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With the photo shoot over we broke away from the Basset and set
the Archer up for the cruise. A very handy feature is that the recommended
power settings for various flight levels are printed on the back
of the pilot's sun visor. Due to a variety of rather tedious reasons
it was decided that I would fly the Archer directly back to Conington,
which was where the car was - Today's Pilot photographer Steve Fletcher
and myself having flown down to Cranfield from Conington in the
Basset earlier that morning. My accomplice for the afternoon, Neil
Plumb, would then return the aircraft back to its Cranfield base.
As we cruised back towards Conington I must say that the Archer
was beginning to grow on me. As already observed, the aircraft is
aimed at the same corner of the market as the Cessna 172, and in
many ways displays similar handling traits and performance figures.
Handling, while not sparkling, is stolid and safe, while respectable
cruise speeds and fuel flows are achieved without the complexity
and additional expense of a constant-speed propeller or a retractable
undercarriage. As with any flying machine, the Archer is best evaluated
when being flown as it was intended to be flown. The less-than-ideal
handling characteristics it displayed when flying formation would
probably never even become apparent to most pilots. It's essentially
a light tourer, good for carrying up to three people and their baggage
over a reasonable distance, or four people and bags but over a reduced
range. So, taken in this context, how do I rate it? Actually, for
doing the job that it was designed to do, quite highly.
Owing to time constraints it was not possible to explore the slow
speed side of the envelope. However, I see from the notes that I
made the last time I flew an Archer, that I found its stall behaviour
- either flaps up or flaps down - perfectly benign, with plenty
of buffet before the wing finally quits flying, and no tendency
to drop a wing. In common with many other American-designed light
aircraft of the 1960s, the Cherokee Archer has been designed with
the average pilot in mind. It has no peculiar traits or unpleasant
vices.
As we slipped into the circuit at Conington I began to reduce power
while holding a steady altitude and waited for the airspeed to slip
back into the white arc. Three flap settings are available; 10,
25 and 40 degrees. Speed control all round the circuit was easy,
and with absolutely no fuss the Archer slid down the approach and
rolled its tyres onto the tarmac just past the numbers.
There are probably around 1,000 of the various types of PA28 on
the UK register, and it was interesting to note that while taxiing
out at Cranfield and back in at Conington I didn't need to look
very hard before I could spot at least a couple of Cherokees. Perhaps
that simple fact says more about how successful the series has been
than I ever could.
HIstory
First flown more than 40 years ago, I doubt that Piper really
expected back then that production of its venerable PA28 series
would continue into the 21st century. The prototype four-seat Piper
PA28-150 Cherokee made its maiden flight on January 14, 1960, and
although it has undergone a considerable number of changes, the
basic aircraft still bears a strong family resemblance to the prototype.
Starting out as an all-metal cantilever low-wing monoplane with
fixed tricycle landing gear and power provided by a 150hp Avco Lycoming
O-320, it offered four-seat accommodation in an enclosed cabin.
The first production Cherokee flew just over a year after the prototype,
on February 10, 1961. Available from the beginning in a number of
different models, the level of equipment fitted determined whether
it was a Standard, Custom, Super Custom or AutoFlite model. In 1962
Piper introduced the PA-28-180 Cherokee, which was fitted with a
more powerful 180hp O-320-A2A engine - the PA-28-235 followed on
the year after. This machine featured a 235hp Avco Lycoming O-540-B2B5
flat-six engine for operation at a higher gross weight. The airframe
was also strengthened to accommodate the bigger engine and increased
weight.
In 1964, having made the PA28 larger and more powerful the previous
year, Piper chose to develop the aircraft in the other direction.
The company therefore introduced the two-seat PA-28-140 Cherokee,
which was powered by the 140hp O-320-A2B flat-four engine. The next
major design change came in 1967, with the introduction of the PA-28-180R
Cherokee Arrow. This aircraft was significantly different from its
predecessors, as it featured a fuel-injected engine, constant-speed
propeller and retractable tricycle landing gear as standard. Concurrent
with the introduction of the Arrow, Piper also decided to cease
production of the PA-28-150 and PA-28-160. Two years later in 1969,
Piper began production of a more powerful Arrow, the 200hp PA-28-200R,
which was powered by a 200hp IO-360-C1C engine. The company also
continued to develop and refine the more basic PA28 variants, and
in 1971 two new models of the PA-28-140 appeared. These were the
Cherokee Flite Liner, a two-seat trainer for use by Piper-sponsored
training schools, and the Cherokee Cruiser 2 Plus 2, which was a
deluxe two/four seat version. In the following year this variant
became the standard production model. In 1973 the PA-28-180 was
renamed the Cherokee Challenger and featured slight increases in
both wing span and fuselage length, along with an improved interior
and higher levels of equipment. Similar changes were also introduced
on the PA-28-235, which was renamed as the Cherokee Charger. A
number of changes were introduced to the Cherokee line in 1974,
with the Cherokee 2 Plus 2 being renamed the Cherokee Cruiser, the
Cherokee Challenger being renamed the Cherokee Archer, and the powerful
PA-28-235 the Cherokee Pathfinder. Also during 1974, Piper decided
to introduce the PA-28-151 Cherokee Warrior. Powered by a 150-hp
O-320-E3D engine, the fuselage was basically similar to the Archer,
although the wing was substantially redesigned. The new wing was
slightly larger in span and also featured tapered outer panels for
better aerodynamics and reduced drag. Three years later in 1977,
Piper ended production of the Cherokee Cruiser and Cherokee Pathfinder,
but introduced at the same time the PA-28-236 Dakota. This machine,
which was essentially similar to the Archer, featured the new wing
of increased span and was powered by a 235hp O-540-J3A5D flat-six
engine. The following year Piper began production of a version of
this aircraft powered by a 200hp Continental TS10-360-FB turbocharged
engine and known as the PA-28-201T Turbo Dakota. However, this particular
PA28 variant never really found favour with the aeroplane-buying
public, and poor sales saw production discontinued barely two years
after its introduction into service.
The same year Piper began work on a tandem two-seat trainer for
the Chilean air force. Loosely based on the Cherokee Arrow and designated
the PA-28R-300 Pillan (devil), it featured a retractable tricycle
landing gear and was powered by the 300hp Avco Lycoming AE10-540-H1K5
flat-six engine.
Production of the Cherokee family continued into the 1980s with
the company introducing the PA-28-161 Warrior II, powered by a 160hp
Avco Lycoming O-320-D3G engine, alongside the PA-28-181 Archer II,
which was powered by a 180hp Avco Lycoming O-360-A4M. At the other
end of the market the PA-28RT-201T Turbo Arrow IV incorporated the
same engine as used in the Turbo Dakota. Production of the PA28
still continues, with New Piper Aircraft, Inc currently manufacturing
Arrows, Archers and Warriors.
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| Statistics and Contacts |
DIMENSIONS |
| Length |
23ft
9in |
7.25m |
| Height |
7ft
3in |
2.23m |
| Wingspan |
35ft
|
10.67m
|
| Wing
Area |
170
sq ft |
15.79m2 |
| Aspect
Ratio |
5.6:1 |
Weights and Loadings
|
| Empty
weight |
1,414lb |
641kg |
| Max
AUW |
2,550lb |
1,156kg |
| Useful
load |
1,136lb |
515kg |
| Wing
loading |
15lb/ft2
|
73.2kg/m2 |
| Power
loading |
14.17lb/hp |
8.63kg/kW |
| Fuel
capacity |
41.5
Imp gal |
189
lit |
| Baggage
capacity |
200lbs |
90kgs |
Performance |
| Vne |
148kts |
275km/h |
| Cruise |
124kts |
243km/h |
| Stall
|
49kts |
91km/h |
| Climb
rate |
740ft/min
|
3.75m/s |
| Service
ceiling |
13,650ft |
4,160m |
| Range |
670nm |
1,243km
|
Engine
Textron-Lycoming
O-360-A4M air-cooled flat
four producing 180hp (134kW) at 2,700rpm.
Propeller
Sensenich
two-blade fixed pitch.
Manufacturer
Piper Aircraft Corporation
Vero Beach
Florida
UK Distributor
Anglo American Airmotive
Tel: 01202 591401
Fax: 01202 570203
Email sales@aaapiper.co.uk
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October
2 0 0 1
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This article appeared in the October
2001 issue of Today's Pilot.
To purchase this back-issue contact
our mail order department on +44(0)1780 480404 or click
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