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Piper SENECA III User Manual

Piper SENECA III
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PIPER
AIRCRAFT
CORPORATION
SECTION
7
PA-34-220T,
SENECA III
DESCRIPTION
&
OPERATION
RIGHT
MAIN
GEAR
LEFT
MAIN
G€AR
HYDRAULIC
CYLINDER
HyOAAU IC
cytlNDER
O
O
WN
DOWN
NOSE
GEAR
PRESSURE
SWITCH
RESTRICTOR
FREE
ALL
CONTROL
600
2000
PSI
RE$ERVO
UNTRE-
THERMAL
REMEF
4000
PSI
CONTROL
660±hõO
PSI GEAR
UP
CNfcMVALVE
DELivERED
PRE5$
400-800 PSI
LANDING
GEAR
HYDRAULIC
SYSTEM
SCHEMATIC
Figure
7-7
ISSUED:
JANUARY
8, 1981
REPORT: VB-1110
7-9

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Piper SENECA III Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelSeneca III
Engine TypePiston
Engine ModelContinental TSIO-360-KB
Seating Capacity6
Cruise Speed188 knots (216 mph, 348 km/h)
Length28 ft 7 in (8.71 m)
Max Takeoff Weight4, 750 lb (2, 155 kg)
Horsepower220 hp each
Service Ceiling25, 000 ft (7, 620 m)
Height9 ft 11 in (3.02 m)
Propellers2-bladed constant speed

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