Piper SENECA III User Manual

PIPER
AIRCRAFT CORPORATION SECTION 2
PA-34-220T,
SENECA III
LIMITATIONS
2.33
PLACARDS
In
full
view
of
the
pilot:
THIS
AIRPI
ANE
MUST
BE OPERATED
ASA NOR
MAL
CATEGORY
AIRPLANE
IN
COMPLIANCE
WlTH
THE
OPERAT]NG
LIMlTATIONS
STATED
IN
THE
FORM OF
PLACARDS,
MARKlNGS. AND
MANUALS.
NO
ACROBATIC MANEUVERS
(lN-
CLUD1NG SPINS)
APPROVED.
THIS
AIRCRAFT
APPROVED FOR V.F.R,
l.F.R.,
DAY,
NIGHT
AND
ICING FLIGHT
WHEN
EQUIPPED
IN
ACCORDANCE WETH FAR 9!
OR
FAR
135.
In
full
view
of
the
pilot:
MAXIMUM
TAKEOFF WEIGH T
4750 POUNDS
MAXIMUM
LANDING WEIGHT 4513 POUNDS
ALL
WEIGHT IN
EXCESS OF4470 POUNDS
MUST
CONSISTOFFUEl..-(EXCEPTlNCASESSPECIFIED
BY
SECTION
6
OF P.O.H.).
MINiMUM
SlNGl E
ENGINE CONTROL SPEED
66
KIAS
On
instrument
panel in full
view
of
the
pilot:
VA
140
AT
4750
LBS.
(SEE A.F.M.)
VI.o
130
DN, 108 UP
VI.E
130 MAX.
DEMO X-WIND 17
KTS
Near
emergency
gear
release:
EMERGENCY GEAR
EXTENSION
PULL TO RELEASE.
SEE
A.F.M.
BEFORE
RE-ENGAGEMENT
ISSUED:
JANUARY
8, 1981
REPORT:
VB-1110
2-9

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