Piper PA-32-260-6 Cherokee Six
1963
Back to the Virtual Aircraft Museum
  SIX/SEVEN-SEAT CABIN MONOPLANEVirtual Aircraft Museum / USA / Piper  

PA-32 Cherokee Six

On 6 December 1963 Piper flew the prototype of a six-seat version of the PA-28 Cherokee, retaining the same general configuration but differing primarily by having a slight increase in wing span, the fuselage lengthened by 1.35m, and the installation of the 194kW Avco Lycoming O-540-E4B5 flat-six engine. Designated Piper PA-32-260-6 Cherokee Six, it was available initially in Standard, Custom, Executive and Sportsman versions with differing standards of installed equipment. By 1966 the company designation had changed to PA-32-260 and the Cherokee Six was then available as an optional six/seven-seat aircraft and, as the PA-32-300, with an optional 224kW IO-540-K engine, in 1971 Piper restyled the name to Cherokee SIX, but apart from annual product improvement, there were no changes until 1975 when a new version designated PA-32R-300 Cherokee Lance entered production to complement the Cherokee SIX, differing by introduction of a new fuselage structure and retractable tricycle landing gear. The 1978 version of the Lance had the conventional tail unit replaced by a T-tail, the designation then changing to PA-32RT-300 Lance II and, at the same time, a model with 224kW TIO-540-S1AD turbocharged engines became available under the designation PA-32RT-300T Turbo Lance II. Production of PA-32-260 Cherokee SIX ended in late 1978, the remaining version then being redesignated PA-32-300 SIX 300, but in the following year this also disappeared, together with the Lance II and Turbo Lance II. These aircraft were superseded by the six/seven-seat PA-32-301 Saratoga (the basic member of the new related family) which had an in-creased-span wing, reversion to a conventional tail unit, fixed tricycle landing gear, and a 224kW IO-540-K1G5D engine driving a constant-speed propeller. Made available simultaneously was the generally similar PA-32-301T Turbo Saratoga, which had a turbocharged version of the same engine, and the corresponding PA-32R-301 Saratoga SP and PA-32R-301T Turbo Saratoga SP which differed by having retractable tricycle landing gear. Only very low volume production continued into the early 1990s.

3-View 
PA-32RT Turbo Lance IIA three-view drawing of PA-32RT Turbo Lance II (1278 x 800)


Specification 
 MODELPA-32-301T Turbo Saratoga
 ENGINE1 x Avco Lycoming TIO-540-S1AD turbocharged flat-six piston engine, 224kW
 WEIGHTS
    Take-off weight1097 kg2418 lb
    Empty weight906 kg1997 lb
 DIMENSIONS
    Wingspan11.02 m36 ft 2 in
    Length8.59 m28 ft 2 in
    Height2.49 m8 ft 2 in
    Wing area16.56 m2178.25 sq ft
 PERFORMANCE
    Max. speed330 km/h205 mph
    Ceiling6095 m20000 ft
    Range1593 km990 miles

Comments 
THIVAN, sam21(@)sltnet.lk, 05.06.2007

send some information

Do you have any comments about this aircraft ?

Name    E-mail


COMPANY
PROFILE



All the World's Rotorcraft


Virtual Aircraft Museum


All rhe World's Rotorcraft AVIATION TOP 100 - www.avitop.com Avitop.com