Piper PA32 300 Cherokee 6 B Model

Piper PA32 300 Cherokee 6 B Model - Advanced Aircraft Data

AirFrame
Fusulage Construction Semimonocoque
Airframe Material All-Metal
Number of Doors 2


Wing
Wing Location Bottom Wing
Wing Construction Full Cantilever
Wing Rib Material Sheet Metal
Wing Skin Material Aluminum
--Aileron
Aileron Type Differential
Aileron Trim Manual
Aileron Control System Pully and Cable
--Flap
Flap Type Plain
Wing Flap Actuation Manual


Empennage
Empennage Type Conventional
Empennage Rib Material Sheet Metal
Empennage Skin Material Aluminum
Rudder Trim Cable Link Trim Tab
Yaw Trim Actuator Manual
Yaw Control System Cable and Pully
Pitch Trim Cable Link Trim Tab
Pitch Control System Cable and Pulley
Pitch Trim Actuator Manual


Landing Gear
Landing Gear Type Tricycle
Retractable No
Retraction System N/A
Emergency Extension N/A
Ground Steering Rudder Pedals
Shock Absorbtion Main Gear Oil/Air Strut
Shock Absorbtion Other Gear Nosewheel Air/Oil Strut
Brake Type Hydraulic Actuated Brake Disc
Brake Controls Toe Brakes


Cabin
Instrument Panel IFR non Glass
Flight Control Ram Horn Yoke
Number of Seats 6
Heating Engine Exhaust Shroud
Window Defrost Ducted Hot Air
Cooling Ducted Ram Air


Profiles
Normal Climb Profile Speed (KIAS) 91-100
Maximum Climb Profile Speed (KIAS) 82
Engine
Number of Engines 1
Engine Manufacturer Lycoming
Engine Model IO-540-K1A5
Engine Type Normally Aspirated Piston
Geared Direct Drive
Cooled Air Cooled
Fuel/Air Mechanism Fuel Injected
Number of Cylinders 6
Max HP 300
Starter System Electric Starter


Propeller
Propeller Manufacturer Hartzell
Propeller Model
Number of Blades 3
Minimum Diameter
Maximum Diameter 80
Propeller Type Constant Speed
Propeller Governor Oil Pressure


Fuel System
Fuel System Type Fuel Pump
Approved Fuel Type 1 100LL
Approved Fuel Type 2 100/130
Approved Fuel Type 3
Fuel Capacity (G) 84
Tank Type 1 Location Left Wing
Tank Type 1 Capacity (G) 42
Tank Type 2 Location Right Wing
Tank Type 2 Capacity (G) 42
Usable Fuel (G) 83.5
Oil Capacity (Quarts) 12


Electrical System
Power Source Engine Driven Alternator
Power Storage Battery
System Voltage 12V
Alternator Amp 60amp
Battery Voltage 12V
Battery Amp/Hour


Limitations
Maximum T/O Weight (lbs) 3400
Maximum LDG Weight (lbs) 3400
Standard Empty Weight (lbs) 1968
Useful Load (lbs) 1432
Station 1 Baggage Location 178.7
Max Weight Station 1 (lbs) 100
Station 2 Baggage Location 42
Max Weight Station 2(lbs) 100
Station 3 Baggage Location
Max Weight Station 3(lbs) 0
Wing Loading (lbs/sq.ft) 19.5
Vne (KCAS) 184
Vno (KCAS) 146
Va(Max Gross) (KCAS) 129