FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N132ME is Assigned

N-Number Entered: 132me Aircraft Description
Serial Number 18280690 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 05/01/2019
Model 182S Expiration Date 05/31/2029
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) 50101667
MFR Year 2000 Mode S Code (Base 16 / Hex) A083B7
Type Registration Individual Fractional Owner NO
Registered Owner
Name PENA JAIRO
Street 4411 SHARI CT
City CATHARPIN State VIRGINIA
County PRINCE WILLIAM Zip Code 20143-1004
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 3A13 Type Certificate Holder TEXTRON AVIATION INC
Engine Manufacturer LYCOMING Classification Standard
Engine Model IO-540 SER Category Normal
A/W Date 03/15/2000 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 20010713
INSTALLED ONE 60.0 US GALLON ALUMINUM FUEL TANK IN CABIN AREA FOR FERRY PURPOSES ONLY. EXTENDED RANGE FUEL TANK INSTALLED BY NORTHEAST AIR INC USING FOLLOWING DRAWINGS: NAI TVD003, NAI M020, NAI TF-001, NAI SC-001, NAI THD-003 AND INSTALLATION WAS PERFORMED PER NAI INSTAL-LATION INSTRUCTIONS 182S KIT. EXTENDED RANGE FUEL TANK PLACED ON WOOD-EN PLATFORM IN REAR PASSENGER SEAT LOCATION FUEL TANK SECURED TO THE AIRFRAME WITH (4EA) 2100 LB LIFT ALL LOAD HUGGER STRAPS. FUEL TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE. FUEL TANK IS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM EXTENDED RANGE TANK SUPPLIED TO AIRCRAFTFUEL SYSTEM BETWEEN AIRCRAFT FUEL SELECTOR AND FIREWALL BY ON-OFF VALVES, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. FUEL TANK IS VENTED OVERBOARD THROUGH A MANUFACTURED VENT ATTACHED TO UNDER SIDE OFRIGHT WING WITH LINE FORWARD FOR POSITIVE PRESSURE. EXTENDED RANGE FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION ANDWAS DETERMINED TO BE SATISFACTORY. FUEL SYSTEM INSTALLED IN ACCORDANCEWITH STANDARD PRACTICES FOUND IN AC 43.13-1B, AC 43.13-2A AND ACCEPTEDINDUSTRY PRACTICES. WEIGHT AND BALANCE FOR THIS EXTENDED RANGE FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATING INSTRUCTIONS AND THIS 337 ARE SUBMITTED TO THE FLIGHT CREW. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 8/11/01.

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