ARROW
E.
AIRSPEED LIMITATIONS AND INSTRUMENT MARKINGS (Calibrated Airspeed)
NEVER EXCEED SPEED
MAXIMUM STRUCTURAL CRUISE SPEED
MANEUVERING SPEED
FLAPS EXTENDED SPEED
MAXIMUM GEAR EXTENSION SPEED
MAXIMUM GEAR RETRACTION SPEED
AIRSPEED INSTRUMENT MARKINGS
Red Radial Line (Never Exceed)
Yellow Arc (Caution Range)
(Smooth Air Only)
Green Arc (Normal Operating Range)
White Arc (Flap Down Range)
F. FLIGHT LOAD FACTORS
Positive Load Factor (Maximum)
Negative Load Factor (Maximum)
214 MPH
170 MPH
131 MPH
125 MPH
150 MPH
125 MPH
214MPH (186KT)
170 MPH to 21 4 MPH
(148 KT to 186 KT)
7
1
MPH to 170 MPH
(62 KT to 148 KT)
64 MPH to 125 MPH
(56 KT to 109 KT)
3.8 G
No inverted maneuvers approved
G. MAXIMUM WEIGHT 2650 LBS
H. BAGGAGE CAPACITY 200 LBS
I. C. G. RANGE
NOTES
Weight
Pounds
2650
2300
1800
1. Straight line variation between points given.
2. The datum used is 78.4 inches ahead of the wing leading
edge at the intersection of the straight and tapered section.
3. It is the responsibility of the airplane owner and the pilot to
insure that the airplane is properly loaded. See "Weight and
Balance Section" for proper loading instructions.
REPORT:
VB-560
PAGE
3-2
MODEL: PA-28R-200
Forward Limit
Inches Aft of Datum
87.3
82.0
80.0
FAA
APPROVED MAY
14,1973
Rearward Limit
Inches After of Datum
93.0
93.0
93.0
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