Piper SENECA III User Manual

PIPER AIRCRAFT CORPORATION
SECTION 4
PA-34-220T, SENECA III NORMAL PROCEDURES
CLIMB
TAKEOFF CLIMB
Best
rate(flaps
up)...........
...........92
KIAS
Best
angle
(flaps
up).........-..
.
............76
KlAS
En
route.............
.
....,......102
KlAS
Cowlflaps
............
. .
.
. .
...........as
required
Power...........
.. . . .
........,..reducetoMCP
CRUlSE CLIMB
Mixture
.............
. ....
..........full
RICH
Power
...........
. .
...........75%
Climb
speed..............
..............102
KIAS
Cowl flaps
............ .
.............as
required
CREISING
Power
............
.
.
..............set
per power
table
Mixture
controls..............
..
.. . . ............
adjust
Cowl
tlaps
..........
............as
required
DESCENT
Mixtures...........
...........adjust
with
descent
Throilles...........
............
set
Cowl
flaps
.......... ..
............
CLOSED
ISSUED:
JANUARY 8, 1981
REPORT:
VB-1110
4-11

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