS.

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