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N104WP is Assigned

N-Number Entered: 104wp Aircraft Description
Serial Number 34-7870048 Status Valid
Manufacturer Name PIPER Certificate Issue Date 10/13/2021
Model PA-34-200T Expiration Date 10/31/2028
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) 50012622
MFR Year 1977 Mode S Code (Base 16 / Hex) A01592
Type Registration Individual Fractional Owner NO
Registered Owner
Name MARTYN CHRISTIAN A
Street 1835 E HALLANDALE BEACH BLVD
STE 236
City HALLENDALE State FLORIDA
County BROWARD Zip Code 33009
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 TSIO-360 SER Category Normal
A/W Date 11/15/1977 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 T218940 Issue Date 10/13/2021 Expiration Date 11/12/2021
Fuel Modifications
Mod Code 28 Mod Date 20110714
THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL CONSISTING OF 2 ALUMINUM FERRY FUEL TANKS, A FUEL SELECTOR VALVE MANIFOLD AND ASSOCI- ATED FERRY FUEL FEED LINES FITTINGS AND VENT SYSTEM. THIS SYSTEM IS USED IN CONNECTION WITH THE NORMAL AIRCRAFT FUEL BOOST PUMPS. THE FUELLINES ARE ROUTED FROM THE FERRY FUEL TANK TO INDIVIDUAL FERRY FUEL SELECTOR VALVES AND THEN TO THE TEE FITTING INSTALLED IN THE AIRCRAFT FUEL LINES, BETWEEN THE LEFT AND RIGHT FUEL SELECTOR VALVES AND THE LEFT AND RIGHT BOOST PUMPS. THERE IS A VENT FITTING INSTALLED IN THE LOWER FUESELAGE TO ALLOW POSITIVE VENT PRESSURE TO THE 2 FERRY FUEL TANKS. THE 2 FERRY FUEL TANKS ARE MOUNTED ON PALLETS ACROSS THE SEAT RAILS, CENTER SECTION FLOORING AND SECURED BY 6 PIPER RAIL TYPE CARGO RINGS, ON THE FORWARD SEAT RAILS AND 4 SEATBELTS ATTACH FITTINGS IN THE REAR OF THE AIRPLANE. ADJUSTABLE CARGO STRAPS ARE USED TO SECURE THE FORWARD AND REAR TANKS. THE TANKS ARE BONDED TO THE FUSELAGE FOR GROUNDING. THIS SYSTEM ALLOWS NORMAL OPERATION OF THE AIRCRAFT FUEL FEED SYSTEM TO THE ENGINE, WITH EITHER THE AIRCRAFT MAIN TANKS OR THE FERRY FUEL TANKS. OTHER MODIFICATIONS TO THE AIRCRAFT TO ACCOMMODATE THE FERRY FUEL SYSTEM ARE THE REMOVAL OF THE COPILOTS SEAT AND SEATS 3,4,5 AND 6 TO ACCOMMODATE THE FERRY FUEL TANKS. ADDITIONALLY THERE ISA TEMPORARY OIL REPLENISHING SYSTEM INTALLED. THE OIL SYSTEM CONSISTS OF A HAND OIL PUMP, OIL SUPPLY LINES, A LEFT AND RIGHT SELECTOR MANIFOLD ND VALVES, SUPPLY LINES THAT FEED TO CAPS INSTALLED ON BOTH OIL FILLER NECKS WITH SUPPLY FITTINGS INSTALLED. THESE 2 SYSTEMS ARE REQUIRED TO EXTEND THE RANGE FOR THE FLIGHT FROM NORTH LAS VEGAS, NV

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