Piper PA-28R-200 Arrow N3811M Photos

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  • Congratulation to Heath Burlando - G1000 Course
  • Congratulation to Mark Hewitt - G1000 course winner
  • Congratulation to Timothy Miller - Instrument Rating
  • Congratulation to Scott Crossen- Private Pilot
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  • Congratulation to Steve Weiner – Sport Pilot
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  • Congratulation to Neal Van Den Langenberg - First Solo
  • Congratulation to Tim Crowe - Private Pilot
  • Congratulation to Scott Crossen - re-solo after having to stop 8 years ago
  • Congratulation to Sam Mogren - Private Pilot
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Piper PA-28R-200 Arrow N3811M Photos

 

Image caption.

 

 

 

Overview

The ideal complex training platform

 The Piper Arrow is the only complex trainer available for purchase direct from an OEM. The Arrow offers an ideal classroom in the sky for complex, single engine training at a price that is manageable for the smallest of flight schools. Thousands are in service around the world, so your choice of the Piper Arrow for your training needs is a wise one.

Performance

  PA-28R-200
Maximum Cruise Speed 170 ktas
Maximum Range  1 880 nm
Takeoff Distance (S.L., ISA, MTOW)  2 1,600ft
Ground Roll 1,000ft
Landing Distance (S.L., ISA, MLW) 1,520ft
Ground Roll 620ft
Maximum Operating Altitude 16,200 ft
Maximum Climb Rate (Sea Level) 600fpm
VNE 214kias
Stall Speed 65kcas

1 45 minute Fuel Reserves, 75% Power @ 12,000 ft.
2 Distance to 50 feet above the runway.

 

Avionics

Coming soon.

 

Powerplant

Lycoming
IO-360-C1C6, 200 hp

 

PA-28R-200 Arrow Weight and Balance Calculator



General Weight and Balance
Required Data Entry
StationWeightArm Moment/1000Information
Empty Weight  
Max Takeoff Weight (MTOW)     Useful Load
Pilot/Front Passenger Seat position range
Rear Passengers Arm is stationary
Cabin Bags Arm Of Bags
Compartment Bags Arm Of Bags
Fuel Quantity
Useable
US Gallons (Total)

   
Ramp ConditionCalculated
 Calculated
Calculated Potential
Useful Load
Remaining
Calculated Center Of Gravity
Disclaimer: USE AT YOUR OWN RISK!
The pilot is solely responsible for accurate weight and balance calculation of his aircraft



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