Maximumweights; Standardairplaneweights; Baggagespace; Specificloadings - Piper CHEROKEE TURBO ARROW III 1976 Pilot Operating Handbook

SECTION 1
PIPER AIRCRAFT CORPORATION
GENERAL
PA-28R-201T, CHEROKEE
TURBO,ARROW III
1.11 MAXIMUMWEIGHTS
(a)
Maximum
Takeoff Weight (lbs)
2900
(b)
Maximum
Landing Weight (lbs)
2900
(c)
Maximum Weights in Baggage Compartment
200
1.13 STANDARD AIRPLANE WEIGHTS
(a)
Standard Empty Weight
(lbs): Weight
of a
standard airplane including unusable fuel,
full operating
fluids
and
full oil.
1645
(b)
Maximum Useful Load
(lbs)*: The difference
between
the
Maximum Takeoff Weight and
the
Standard Empty Weight.
1255
1.15 BAGGAGE SPACE
(a) Compartment Volume (cubic feet)
24
(b)
Entry Width
(inches)
22
(c)
Entry Height
(inches)
20
1.17 SPECIFIC LOADlNGS
(a)
Wing Loading
(lbs
per sq
ft)
17
(b)
Power Loading
(lbs
per
hp)
14.5
*This
value is for
a standard airplane without optional equipment. Refer
to
Figure 6-5 for the
useful
load
value
to
be used for C.G.
calculations
for the
airplane specified.
REPORT: VB-800
ISSUED: DECEMBER 20,
1976
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