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N-Number Inquiry Results

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N669RP is Assigned

N-Number Entered: 669rp Aircraft Description
Serial Number E-1618 Status Valid
Manufacturer Name BEECH Certificate Issue Date 07/03/2002
Model A36 Expiration Date 10/31/2027
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) 52153455
MFR Year 1979 Mode S Code (Base 16 / Hex) A8D72D
Type Registration Individual Fractional Owner NO
Registered Owner
Name FANNING WILLIAM J
Street 6631 CAMILLE AVE
City DALLAS State TEXAS
County COLLIN Zip Code 75252-5484
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 520 SERIES Category Utility
A/W Date 11/28/1979 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 T147278 Issue Date 09/19/2014 Expiration Date 10/19/2014
Fuel Modifications
Mod Code 28 Mod Date 20070720
INSTALLED J.L. OSBORNE WING TIP TANKS KIT IAW STC SA4-1629 USING J.L. OSBORNE WING TIP TANK INSTALLATION INSTRUCTIONS 11993 FOR BEECH MODELS36, A36 AND A36TC. THE SYSTEM WAS FUNCTION TESTED IN ACCORDANCE WITH J.L. OSBORNE CONTINUED AIRWORTHINESS INSTRUCTIONS, P.N 668-7-8. THESEINSTRUCTIONS WERE ADDED TO THE MAINTENANCE MANUAL FOR THIS AIRCRAFT. THE AIRCRAFT POH WAS AMENDED WITH AN FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT DATED APRIL 15, 1992. THIS AIRCRAFT WAS RE-WEIGHED AND THE WEIGHT AND BALANCE FORMS WERE SUPERCEDED AND AMENDED. A COPY OF THIS FORM 337 IS NOT REQUIRED TO BE CARRIED IN THE CABIN OF THIS AIRCRAFT IN ACCORDANCE WITH FAR PART 43, APPENDIX B, PARAGRAPH D.

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