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==Specifications (1979 model PA-28-161 Cherokee Warrior II)==
==Specifications (1979 model PA-28-161 Cherokee Warrior II)==


{{Aircraft specs
{{aircraft specifications
|prime units? = imp
|plane or copter?=plane<!-- options: plane/copter -->
|plane or copter?=plane<!-- options: plane/copter -->
|jet or prop?=prop<!-- options: jet/prop/both/neither -->
|jet or prop?=prop<!-- options: jet/prop/both/neither -->
Line 9: Line 10:
|crew=one pilot
|crew=one pilot
|capacity=three passengers
|capacity=three passengers
⚫
|length ft=23.8
|payload main=
⚫
|payload alt=
⚫
|length main=23.8 feet
|length alt=
|length alt=
|span main=35.0 feet
|span ft=35.0
|span alt=
|span alt=
|height main=7.3 feet
|height ft=7.3
|height alt=2.25 m
|height m=2.25
|area main=170 sq ft
|wing area sqft=170
|area alt=
|wing area alt=
|airfoil=[[NACA]] 65<sub>2</sub>-415
|airfoil=[[NACA]] 65<sub>2</sub>-415
|empty weight main= 1340 lb
|empty weight lb= 1340
|loaded weight main= 2325 lb
|gross weight lb= 2325
|loaded weight alt= 1054.6 kg
|gross weight kg= 1054.6
|useful load main= 985 lb
|useful load main= 985 lb
|useful load alt=
|useful load alt=
|max takeoff weight main= 2325 lb
|max takeoff weight lb= 2325
|max takeoff weight alt= 1054.6 kg
|max takeoff weight kg= 1054.6
|more general= For Utility Category, Max Takeoff wt = 2020 lb.
|more general= For Utility Category, Max Takeoff wt = 2020 lb.
|engine (jet)=
|eng1 main=
⚫
|eng1 name=[[Lycoming O-320|Lycoming O-320-D3G or Lycoming O-320-D2A]]
|type of jet=
⚫
|eng1 type=[[Sensenich Propeller|Sensenich]] 74DM6-0-60 or 74DM6-0-58 propeller
|number of jets=
|eng1 number=1
|thrust main=
⚫
|eng1 hp= 160
|thrust alt=
⚫
|eng1 alt=
|thrust original=
|eng1 original=
|afterburning thrust main=
|afterburning thrust alt=
⚫
|engine (prop)=[[Lycoming O-320|Lycoming O-320-D3G or Lycoming O-320-D2A]]
⚫
|type of prop=[[Sensenich Propeller|Sensenich]] 74DM6-0-60 or 74DM6-0-58 propeller
|number of props=1
⚫
|power main= 160 hp
|power alt=
|power original=
|propeller or rotor?=propeller<!-- options: propeller/rotor -->
|propeller or rotor?=propeller<!-- options: propeller/rotor -->
|propellers=
|propellers=
|number of propellers per engine=
|number of propellers per engine=
|propeller diameter main=74 inches
|prop dia in=74 ches
|propeller diameter alt= 1.9 m
|prop dia m= 1.9
|max speed main= 126 knots
|max speed kts= 126
|max speed alt=
|max speed alt=
|cruise speed main= 118 knots
|cruise speed kts= 118
|cruise speed more = V<sub>NO</sub> (Max Structural Cruise): 126 KIAS, V<sub>A</sub> (Maneuvering Speed) (2325 lb GW): 111 KIAS, V<sub>FE</sub> (Max Flaps Extended Speed): 103 KIAS
|cruise speed note = V<sub>NO</sub> (Max Structural Cruise): 126 KIAS, V<sub>A</sub> (Maneuvering Speed) (2325 lb GW): 111 KIAS, V<sub>FE</sub> (Max Flaps Extended Speed): 103 KIAS
|stall speed main= 44 KIAS
|stall speed main= 44 KIAS
|stall speed alt=
|stall speed alt=
|never exceed speed main= 160 KIAS
|never exceed speed main= 160 KIAS
|never exceed speed alt= 153 KCAS
|never exceed speed alt= 153 KCAS
|range main= 574.7 nm (Best Economy Mixture, no Reserve, 5000 ft pressure altitude, [[international standard atmosphere|ISA]])
|range nmi= 574.7 (Best Economy Mixture, no Reserve, 5000 ft pressure altitude, [[international standard atmosphere|ISA]])
|range alt=
|range alt=
|range more=
|range note=
|combat radius main=
|combat range main=
|combat radius alt=
|combat range alt=
|combat radius more=
|combat range note=
|ferry range main=
|ferry range main=
|ferry range alt=
|ferry range alt=
|ferry range more=
|ferry range note=
|ceiling main= 14,300 feet
|ceiling ft= 14,300
|ceiling alt= 4400 m
|ceiling m= 4400
|climb rate main= 660 ft/min (at sea level, [[international standard atmosphere|ISA]])
|climb rate ftmin= 660 (at sea level, [[international standard atmosphere|ISA]])
|climb rate alt=
|climb rate alt=
|loading main=13.7 lb/sq ft
|wing loading main=13.7 lb/sq ft
|loading alt=66.89 kg/m<sup>2</sup>
|wing loading kg/m2=66.89
|thrust/weight=
|thrust/weight=
|power/mass main=14.5 lb/hp
|power/mass main=14.5 lb/hp

Latest revision as of 14:36, 28 March 2021

Specifications (1979 model PA-28-161 Cherokee Warrior II)

[edit]

Data from Piper Aircraft Owner's Handbook, Piper Part No. 761649, Revision 13, Oct 9, 1990[1]

General characteristics

  • Crew: one pilot
  • Capacity: three passengers
  • Length: 23.8 ft (7.3 m)
  • Wingspan: 35.0 ft (10.7 m)
  • Height: 7 ft 4 in (2.25 m)
  • Wing area: 170 sq ft (16 m2)
  • Airfoil: NACA 652-415
  • Empty weight: 1,340 lb (608 kg)
  • Gross weight: 2,325 lb (1,054.6 kg)
  • Max takeoff weight: 2,325 lb (1,054.6 kg)For Utility Category, Max Takeoff wt = 2020 lb.
  • Powerplant: 1 × Lycoming O-320-D3G or Lycoming O-320-D2A Sensenich 74DM6-0-60 or 74DM6-0-58 propeller, 160 hp (120 kW)
  • Propellers: 6 ft 3 in (1.9 m) diameter

Performance

  • Maximum speed: 145 mph (233 km/h, 126 kn)
  • Cruise speed: 136 mph (219 km/h, 118 kn) VNO (Max Structural Cruise): 126 KIAS, VA (Maneuvering Speed) (2325 lb GW): 111 KIAS, VFE (Max Flaps Extended Speed): 103 KIAS
  • Range: [convert: unknown unit] ([convert: unknown unit], [convert: unknown unit])
  • Service ceiling: 14,300 ft (4,400 m)
  • Rate of climb: 660 (at[convert: unknown unit]
  • Wing loading: 13.70 lb/sq ft (66.89 kg/m2)
  1. ^ Cite error: The named reference PA-28-161 POH was invoked but never defined (see the help page).
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