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

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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