Piper SENECA III User Manual

SECTlON
3
PIPER
AIRCRAFT
CORPORATION
EMERGENCY
PROCEDURES
PA-34-220T,
SENECA
III
3.3
EMERGENCY
PROCEDURES
CHECKLIST
AIRSPEEDS
FOR
SAFE
OPERATIONS
One
engine
inoperative
air minimum
control
................66
KIAS
One
engine
inoperative best
rate
of
climb
...................92
KIAS
One
engine
inoperative
best
angle
of
climb
.
-
. . . . . .
. .
. .
. .
,
,
. .
78
KIAS
Maneuvering
..............
-
.
. ..
............140
KlAS
Never
exceed
............ ..
.
............205
KlAS
ENGINE
INOPERATIVE
PROCEDURES
NOTE
The
power
on
the
operating
engine should
be
reduced when
safe
to
do
so
DETECTING DEAD
ENGlNE
Loss
of
thrust.
Nose
of
aircraft
will
yaw
in direction
of
dead
engine
(with
coordinated
controls).
ENGINE
SECURlNG
PROCEDURE
(FEATHERING PROCEDURE)
Minimurn
control speed...............
.
............66
KIAS
One
engine
inoperative
best
rate
of climb
...................92
KIAS
Maintain
direction
and airspeed above
85 KIAS.
Mixture
controls........
..
.
...........forward
Propeller
controls
. . .. . , , ..
..
..
..
. . . . . . ..
.. .,
forward
Throttle
controls............
..
.........(40
in. Hg.
Max.)
forward
Flaps............
.
............
retract
Gear
....,.............
.............
retract
Identify inoperative
engine.
Throttle
of
inop.
engine............
...........
retard
to
verify
REPORT:
VB-1110
ISSUED: JANUARY
8,
1981
3-2

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