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Piper Aircraft Corporation PA-32R-301T Owner's manual

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PIPER AIRCRAFT CORPORATION
PA.32R.3OI, SARATOGA SP
SECTION I
GENERAL
SECTION I
GENERAL
1.T INTRODUCTION
This Pilot's Operating Handbook is designed for maximum utilization
as an operating guide for the pilot. It includes the material required to be
furnished to the pilot by FAR/CAR. It also contains supplemental data
supplied by the airplane manufacturer.
This handbook is not designed as a substitute for adequate and
competent flight instruction, knowledge of current airworthiness directives,
applicable federal air regulations or advisory circulars. It is not intended to
be a guide for basic flight instruction or a training manual and should not be
used for operational purposes unless kept in a current status.
Assurance that the airplane is in an airworthy condition is the
responsibility of the owner. The pilot in command is responsible for
determining that the airplane is safe for flight. The pilot is also responsible
for remaining within the operating limitations as outlined by instrument
markings, placards, and this handbook.
Although the arrangement of this handbook is intended to increase its
in-flight capabilities, it should not be used solely as an occasional operating
reference. The pilot should study the entire handbook to familiarize himself
with the limitations, performance, procedures and operational handling
characteristics of the airplane before flight.
The handbook has been divided into numbered (arabic) sections each
provided with a "finger-tip" tab divider for quick reference. The limitations
and emergency procedures have been placed ahead of the normal
procedures, performance and other sections to provide easier access to
information that may be required in flight. The "Emergency Procedures"
Section has been furnished with a red tab divider to present an instant
reference to the section. Provisions for expansion of the handbook have
been made by the deliberate omission of certain paragraph numbers, figure
numbers, item numbers and pages noted as being intentionally left blank.
REPORT: VB'1080
l-l
ISSUED: NOVEMBER 8, 1979
SECTION I
GENERAL
PIPER AIRCRAFT CORPORATION
PA-32R-301, SARATOGA SP
12'11'
36',2
178.3
30.0
Wing Area (sq. ft.)
Min. Turning Radius (ft.)
(from pivot point to wing tip)
5',6"
REPORT: VB-r080
r-2
27'4"
THREE VIEW
Figure l-l
7' 1"
ll,r)Zl^
11',1"
d 'u" {'
o
7' 11"
ISSUED: NOVEMBER 8, 1979
PIPER AIRCRAFT CORPORATION
PA-32R-301, SARATOGA SP
SECTION T
GENERAL
I.3 ENGINE
2 BLADE PROPELLER
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model Number
(d) Rated Horsepower
(e) Rated Speed (rpm)
(0 Bore (inches)
(g) Stroke (inches)
(h) Displacement (cubic inches)
(i) Compression Ratio
0) Engine Type
3 BLADE PROPELLER
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model Number
(d) Rated Horsepower
(e) Rated Speed (rpm)
(0 Bore (inches)
(g) Stroke (inches)
(h) Displacement (cubic inches)
(i) Compression Ratio
ü) Engine Type
1.5. PROPELLER
2 BLADE PROPELLER
(a) Number of Propellers
(b) Propeller Manufacturer
2600
300
2700
5.t25
4.375
541.5
8.7: I
Six Cylinder, Direct Drive,
Horizontally Opposed, Air Cooled,
Fuel Injected
I
Lycoming
ro-540-KlG5D
300
2700
5.125
4.375
541.5
8.7:l
Six Cylinder, Direct Drive,
Horizontally Opposed, Air Cooled,
Fuel Injected
Hartzell
REPORT: VB-10t0
1-3
Max. Cont.
Power
I
Lycoming
ro-540-KlG5D
T.O. Power-
5 Min. Limit
294
ISSUED: NOVEMBER t, 1979
SECTION I
GENERAL
PIPER AIRCRAFT CORPORATION
PA-32R-30r, SARATOGA SP
(c) Blade Model
(d) Number of Bladqs
(e) Ilub-Modet--
(f) Propeller Diameter (inches)
(l) Minimum
(2) Maximum
(g) Propeller Type
3 BLADE PROPELLER
(a) Number of Propellers
(b) Propeller Manufacturer
(c) Blade Model
(d) Number of Blades
(e) Hub Model
(f) Propeller Diameter (inches)
(l) Minimum
(2) Maximum
(g) Propeller Type
r.7 FUEL
AVGAS ONLY
(a) Fuel Capacity (U.S. gal.) (total)
(b) Usable Fuel (U.S. gal.) (total)
(c) Fuel Grade, Aviation
(l) Minimum Grade
(2) Alternate Fuels
REPORT: VB-1080
t-4
F8475D-4
2
HC-C2Y(K,R)-r( )F
78.5
80
Constant Speed,
Hydraulically Actuated
I
Hartzell
F7663R-O
3
HC-C3YR-r( )F
76
78
Constant Speed,
Hydraulically Actuated
107
102
100 - Green or I00LL - Blue
Aviation Grade
Refer to latest revision of
Lycoming Service Instruction 1070.
ISSUED: NOVEMBER 8. 1979
REVISED: SEPTEMBER 17, 1984
PIPER AIRCRAFT CORPORATION
PA.32R-301, SARATOGA SP
SECTION I
GENERAL
1.9 oIL
Capacity (U.S. quarts) 12
Specification Refer to latest issue of
Lycoming Service Instruction 1014.
Viscosity per Average Ambient Temp. for Starting
SINGLE MULTI
Above 60oF 50 40 or 50
30oF to 90oF 40 40
0o to 70oF 30 zl0 or 20W-30
Below l0oF 20 20W-30
I.T1 MAXIMUM WEIGHTS
(a) Oil
(b) oil
(c) Oil
(l)
(2)
(3)
(4)
(a) Maximum Takeoff Weight (lbs.)
(b) Maximum Landing Weight (lbs.)
(c) Maximum Ramp Weight (lbs.)
(d) Maximum Weights in Baggage
Compartments
(a) Compartment Volume (cubic feet)
(b) Entry Width (inches)
(c) Entry Height (inches)
1.I7 SPECIFIC LOADING
(a) Wing Loading (lbs. per sq. ft.)
(b) Power Loading (lbs. per hp)
ISSUED: NOVEMBER 8, 1979
REVISED: SEPTEMBER 17' 1984
3600
3600
361 5
AFT
FORWARD
100
FORWARD
7.0
16.0
22.0
100
I.I3 STANDARD AIRPI,ANE WEIGHTS
Refer to Figure 6-5 for the Standard Ernpty Weight and the Useful
Load.
r.15 BAGGAGE SPACE
AFT
t7.3
48.0
26.0
20.2
t2.0
REPORT: VB-10t0
1-5
PIPER AIRCRAFT CORPORATION
PA-32R-301, SARATOGA SP
SECTION 2
LIMITATIONS
SECTION 2
LIMITATIONS
2.1 GENERAL
This section provides the "FAA Approved" operating limitations,
instrument markings, color coding and basic placards necessary for
operation of the airplane and its systems.
Limitations associated with those optional systems and equipment
which require handbook supplements can be found in Section 9
(Supplements).
2.3 AIRSPEED LIMITATIONS
SPEED KIAS KCAS
Never Exceed Speed (Vr.rr) - Do not ex-
ceed this speed in any operation. 197 189
Maximum Structural Cruising Speed
(VNd - Do not exceed this speed
except in smooth air and then only
with caution.
Design Maneuvering Speed (Va ) - Do
not make full or abrupt control move-
ments above this speed.
At 3600 LBS. G.W.
At 2230 LBS. G.W.
154 150
134
105
t32
104
REPORT: VB-10t0
2-l
ISSUED: NOVEMBER 8, 1979
SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA.32R.3OI, SARATOGA SP
CAUTION
Maneuvering speed decreases at lighter weight
as the effects of aerodynamic forces become
more pronounced. Linear interpolation may be
used for intermediate gross weights.
Maneuvering speed should not be exceeded
while operating in rough air.
SPEED
Maximum Flaps Extended Speed (Vrs) -
Do not exceed this speed with the flaps
extended.
Maximum Landing Gear Extension
Speed (Vlo) - Do not exceed this speed
when extending the landing gear.
Maximum Landing Gear Retraction
Speed (Vr-o) - Do not exceed this speed
when retracting the landing gear.
Maximum Landing Gear Extended
Speed (V'u) - Do not exceed this speed
with the landing gear extended.
2.5 AIRSPEED INDICATOR MARKINGS
MARKING
Red Radial Line (Never Exceed)
Yellow Arc
(Caution Range - Smooth Air Only)
Green Arc (Normal Operating Range)
White Arc (Flap Down)
REPORT: VB-1080
2-2
KIAS KCAS
n2 109
t32
il0 r09
t32 r30
IAS
I97 KTS
130
154 KTS to
60 KTS to
57 KTS to
I97 KTS
I54 KTS
I 12 KTS
ISSUED: NOVEMBER 8, 1979
PIPER AIRCR AI.-'t COR PORATION
I'A-32R-30I, SARATO(;A SP
SECTION 2
LIMITATIONS
2.7 POWUR PLANT LIMITATIONS
2 lll.ADE PROPEI-t-l:l(
(l) Numbcr of Engincs
(h) Enginc Manufacturcr
(c) Engine Model No.
(d) Enginc Operating [-imits
(l) Maximum Horse Power
(2) Maxinum Engine Speed
(RPM)
(3) Maximum Oil Temperature
('F)
(e) Oil Pressure
Minimum (red line)
Maximum (red line)
(f) Fuel Flow/ Pressure
Maximum (red line)
(g) Fuel (AVGAS ONLY)
(mininrum grade)
(h) Number of Propellers
(i) Propeller Manufacturer
0) Propeller Hub and Blade Model
(k) Propeller Diameter (inches)
Minimum
Maximum
(l) Blade Angle Limits
l-ow Pitch Stop
High Pitch Stop
lSSl-lED: NOvf,MBER 8. 1979
REVISED: SEPTEMBER 17, 1984
25 PSI
t00 PSt
35 gal/hr; 14 PSI
100 or l00LL
Aviation Grade
I
Hartzell
HC-C2Y(K,R)-r( )F/
F8475D-4
78.5
80
13.5o t 0.2"
34" t lo
REPORT: VB-10t0
2-3
Max. Cont.
Power
294
2600
245
I
Lycoming
r0-540-K rc5D
T.O. Power-
5 Min. Limit
300
2700
245
sEcTloN 2
LIMITATIONS
PIPER ATRCRAFT CORPORATION
PA.32R.3OI, SARATOGA SP
3 BLADE PROPEL.LER
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model No.
(d) Engine Operating Limits
(l) Maximum Horse Power
(2) Maximum Rotation Speed (RPM)
(3) Maximum Oil Temperature (o F)
(e) Oil Pressure
Minimum (red line)
Maximum (red line)
(0 Fuel Flow/ Pressure
Maximum (red line)
(g) Fuel Grade (minimum grade)
(h) Number of Propellers
(i) Propeller Manufacturer
0) Propeller Hub and Blade Model
(k) Propeller Diameter (inches)
Minimum
Maximum
(l) Blade Angle Limits
Low Pitch Stop
High Pitch Stop
I
Lycoming
I0-540-KrG5D
2700
25 PSI
100 PSI
35 gal/hr; 14 PSI
100 - Green or
l00LL - Blue
Aviation Grade
I
Hartzell
HC-C3YR-l ( )F/
F7663R-0
12.4" ! 0.2"
32.0o t 1.0"
ISSUED: NOVEMBER t, 1979
REVISED: SEPTEMBER I, l9t6
300
245
I
76\
78
REPORT: VB-1080
2-4
PIPER AIRCRAFT CORPORATION
PA.32R.301, SARATOGA SP
SECTION 2
LIMITATIONS
2.9 POWER PLANT INSTRUMENT MARKINGS
(a) Tachometer
(l) 2 Blade Propeller
Green Arc (Normal Operating Range) 500 to 2600 RPM
Yellow Arc (5 Minute Limit) 2600 to 2700 RPM
Red Line (Maximum) 2700 RPM
(2) 3 Blade Propeller
Green Arc (Normal Operating Range) 500 to 2700 RPM
Red Line (Maximum) 2700 RPM
(b) Oil Temperature
Green Arc (Normal Operating Range) 75o to 245oF
Red Line (Maximum) 245"F
(c) Oil Pressure
Green Arc (Normal Operating Range) 60 PSI to 90 PSI
Yellow Arc (Caution Range) (ldle) 25 PSI to 60 PSI
Yellow Arc (Caution Range)
(Start and Warm Up) 90 PSI to 100 PSI
Red Line (Minimum) 25 PSI
Red Line (Maximum) 100 PSI
(d) Fuel Flow/ Pressure
Green Arc (Normal Operating Range) 0 gal/hr. to 34.9 gal/hr.
Red Line (Maximum) 35 gal/hr.: 14 PSI
2.IIWEIGHT LIMITS
(a) Maximum Weight
(b) Maximum Ramp Weight
(c) Maximum Baggage (100 lbs. each compartment)
NOTE
Refer to Section 5 (Performance) for maximum
weight as limited by performance.
3600 LBS.
3615 LBS.
2OO LBS.
REPORT: VB-1080
2-5
ISSUED: NOVEMBER t, 1979