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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Piper_PA-28-201
gptkb:Piper_PA-28-235
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gptkbp:aircraft_operated
|
Light Aircraft
low-wing
15 lb/sq ft
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gptkbp:avionics
|
basic VFR avionics
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gptkbp:category
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gptkb:General_Aviation
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gptkbp:climb_rate
|
1,000 ft/min
|
|
gptkbp:cockpit
|
two-seat cockpit configuration
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|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
Piper Aircraft design team
Training and personal use
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gptkbp:engine
|
300 hp
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gptkbp:engine_type
|
gptkb:Lycoming_IO-540
|
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gptkbp:first_flight
|
gptkb:1961
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|
gptkbp:fuel_capacity
|
50 US gallons
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gptkbp:fuel_type
|
Avgas 100 LL
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gptkbp:height
|
8 ft 6 in
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-28-236
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|
gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
24 ft 0 in
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|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:market_segment
|
Private and training market
|
|
gptkbp:material
|
metal and composite construction
|
|
gptkbp:max_speed
|
135 knots
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gptkbp:max_takeoff_weight
|
2,550 lb
65 knots
|
|
gptkbp:notable_users
|
gptkb:aircraft
Private Owners
Flying Schools
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|
gptkbp:power_consumption
|
8 lb/hp
|
|
gptkbp:produced_by
|
over 32,000 units
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|
gptkbp:production_years
|
1961-1984
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gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
600 nautical miles
|
|
gptkbp:safety_record
|
generally good safety record
|
|
gptkbp:seating_capacity
|
gptkb:3
|
|
gptkbp:service_ceiling
|
14,000 ft
|
|
gptkbp:speed
|
120 knots
55 knots
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
single-engine aircraft
|
|
gptkbp:variant
|
gptkb:PA-28-201
gptkb:PA-28-235
gptkb:PA-28-161
|
|
gptkbp:weight
|
1,500 lb
1,050 lb
|
|
gptkbp:wing_area
|
174 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|