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N292BW is Assigned

N-Number Entered: 292bw Aircraft Description
Serial Number 20800403 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 04/17/2025
Model 208 Expiration Date 04/30/2032
Type Aircraft Fixed Wing Single-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50576426
MFR Year 2006 Mode S Code (Base 16 / Hex) A2FD16
Type Registration LLC Fractional Owner NO
Registered Owner
Name SKYLINE AVIATION SERVICES LLC
Street 4200 SW 149TH TER
City MIRAMAR State FLORIDA
County BROWARD Zip Code 33027-3337
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 P&W CANADA Classification Standard
Engine Model PT6A-114A Category Normal
A/W Date 04/07/2022 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 20070623
INSTALLED TEMPORARY AUXILLARY LONG RANGE FUEL TANKS IN ACCORDANCE WITHWINGS OF EAGLES INSTALLATION MANUAL WOE 208IM DATED 1/27/03, DRAWINGS NO WOE 208-1, WOE 3001, WOE 208FL, WOE 208VT SHEETS 1 AND 2, WOE 200A SHEET 1, WOE 250A SHEET 1, WOE 250-1 SHEET 2, WOE 200A SHEET 4 AND WOE 3001FP SHEET 8, ALL DATED 8/20/02, AC-43-13-1B AND INDUSTRY PRACTICES PERTAINING TO HARDWARE TNE FITTINGS. AUX TANKS HAVE BEEN PRESSURE TESTED TO 3.5 PSI AND FOUND TO BE SATISFACTORY FOR THE INTENDED INSTALLATION. STRUCTURAL SUBSTANTIATION WAS PROVIDED IN REPORT WOE 02-01 DATED JUNE 2002 AND APPROVED BY 8110-3 DATED 6/9/02 BY DERT 510375-CE. THE NEW WEIGHT AND BALANCE WAS COMPUTED AND PROVIDED TO THE PILOT. THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS IN ACCORDANCE WITH WICHITA ACO LETTER OF AUTHORIZATION DATED 2/10/88. THE FUEL SYSTEM HAS BEEN OPERATIONALLY CHECKED AND THE ENGINE RUNS ON ALL TANKS. THE FUEL SYSTEM HAS BEEN OPERATIONALLY CHECKED AND DOES NOT LEAK. THE PILOT HAS BEEN PROVIDED WITH AN AIRPLANE AUXILLIARY FUEL SYSTEM INSTRUCTIONS BOOKLET FOR THE PROPER OPERATION OF THE AUXILLIARY FUEL SYSTEM. UPON ARRIVAL AT THE DESTINA-TION LISTED ON THE FAA FORM 8130-7 FERRY PERMIT, THIS FIELD APPROVAL EXPIRES AND IS VOID. THE AIRCRAFT MUST BE RETURNED TO SERVICE AND THEAUXILLIARY FUEL SYSTEM REMOVED IN ACCORDANCE TO THE ATTACHED WOE 208RIREMOVAL INSTRUCTIONS.
Deregistered Aircraft
None
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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