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Archer and Seminole POH

PA-28 and PA-44
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Nohryk
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Last updated: March 25, 2026
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First submittedJanuary 25, 2026
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Piper Archer
Answer
Chapter 1
General
Wing Span (ft)
35.5
Engine Model #
IO-360-B4A
Engine Manufacturer
Lycomming
Engine Specs
4 cylinder
-
horizontally opposed
-
air cooled
-
naturally aspirated
-
direct drive
Alternator Volts
28
Battery Volts
24
Takeoff Power (hp)
180
Takeoff RPM
2700
Propeller Manufacturer
Sensenich
Propeller Diameter Max. (in)
76
Propeller Diameter Min. (in)
76
Max. Fuel Capacity (gal)
50
Usable Fuel (gal)
48
Min. Octane Fuel
100 / 100LL
Max. Oil Capacity (qt)
8
Max. Demonstrated Crossinwd (kts)
17
Max. Ramp Weight (lbs) (Normal Category)
2558
Max. Takeoff Weight (lbs) (Normal Category)
2550
Max. Landing Weight (lbs) (Normal Category)
2550
Max. Weight in Baggage Area (lbs) (Normal Category)
200
Max. Ramp Weight (lbs) (Utility Category)
2138
Max. Takeoff Weight (lbs) (Utility Category)
2130
Max. Landing Weight (lbs) (Utility Category)
2130
Max. Weight in Baggage Area (lbs) (Utility Category)
0
Chapter 2
Limitations
Vne
154
Vno
125
Vo (at 2550 lbs)
113
Vo (at 1917 lbs)
98
Vfe
102
Red Line
154
Yellow Band
125-154
Green Band
50-125
White Band
45-102
Max. Oil Temperature
245
Min. Oil Pressure (psi)
25
Max. Oil Pressure (psi)
115
Alternator Amps
70
E-Battery Min. Volts
23.3
Positive Load Factor (Normal Category)
3.8
Negative Load Factor (Normal Category)
-1.5
Positive Load Factor (Utility Category)
4.4
Negative Load Factor (Utility Category)
-1.7
Chapter 7
Aircraft & Systems
Aspen Battery Life
30 min
G5 Battery Life
4 hours
Chapter 8
Handling, Service & Maintenance
Nose Gear Tire Pressure (psi)
18
Main Gear Tire Pressure (psI)
24
Strut Type
air-oil / oleo
Wheel Ply
4
Piper Seminole
Answer
Chapter 1
General
Wing Span
38 ft 6.6 in
Left Engine Model #
IO-360-B1G6
Right Engine Model #
LIO-360-B1G6
Rated HP
180
Rated RPM
2700
Straight Propeller Diameter Max. (in)
74
Straight Propeller Diameter Min. (in)
72
Straight Propeller Type
constant speed
-
hydraulically actuated
-
full feathering
Scimitar Propeller Diameter Max. (in)
74
Scimitar Propeller Diameter Min. (in)
72.5
Scimitar Propeller Type
constant speed
-
hydraulically actuated
-
full feathering
Fuel Capacity (gal)
110
Usable Fuel (gal)
108
Minimum Octane
100 / 100LL
Oil Capacity (qt)
8
Max. Ramp Weight (lbs)
3816
Max. Takeoff Weight (lbs)
3800
Max. Landing Weight (lbs)
3800
Max. Weight in Baggage Area (lbs)
200
Chapter 2
Limitations
Vne
202
Vno
169
Vo at 3800
135
Vo at 2870
115
Vle
140
Vlo (extending)
140
Vlo (retracting)
109
Vfe
111
Vyse
88
Vmca
56
Upper Red Line
202
Yellow Band
169-202
Green Band
57-169
White Band
55-111
Blue Line
88
Lower Red Line
56
Max. Manifold Pressure
full throttle
Max. Cylinder Head Temperature
500
Max. Oil Temperature
245
Min. Oil Pressure
25
Max. Oil Pressure
115
Alternator Max. Amps (Ground)
60
Alternator Max. Amps (Flight)
65
Battery Min. Volts
25
Battery Max. Volts
32
E-Battery Min. Volts (Ground)
20
E-Battery Min. Volts (Flight)
23.3
E-Battery Max. Volts
32
Positive Load Factor (no flaps)
3.8
Positive Load Factor (with flaps)
2
Negative Load Factor
-1.5
Chapter 3
Emergency Procedures
Vxse
82
Chapter 4
Normal Procedures
Vy
88
Vx
82
Vsse
82
Max. Demonstrated Crosswind
17
Chapter 7
Aircraft & Systems
Aspen Battery Life
30 min
G5 Battery Life
4 hours
Chapter 8
Handling, Service, & Maintenance
Main Tire Ply
8
Nose Tire Ply
6
Strut Type
air-oil / oleo
Minimum Safe Oil (qt)
2
Main Gear Pressure (psi)
55
Nose Gear Pressure (psi)
50
Archer
Spin Recovery
Rudder opposite
full forward
ailerons neutral
throttle idle
rudder neutral
smooth back pressure
Engine Fire On Start
start switch continue cranking
mixture idle
throttle full
fuel pump off
fuel selector off
evacuate
extinguish
Engine Failure On Takeoff (Sufficient Runway)
safe airspeed
land straight ahead
brakes as needed
(Insufficient Runway)
safe airspeed
flaps as needed
shallow turns
(Sufficient Alt. For Restart)
airspeed 76
fuel selector switch tanks
fuel pump on
mixture rich
alt air open
land power off
mayday
secure
Engine Fire In Flight
fuel selector off
throttle idle
mixture idle
fuel pump off
heat defrost off
emergency descent
Electrical Fire In Flight
E battery arm
battery off
alternator off
vents open
heat defrost off
extinguish
emergency descent
Emergency Descent
throttle idle
flaps as needed
no flaps 125
flaps 102
bank 45
Engine Failure In Flight
airspeed 76
locate landing area
fuel selector switch tanks
fuel pump on
mixture rich
alt air open
left mag off then on
right mag off then on
mayday
secure
Seminole
Engine Fire During Start
mixture idle
throttle full
starter continue to engage
fuel selectors off
fuel pumps off
extinguish
evacuate
Engine Fire In Flight
affected engine
fuel selector off
throttle idle
prop feather
mixture idle
cowl flaps open
secure
emergency descent
land as soon as possible
Electrical Fire
e battery arm
battery off
alternators off
vents closed
cabin heat off
extinguish
manual gear
land as soon as possible
Emergency Descent
alt air open
throttles idle
props full
mixture as required
below 140 gear down
airspeed 135
bank 45
Engine Failure - Takeoff (Below 75 or Gear Down)
throttles idle
brakes as required
directional control maintain
(Insufficient Runway)
brakes maximum
mixtures idle
fuel selectors off
mags off
battery off
directional control maintain
obstacles avoid
Engine Failure - Takeoff (Above 75, Sufficient Runway))
gear verify down
land straight ahead
directional control maintain
throttles idle
brakes as required
(Gear in Transit or UP, and Continuing)
directional control maintain
airspeed at least 88
mixture full
props full
throttles full
flaps up
gear up
fuel selectors on
fuel pumps on
inop engine identify and verify
inop throttle idle
inop prop feather
inop mixture idle
bank 2, 3 into op engine
climb speed 88
inop cowl flaps closed
inop mags off
inop fuel pump off
inop alternator off
inop fuel selector off
land as soon as practical
Engine Failure In Flight
airspeed 88
directional control maintain
mixture full
props full
throttles full
gear up
flaps up
inop engine identify and verify
Fix - Before Securing Engine
fuel quantity check
fuel selector on, cross feed
fuel pump on
mixture full
alt air open
inop left mag off then on
inop right mag off then on
oil temperature check
oil pressure check
Feather
secure
On Operating Engine
power as required
fuel selector on
fuel pump as required
cowl flap as required
bank 2, 3 into op engine
airspeed at least 88
electrical load reduce
land as soon as practical
Spin Recovery
throttles idle
rudder opposite
full forward
ailerons neutral
rudder neutral
smooth backpressure
Performance
 
Condition
FPM loss
gear down / flaps up
250
gear down / flaps 25
490
gear down / flaps 40
525
windmilling and gear / flaps up
200
Autopilot Limitations
 
must be disengaged:
during takeoff and landing
min. altitude engaged:
400 during takeoff
-
1000 during cruise and descent
-
200 during approach
min. airspeed engaged:
90 during approach
-
80 all other times
max. airspeed engaged:
190
max. fuel imbalance:
10
Prohibited for:
coupled OEI go around
max. autopilot engage limits:
pitch +-50
-
roll +-75
If stall warning system is inop:
USP will not activate in altitude critical modes
autopilot approved for:
cat 1 precision and non precision
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