Piper SENECA III User Manual

TABLE
OF
CONTENTS
SECTION 2
LIMITATIONS
Paragraph
Page
No.
No.
2.1
General
..........,
.
.......
2-1
2 3
Airspeed
Limitations
..
.........
.
.
.........
2-1
2.5
Airspeed
Indicator
Markings.........
.. . .......
2-2
2.7
Power
Plant
Limitations..........
...
. .
.......
2-3
2.9
Power
Plant
instrument
Markings
...................
2-5
2.11
Weight
Limits.............
.
.
.........
2-6
2.13
Center
of
Gravity Limits..............
..
........
2-6
2.15
Maneuver
Limits
............
.
.
........
2.7
2.17
Flight
Maneuvering
Load
Factors
...................
2-7
2.19
Types
of
Operation
..........
.....
2-7
2.2 I
Fuel
Limitations
- , .
-
- -
- - .
.
. .
.
. . .
.
.
2-7
2,23
Noise
Level
...........
........
2-8
2.25
Heater
Limitations..........
.......
2-8
227
Operating
Altitude
Limitations
........... .
.......
2-8
229
Gyro
Suction
limits
.............
.........
2-8
2 31
Operation
with
Aft Doors
Removed
.........
.......
2-8
233
Placards...--......
.
.
.......
2-9
REPORT:
VB-1110
2-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