Airplane time state
Airframe sn 24-4048.
Lycoming IO-540 260 hp engine, TSOH: 1015 hrs
160 hrs since Top overhaul with Millennium cast iron cylinders.
Engine overhauled in 1984 by Bosio
Fuel injection system overhauled Nov. 2014
All compressions around 78/80
New iridium fine wire spark pluts installed in Nov. 2014
Two blade propeller. Last overhaul 05/2009.
Window plastic frames replaced in 2003.
White and metallic gray with red stripe.
Repainted in 2003.
King KMA24 Audio Panel with Marker Beacon
2 x King KX165 NAV-COM 760 Channels, FM Immune
Garmin 100 GPS
King KR87 Digital ADF
King KT76A Mode C Transponder
Shadin digital fuel flow
JPI 700 engine analyzer
70 Amp alternator. Replaced in 2010
406 MHz ELT
Empennage reinforcement kit
Recent stainless steel exhaust collector pipes
Door top lock improvement kit
M20 engine breather oil separator
Omaco sound proofing
1/8th inch windows replaced in 2003.
Gami fuel injector nozzles
4 new fuel cells replaced 05/2013.
Electric fuel pump recently replaced.
Ignition harness replaced in 2010.
Engine oil and fuel hoses replaced in 2010.
Last 1000 hrs inspection performed at TT: 1884
Last 500 hrs inspection performed at TT: 2107
Annual inspection and ARC performed 5/2014
Total fuel capacity 90 USG
MTOW: 1315 kg (2900 lbs)
NO CO-PILOT BRAKES!
Italian Luxury Tax not applicable due to aircraft age category!
Specification subject to verification by purchaser.
Complete Logbooks are available.
|Model Series:||piper comanche|
|Fuel Efficiency (mpg US):||14.5|
|Per Seat Efficiency:||58|
|Wing Loading lb/sq ft:||16.3|
|Power Loading lb/hp:||11.2|
|External Length (FT):||25|
|External Height (FT):||7.5|
|External Span (FT):||36|
|Internal Length (Overall/Net Height):||108 IN|
|Internal Width (Max/Floor):||45 IN|
|Internal Height:||47 IN|
|Baggage Area 1 Cubic Feet / Lbs:||20 CU FT / 200 LBS|
|Max Takeoff Weight (LBS):||2900|
|Empty Weight-BOW (LBS):||1700|
|Useful Load (LBS):||1200|
|Max Fuel (LBS):||360|
|Max Fuel (Gallons):||60|
|Avail Payload Max Fuel (LBS):||840|
|TO Distance (SL @ ISA) FT:||660|
|Landing Distance (FT):||650|