Piper SENECA III User Manual

TABLE
OF
CONTENTS
SECTION 6
WEIGHT
AND
BALANCE
Paragraph
Page
No.
No.
6.]
General
............... ..
.
..
.........
6-1
6.3
Airplane
Weighing
Procedure
.............
.........
6-2
6.5
Weight
and
Balance
Data
and
Record
..,
.
............
6-5
6,7
General
Loading
Recommendations..................
6-9
6.9
Weight and
Balance
Determination for
Flight
.
. . .
. .
.
.
.
6-10
6.11
Instructions
for
Using
the
Weight and
Balance
Plotter.. 6-15
6.13
*Equipment
List....
.
6-19
(a)
Propeller
and
Propeller
Accessories
. . . .
.
.
6-20
(b)
Engine
and
Engine
Accessories
. . . . .
. .
.
. .
. . . . .
6-21
(c)
Landing
Gear
and Brakes
...................
6-22
(d)
Electrical
Equipment.......
................
6-23
(e)
Instruments............
..........
6-26
(f)
Miscellaneous..............................
6-28
(g)
Propeller
and
Propeller
Accessories
(Optional
Equipment).....................
6-29
(h)
Engine
and
Engine
Accessories
(Optional
Equipment)..............................
6-30
(i)
Landing
Gear
and
Brakes
(Optional
Equipment)...............
..............
6-31
(j)
Electrical
Equipment
(Optional
Equipment)....
6-32
(k)
Instruments
(Optional
Equipment)
.
. . .
.
.
.
. .
. . .
6-34
(I)
Autopilots
(Optional
Equipment)
.............
6-40
(m)
Radio
Equipment
(Optional
Equipment).......
6-41
(n)
Miscellaneous
(Optional
Equipment)
..........
6-55
(o)
Maximum
Zero
Fuel
Weight
Increase
. .
. .
. . . . .
6-65
**Equipment
List
(Form
240
0010)
........
ENCLOSED WITH
THlS HANDBOOK
*For
1982
and
preceding
models
only.
**For
1983
and
subsequent
models
only.
REPORT:
VB-1110
6-i

Piper SENECA III Specifications

General

Manufacturer	Piper Aircraft
Model	Seneca III
Engine Type	Piston
Engine Model	Continental TSIO-360-KB
Seating Capacity	6
Cruise Speed	188 knots (216 mph, 348 km/h)
Length	28 ft 7 in (8.71 m)
Max Takeoff Weight	4, 750 lb (2, 155 kg)
Horsepower	220 hp each
Service Ceiling	25, 000 ft (7, 620 m)
Height	9 ft 11 in (3.02 m)
Propellers	2-bladed constant speed