Piper SENECA III User Manual

TABLE
OF CONTENTS
(cont)
SECTION 3
(cont)
Paragraph Page
No.
No.
3.9
Fire........
...
..
..... .....
. .......
3-17
Engine.Fire
On
The Ground
...........
.........
3-17
Engine
Fire In-Flight...............
.............
3-17
3. I
I
Fuel
Management
During
One
Engine
Inoperative
Operation
........... .
..
.
..........
3-17
Cruising........
.. .
. .........
3-18
Landing
............. ...
..
. .........
3-18
3. I3
Engine
Driven
Fuel Pump
Failure
.
. .
3-18
3.15
Landing Gear
Unsafe
Warnings
.....................
3-19
3.17
Manual
Extension Of
The
Landing
Gear
.............
3-19
3.19
Gear-Up Emergency
Landing.............
..........
3-20
3.21
Engine
Failure With
Rear
Cabin
and
Cargo
Doors
Removed
.......... ..
. ..
..
3-20
23
Electrical
Failures
........ . .......
3-20
3.25 Gyro
Suction
Failures..........
. ....,
3-23
3.27
Spins
...........
.....
.
3-24
129 Emergency
Descent
.......... ,...
.
3-24
3.31 Combustion
Heater
Overheat
......,...
.....,. .
3-24
3.33 Open Door
.........
....... .
3-25
3,35
Propeller
Overspeed..........
........
3-25
REPORT:
VB-Ill0
3-ii

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