Piper PA28R 200B

Piper PA28R 200B - Advanced Aircraft Data

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


Wing
Wing Location Bottom Wing
Wing Construction Spar Box Carry Through
Wing Rib Material Sheet Metal
Wing Skin Material Aluminum
--Aileron
Aileron Type Differential
Aileron Trim None
Aileron Control System Pully and Cable
--Flap
Flap Type Slotted
Wing Flap Actuation Manual


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


Landing Gear
Landing Gear Type Tricycle
Retractable Yes
Retraction System Hydralic/Electric
Emergency Extension Gravity Downlock
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 4
Heating Engine Exhaust Shroud
Window Defrost Ducted Hot Air
Cooling Ducted Ram Air


Profiles
Normal Climb Profile Speed (KIAS) 82
Maximum Climb Profile Speed (KIAS) 82
Engine
Number of Engines 1
Engine Manufacturer Lycoming
Engine Model IO-360-C1C
Engine Type Normally Aspirated Piston
Geared Direct Drive
Cooled Air Cooled
Fuel/Air Mechanism Fuel Injected
Number of Cylinders 4
Max HP 200
Starter System Electric Starter


Propeller
Propeller Manufacturer Hartzell
Propeller Model HC-C2YK-1/7666A-2
Number of Blades 2
Minimum Diameter
Maximum Diameter
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) 50
Tank Type 1 Location Inboard Wing
Tank Type 1 Capacity (G) 25
Tank Type 2 Location
Tank Type 2 Capacity (G) 0
Usable Fuel (G) 50
Oil Capacity (Quarts) 8


Electrical System
Power Source Engine Driven Alternator
Power Storage Battery
System Voltage 12
Alternator Amp 60
Battery Voltage 12
Battery Amp/Hour 35


Limitations
Maximum T/O Weight (lbs) 2600
Maximum LDG Weight (lbs) 2600
Standard Empty Weight (lbs) 1450
Useful Load (lbs) 1150
Station 1 Baggage Location Behind Last Row of Seats
Max Weight Station 1 (lbs) 200
Station 2 Baggage Location
Max Weight Station 2(lbs) 0
Station 3 Baggage Location
Max Weight Station 3(lbs) 0
Wing Loading (lbs/sq.ft) 16.3
Vne (KCAS) 153
Vno (KCAS) 144
Va(Max Gross) (KCAS) 0