Piper SENECA III User Manual

PA-34-220T
MAXIMUM
EFFORT TAKEOFF
-
FLAPS
25°
ASSOCIATED
COND'TiO'\l:2
2800
RFM AND 40 1NCilES MAP
SEFORE
-
BRAKE
RELEASE
PAVED, LEVEL
DRY RUNWAY
--
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LIFTOFF
AT
84 KIAS BARRIER
AT 86 KIAS
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-
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S 25 COWi i LAPS
1/2
OPEN
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- -
OAT 2Pc
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Pressure
altitude
2000
ft
L
Gross
weight
4250
lbs
-
Headwmd
9
Pois
¯
Takeoff
groor.d
ro!!
800
ft ¯ ¯
2000
og
Takeoff
dwance
over
50 ft
bamer 104
1500
i
I
--
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-40
-20
0
20
40 4&OO
4000
3500
3000
O
& 10
1
UTSIDE
AIR TEMPERATURE
-°C
WEIGHT
-
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