Piper SENECA III User Manual

PA-34-220T
naoE
-
O
SOO
USABLE
FUEL
123
GALLONS
4750
LBS.
-
GEAR
UP
Cruise
altitude
16500 ft
COWL
FLAPS
CLOSED
-
WING
FLAPS
UP
-
CLIMB
AT
M.C,P,
Power:
55%
DESCENT
AT 1000 FPM
AND
145
KIAS
-
NO
WIND
Range
with
reserve
894
nm
4 2
GAL
FUEL
FOR
START.
TAXI AND
TO
Range
without
reserve
1010
nm
whúTURE4 LEANED
IN ACCORDANCE
i
a
W1TH
PROCEDURES
IN SECTION 4 37
HibH
SPEED 75
25,000
-
NOTES
95
I
-
HANGE
INCLUDES CUMB &
LONG
RANGL
(M
I
DESCENT
DISTANCES
MAN
REA
OX
I
55%
POWER
-55%
POWER
1 NM
FOR
EACH C
"'
C
,
20,000
N
F
EACH
STD TEMP
75
15,000
soo
600
700
000 900
1000
r
Too
soo
soo
tooo
11oo
RANGE
--
NAUTICAL
MILES
RANGE
-
NAUTICAL
M1LES
WITH
45
MIN.
RESERVE
AT45% POWER
WITH
NO
RESERVE
oc oc

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