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N882JH is Assigned

N-Number Entered: 882jh Aircraft Description
Serial Number 23056C Status Ineffect/Invalid
Manufacturer Name MAULE Certificate Issue Date 09/08/2015
Model M-7-235B Expiration Date 09/30/2028
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) 53023023
MFR Year 1999 Mode S Code (Base 16 / Hex) AC2613
Type Registration Corporation Fractional Owner NO
Registered Owner
Name SOUTHERN AIRCRAFT CONSULTANCY INC TRUSTEE
Street GLEBE COTTAGE COOKES RD
City BERGH APTON NFLK State
County Zip Code NR15 1AA
Country UNITED KINGDOM
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 LYCOMING Classification Standard
Engine Model IO-540 SER Category Normal
A/W Date 07/29/1999 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 T156669 Issue Date 09/08/2015 Expiration Date 10/08/2015
Fuel Modifications
Mod Code 28 Mod Date 19991015
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 ON 9-1-93 AND ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-ML-7-II, AF-ML-7-ID, AF-ML-7-FS, AF-ML-7-OI AND AF-TYP(S) 90. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIR-CRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, STRUCTURAL EVALUATION LETTER FROM APPRO- PRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT FURNISHED FUEL MANAGEMENT INSTRUC-TIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 11/11/99.

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