N55804 Piper Arrow

Note: The information on this page may not be accurate or current and is not valid for navigation, flight planning, or for use in flight.

Facts and Figures

Model Piper Arrow II
Year 1973
Engine Lycoming IO-360-C1C
Horsepower 200 bhp @2700 RPM
Oil Capacity 8 qts
Propeller Constant Speed
Useable Fuel 48 gal (2 gal unusable)
Cruise Speed (2,000') 156 mph, 135 KTAS @75% pwr
Cruise Speed (8,000') 170 mph, 148 KTAS @full pwr
Cruise Range 780 nm @65% power
Climb Rate (SL) 900 fpm
Max Demonstrated X-Wind 20 kts
Takeoff Distance (SL, std temp, gross wt, 25o flaps) 770'; 1600' over 50' obstacle
Landing Distance (SL, std temp, gross wt, full flaps) 780'; 1,380' over 50' obstacle
Stall Speed 56 KIAS full flaps
Max Weight 2650 lbs
Empty Weight 1644 lbs
People/Baggage payload 716 lbs, w/full fuel (300 lbs)

Avionics

NAV/COMM/GS #1 Garmin 430 with nav/GS indicator
NAV/COMM/GS #2 King KX155 with nav/GS indicator
DME King KN-64
Transponder Garmin GTX-327
Audio Panel/Intercom PSI-PMA8000
GPS Garmin 430 GPS - IFR cert
Autopilot Century IIB can track Nav1, Nav2, or GPS
Engine Monitor JPI EDM-700

IFR Configuration Chart

Configuration Manifold RPM Attitude/Pitch KIAS VSI
Climb 25" Full 7.5o up 90 kt 800 fpm up
Cruise 23.5" 2350 0 125 kt 0
Cruise Descent 20" 2000 2.5o down 130 kt 500 fpm down
Approach Level - gear up 20" 2400 3o up 107 kt 0
Approach Level - gear down 22" 2400 4o up 90 0
Precision Approach Descent
10o Flaps
15" 2400 5o down 90 kt 500 fpm down
Non-precision Approach Descent
10o Flaps
15" 2000 5o down 90 kt 800 fpm down

Other Information