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55804 - Piper Arrow II

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.  Some pictures are "clickable" to view high resolution images.

55804 Facts & 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, 25
o  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)

Installed 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/Marker Bcn  King
GPS Garmin 430 GPS - IFR cert
Autopilot Century IIB can track Nav1, Nav2, or GPS
Intercom Sigtronics SPA400 - 4 place
Engine Monitor JPI EDM-700 (web site)
Pilots User Guide (4MB)

JPI EzPlot software

 

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 107kt

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 Info:


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Last updated: 05/31/07.