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:Lycoming_O-360
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Piper_PA-28_family
popular in the 1960s and 1970s
N-number
touring aircraft
private pilot license required
good performance in short fields
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gptkbp:avionics
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basic navigation equipment
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gptkbp:category
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general aviation
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gptkbp:climb_rate
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700 ft/min
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gptkbp:cockpit
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two-seat cockpit
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gptkbp:community
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active pilot community
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gptkbp:crew
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1 pilot
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gptkbp:design
|
Piper Aircraft design team
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gptkbp:engine_type
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gptkb:Lycoming_IO-540
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gptkbp:first_flight
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gptkb:1961
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gptkbp:fuel_capacity
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50 US gallons
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gptkbp:fuel_type
|
avgas
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gptkbp:height
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8 ft 6 in
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gptkbp:historical_significance
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popular among private pilots
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https://www.w3.org/2000/01/rdf-schema#label
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Piper 28-200
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gptkbp:is_often_used_in
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flight training
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gptkbp:landing_gear
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tricycle gear
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gptkbp:length
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26 ft 0 in
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gptkbp:maintenance
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relatively low maintenance costs
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gptkbp:manufacturer
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gptkb:Piper_Aircraft
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gptkbp:market
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private pilots
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gptkbp:max_speed
|
140 knots
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gptkbp:max_takeoff_weight
|
1,200 ft
2,800 lbs
1,500 ft
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gptkbp:modifications
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various aftermarket modifications available
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gptkbp:notable_battle
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used for flight training programs
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gptkbp:notable_features
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low-wing design
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gptkbp:operational_area
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moderate operating costs
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gptkbp:power_output
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1 × Lycoming IO-540-U2 A
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gptkbp:production_years
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1961-1977
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gptkbp:propulsion
|
constant-speed propeller
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gptkbp:range
|
800 nautical miles
suitable for cross-country flights
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gptkbp:safety_record
|
generally good safety record
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gptkbp:seating_capacity
|
3 passengers
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gptkbp:service_ceiling
|
14,000 ft
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gptkbp:speed
|
120 knots
60 knots
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gptkbp:successor
|
gptkb:Piper_PA-28-201_T
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gptkbp:supports
|
FAA certified
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gptkbp:surface
|
elevator, ailerons, rudder
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gptkbp:tail_type
|
N-number format
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gptkbp:type
|
single-engine aircraft
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gptkbp:values
|
stable resale value
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gptkbp:weight
|
3,200 lbs
1,700 lbs
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gptkbp:wing_area
|
174 sq ft
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gptkbp:wingspan
|
36 ft 0 in
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gptkbp:year_created
|
gptkb:1961
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