Piper PA-32RT-300T User Manual

FUEL
SYSTEM
Fuel
Tanks:
LANCE
II
SERVICE
MANUAL
TABLE
II-I.
LEADING
PARTICULARS
AND
PRINCIPAL
DIMENSIONS
(cont.)
MODEL
PA-32RT-300
PA-32RT-300T
Overvoltage
Relay,
WICO
Fuel
Pump
Drive
X16799
Lear-Siegler
RG17980-K
AC
Pump
Lycoming
Part
No.
75247
X16799
PROPELLER
Manufacturer
Hub
Model
Blade
Model
Diameter
Diameter,
Minimum
Blade
Angle,
Low
Pitch
(at
30
in.
Radius)
Blade
Angle,
High
Pitch
(at
30
in.
Radius)
Governor
Control
Governor
Model
Hartzell
See
Table
VIII-I
See
Table
VIII-I
80.0 in.
78.5
in.
13.5
°
±0.2
°
34.0
°
±
1.0
°
Hartzell
F4-11B
Hartzell
See
Table
VIIIA-I
See
Table
VIIIA-I
80.0
in.
78.5
in.
15.6
°
t
0.2
°
34.0'
±
1.0°
Hartzell
F-4-
lB
4 (2
interconnected
each
wing)
49
U.S.
gallons
(each
set)
Capacity
Unusable
Fuel
2
U.S.
gallons
(each
set)
4
(2
interconnected
each
wing)
49
U.S.
gallons
(each
set)
2 U.S.
gallons
(each
set)
98
U.S.
gallons
4
U.S.
gallons
Total
Capacity
Total
Unusable
Fuel
Electric
Fuel
Pump
98
U.S.
gallons
4 U.S.
gallons
Airborne
1B5-6
Issued:
1/3/78
HANDLING
AND
SERVICING
1A23

Piper PA-32RT-300T Specifications

General

Brand	Piper
Model	PA-32RT-300T
Category	Aircrafts
Language	English