Piper SENECA III User Manual

PIPER
AIRCRAFT CORPORATION SECTION
2
PA-34-220T,
SENECA III LIMITATIONS
2.15
MANEIR
ER LIMITS
All
intentional
acrobatic
maneuvers
(including
spins)
are
prohibited.
Avoid
abrupt
maneuvers.
2.17
FLIGHT
MANEUVERING LOAD
FACTORS
(a)
Positive
Load Factor
(Maximum)
(1)
Flaps
Up 3.8 G
(2)
Flaps
Down 2.0
G
(b)
Negative
Load Factor (Maximum) No
inverted
maneuvers
approved.
2,19
TYPES OF
OPERATION
The
airplane
is
approved
for
the
following
operations
when equipped
in
accordance
with
FAR
91
or
FAR 135.
(a)
Day
LF.R.
(b)
Night
L
F.R.
(c)
Day
LF.R.
(d)
Night
I.F.R.
(e)
Icing
conditions
when
equipped
per
Ice Protection
System
Instal-
lation
Supplement
(refer
to
Section
9).
2.21
FUEL
LIMITATIONS
(a)
Standard
Fuel Tanks
(1)
Total
Capacity
98 U.S. GALS.
(2)
Unusable
Fuel
5 U.S. GALS.
The
unusable
fuel
for this
airplane
has been determined
as
2.5
U.S.
gallons
in
each
wing
in
critical
flight
attitudes.
(3)
Usable Fuel
93 U.S. GALS.
(b)
Optional Fuel Tanks
(1)
Total
Capacity
128
U.S. GALS.
(2)
Unusable
Fuel
5
U.S.
GALS.
(3)
Usable Fuel
123
U.S.
GALS.
ISSUED:
JANUARY
8, 1981
REPORT:
VB-1110
2-7

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