ATP Electronics Piper Archer - Fuel System Differences; Performance & Weight Differences; System & Configuration Differences

172 & Archer Dierences • 53
1690
BEW
1640
2558
Max Ramp
Weight
2558
120
Max Baggage
Weight
200
2550
Max TOW
2550
55
Fuel Capacity
50
53
(Usable Fuel)
48
10 GPH
Approximate
Fuel Burn
10 GPH
Flaps 10
Cessna 172 Training Supplement page 14
Short Field
Takeo
Flaps 25
Piper Archer Training Supplement
page 17
Flaps 10
Cessna 172 Training Supplement page 15
Soft Field Takeo
Flaps 25
Piper Archer Training Supplement
page 18
62
Short Field
Approach Speed
66
General
Rudder Trim Installed
Stall horn tested during preight
Step only on non-skid surface when
entering & exiting aircraft.
Do not lean or hang on door, hinges will
bend or break easily.
Most performance charts displayed as
a table
Most performance charts displayed as
graphs
Electrically actuated; 0°, 10°, 20° & 30°
Flaps
Manual; 0°, 10°, 25° & 40°
Piper Archer Training Supplement page 3
When M BUS VOLTS falls below 20
volts, the standby battery system will
automatically supply electrical power to
the essential bus for at least 30 minutes.
(172S NAV III Manual, pg 3-17)
Standby Power
The Standby Attitude Indicator will
operate for approximately one hour
with the internal battery, depending on
battery condition at the time of power
failure.
(Piper Archer III Manual, pg 9-141)
Piper Archer Training Supplement page 8
Altimeter & Airspeed Indicator - Pitot
Static
Attitude Indicator - Vacuum
Standby
Instruments
Altimeter & Airspeed Indicator - Pitot
Static
Attitude Indicator - Standby Battery
Piper Archer Training Supplement pages
8 & 9
(55 Gallon Fuel Capacity) Approx 5.5 hrs
with 45 Minute Reserve
Endurance Prole
Cessna 172S NAV III - Model Years 2008+
Manual, page 5-23
Endurance @
55% Power
(Note: Can
be aected
considerably by
altitude, leaning,
power setting,
etc.)
Approx 4.5 hrs with 45 Minute Reserve
Endurance chart
Piper Archer III Manual, page 5-28