Piper SENECA III User Manual

PA-34-220T
LÄÑÒiÑÖ
Ò18ÏAÑÖE
NÒÑMÄLPRÖCEDURE
STANDARD
WHEELS,
TIRES,
AND BRAKES
THROTTLES
CLOSED 40"
WING
FLAPS
FULL
STALL
TOUCHDOWN PAVED,
LEVEL DRY
3000
i i i
i
i
RUNWAY
MAXIMUM BRAKING
-
Example:
2000
O.A.T.:
22°C
30
as
4 82
76
Pressure
altitude: 3000
ft. 2600
Gross
weight: 3655 lbs.
Head wind: 10
knots
2400
Landing
ground roll
1120
ft
Total
lavrlinr stietance
war
Wh
ha
r
er
Dann
ft
no
B
irrier
s
eed: 82 KIAS
T
rl,, en
H-H¯
H
2ooo
2
m
600
soo
2
LTI
-
600
-40 -20
0
20
40
4500 4000 3500
3000
0 5 10 15
OUTSIDE AIR
TEMPERATURE-°C
WEIGHT
-
POUNDS WIND COMPONENTS
-
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