Avionics:
Garmin GNS530W NAV/COM/GPS
Garmin GNS430W NAV/COM/GPS
Terrain Modification Kits
KMD540
Garmin GMA340 Audio Panel
Garmin GTX330 Mode S Transponder
Sandel SN3500 Primary Navigation Display with Attitude Heading Reference System Sandel SG102 and additional Electronic compass (RH wing)
Bendix King KN63 DME Transceiver
Bendix King KDI572 DME Master Indicator
Bendix King KR87 ADF Receiver
Bendix King KI227 ADF Indicator
Bendix King KI256 Flight Director Indicator
Bendix King KI825 Horizontal Situation Indicator
Bendix King KI204-02 VOR/LOC Glidescope Indicator
Bendix King KEA346 Servoed Encoding Altimeter 50K Ft
Bendix KFC200 Autopilot with Flight Director
Bendix King KAS297 Altitude Preselector
Bendix-King KG102A Directional Gyro
L-3, SKY497 Stormscope Display
L-3, WX-1000E Stormscope Processor
Ameri-King AK350 2x Altitude Encoders, 30K Ft
MidContinent MD41-1468A Annunciation Control Unit
United Instruments 5934PAM-3 Altimeter 35K Ft
Ryan ATS8000 Traffic and Collision Alert Device
Shadin Fuel Flow Computer
Kannad 406AF ELT
Davtron Digital OAT / Volt Indicator.
Equipment:
Modification 262: 5.5 PSI differential pressure
Modification 264: 30,000 ft service ceiling.
According to Aerostar AMM, chapter 4, Airworthiness limitations: Limitation for Option 262 and 264, widshield and windows must be replaced at 9900 hours.
Aircraft approved for operation at 30,000 ft ceiling
Inconal exhausts and tail pipe (allows higher TIT)
Inconel front EXHAUST SYSTEM SERVICE BULETIN 600-123 carried out 12/03/97
Six puck heavy duty brakes, (3 brake calipers on each wheel, important for operation on short runways)
Dual Three piston caliper brake conversion kit installed.
FIKI certified per Flight Manual Supplement 17,
Ice protection system,
Approved for flight into known icing condition.
Machen pneumatic door seal pressure system 65-30 S.N.65-30-020.
Oil Breather Recovery System, Machen 62-1.2 option two, optional oil breather separator
Oil Scavenge Pumps
Air conditioning
De-Ice system
Oxygen Cylinder
Machen Aux Tank
Vortex Generators
Aircraft Cover
Exterior:
White with red blue and light blue accents. Condition 7/10
.
Interior:
Beige and red leather interior, 6 seats
Courtesy table.
Condition 7/10
Other comments:
For sale as is as project, where is, disassembled and out of annual inspection
Last time flown in 2009
Specifications subject to verification by purchaser.
PA-60-602P
Airframe S/N: 60-8265046
Total Time: 3040:31
Engines Lycoming TIO-540-U2A (350 hp), factory intercooled engines.
LH Side, S/N: L-2052-61A
TT: 6555:25
TSOH: 96:25
Overhauled in June 2009 with new crankshaft as the original one was affected by an FAA AD. Invested 132,0000 Swiss Francs
RH Side, S/N: L-238-61A
TT: 10283:55
TSOH: 511
Overhauled in 2003
Propellers Hartzell HC-C3YR-2UF
LH Side, S/N: CK4693A
TSOH: 96:25
Overhauled by Hoffmann Propeller, Germany on 28 September 2007 with new blades, invested 21,000 Swiss Francs, Installed in 2009
New Hub installed in 2001
RH Side, S/N: CK3571A
TSOH: 423:07
Overhauled with governor in 2003
For sale as is, where is, out of annual inspection, as project
Currently disassembled for transportation, removed engines, propellers, wings, horizontal stabilizer
Previously registered N566DC
Piper PA-60-602P Aerostar/Superstar 700 (700 Horse Power)
Pressurized 6 seat aircraft
Total Fuel Capacity. 218.5 USG (2 wing tanks x 65 USG, One 43.5 USG Fuselage Auxiliary Tank, One Mach 45 USG Fuselage Tank
