Piper CHEROKEE ARROW 200 Guía del usuario
CHEROKEE
ARROW
.__
PA-28R-200
., .
This
handbook
for
airp
l
anes
with
serial
nos
.
28R-35001
through
28R
-
35392
.
Owner's
Handbook
Piper
Aircraft
Corporation,
Vero
Beach,
Florida
U.S.
A.
NOTICE
THIS HANDBOOK
IS
NOT DESIGNED,
NOR
CAN ANY
HANDBOOK SERVE,
AS
A SUBSTITUTE
FOR
ADEQUATE AND
COMPETENT FLIGHT INSTRUCTION,
OR
KNOWLEDGE
OF
THE
CURRENT AIRWORTHINESS DIRECTIVES,
THE
APPLICABLE
FEDERAL AIR REGULATIONS, AND ADVISORY CIRCULARS. IT
IS
NOT INTENDED TO
BE
A GUIDE
OF
BASIC FLIGHT
INSTRUCTION, NOR A TRAINING MANUAL.
THE HANDBOOK
IS
DESIGNED:
1. TO HELP YOU OPERATE YOUR CHEROKEE WITH
SAFETY AND CONFIDENCE.
2. TO MORE FULLY ACQUAINT YOU WITH
THE
BASIC
PERFORMANCE AND HANDLING CHARACTERISTICS
OF
THE
AIRP~ANE.
3.
TO
MORE FULLY EXPLAIN YOUR CHEROKEE'S
OPERATION THAN
IS
PERMISSIBLE
TO
SET
FORTH
IN
THE AIRPLANE FLIGHT MANUAL.
IF THERE
IS
ANY INCONSISTENCY BETWEEN THIS
HANDBOOK AND THE AIRPLANE FLIGHT MANUAL APPROVED
BY
THE F.A.A., THE FLIGHT MANUAL SHALL GOVERN.
Revised
text
and illustrations shall
be
indicated
by
a
black venical line in the margin opposite
the
change.
Additional copies
of
this manual, Pan No. 753
795,
may
be
obtained from
YO':'.!'
Piper Dealer.
Published
by
·PUBLICATIONS DEPARTMENT
Piper Aircraft Corporation
753
795
Issued: February 1969
Revised: January
1987
Performance
Weights.
Power
Plant
Fuel
and
Oil
Baggage
Dimensions
Landing
Gear
.
SECTION
I
SPECIFICATIONS
1
2
2
2
2
3
3
CHEROKEE
"ARROW"
SECTION
I
SECTION
I
SPECIFICATIONS
PERFORMANCE
Performance figures are for
airplanes
equipped for
cross-
country transportation and flown
at
gross
weight under standard
conditions
at
sea
level
or
stated
altitude.
Any changes in equip-
ment
may
result
in
changes
in performance.
Take-off Run (maximum effort,
25°
flap) (ft)
Take-off over 50-ft barrier (maximum effort,
25°
flap)
(ft)
Best
Rate
of Climb Speed (mph)
Rate
of Climb (ft per min)
Service
Ceiling
(ft)
Absolute
Ceiling
(ft)
Top Speed {mph)
Optimum Cruising Speed
(75%
power, optimum
altitude)
(mph)
Cruising Range
(75%
power, optimum altitude)(mi)
Optimum Cruising Range
(55%
power, optimum
altitude)
(mi)
Stalling Speed (flaps down, gear down) (mph)
Stalling Speed (flaps and gear up) (mph)
Landing
Roll
(flaps down) (ft)
Landing
Roll
aver 50-ft barrier (ft)
i690203
770
1600
95
910
16,000
18,000
176
166
810
950
64
70
780
1380
1
SECTION
I
SPECIFICATIONS
(cont):
WEIGHTS
Gross Weight
(lbs)
Empty Weight (Standard)
(lbs)
USEFUL
LOAD
(Standard) {lbs)
POWER
PLANT
Engine {Lycoming)
Rated
Horsepower
Rated Speed (rpm)
Bore
(in.)
Stroke
(in.)
Displacement (cu
in.)
Compression
Ratio
Dry Weight
(lbs)
Propeller
FUEL
AND
OIL
Fuel
Capacity
(U.S.
gal)
Oil Capacity
(qts)
Fuel,
Aviation Grade (min
octane)
BAGGAGE
2
Maximum
Baggage
(lbs)
Baggage Space (cu
ft)
Baggage Door Size
(in.)
CHEROKEE
"ARROW"
2600
1450
1150
10-360-ClC
200
2700
5.125
4.375
361.0
8.7:1
326
HC-C2YK-1/7666A-2
so
8
100/130
200
17
20
X
22
. 690203
CHEROKEE
"ARROW"
SPECIFICATIONS
(cont):
DIMENSIONS
Wing
Span (ft)
Wing
Area
(sq
ft)
Wing
Loading (lbs per
sq
ft)
Length
(ft)
Height (ft)
Power Loading (lbs per
hp)
LANDING
GEAR
Wheel
Base
(ft)
Whee
1
Tread
(ft)
Tire
Pressure
(psi)
Nose
Tire
Size
690203
Main
Nose (4 ply
rating)
Main (4 ply
rating)
SECTION
I
30
160
16.3
24.2
8.0
13.0
7.4
10.5
30
27
5.00 X 5
6.00
X 6
3
SECTION
I
CHEROKEE
''ARROW''
.___10'10.0"-____.
...,.._--------30'-------___.
1
8'
4
690203
SECTION
II
DESIGN
INFORMATION
Engine
and
Propeller
.
Induction
System.
Structures . .
Landing
Gear .
Control Systems .
Fue
1 System .
Electrical
System
Heating
and
Ventilating
System .
Cabin
Features
.
5
5
6
7
11
.
11
.
12
.
16
. 16
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1
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