Piper SENECA III User Manual

PA-34-22OT
NORMAL
PROCEDURE
TAKEOFF
ASSOCIATED CONDITIONS:
Example:
2800
RPM
AND 40 INCHES MAR
,
O.A.T 2
C
PAVED,
LEVEL, DRY
RUNWAY LIFTOFF AT 79 KIAS
Pressure
altitude
2000 ft
BARRIER AT 79
KIAS
FLAPS
O'
COWL
FLAPS 2
OPEN
Gross
weight
3969
Ibs
Headwind 9
knots
¯
'
Takeoff ground
roll
1350 f
-
3000
Takevil
distane
over
5 ba
rwr
!650
rn
-«
O -20
0
20 40
4500 4000 3500
0
0
10
15
OUTSIDE AIR
TEMPERATURE
-°C
WElGHT
-
POUNDS
WIND
COMPONENT
-
KTS.

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