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  9. Piper Aircraft Corporation PA-28RT-201T TURBO ARROW IV User manual

Piper Aircraft Corporation PA-28RT-201T TURBO ARROW IV User manual

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PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SECTION 1
GENERAL
SECTION I
GENERAL
1.1 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 CAR 3 and FAR Parl2l SubpartJ.It also contains
supplemental data supplied by the airplane manufacturer.
This handbook is not designed as a substitute for adequate and compe-
tent flight instruction, knowledge of current airworthiness directives, appli-
cable 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 responsi-
bility 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 proce-
dures, performance and other sections to provide easier access to informa-
tion 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 ofthe 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-940
1-1
ISSUED: NOVEMBER 30, 197t
SECTION 1
GENERAL
PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
I
2'6.m"
a
I
Wing Area (sq. ft.) 170.0
Min. Turning Radius (ft.)
(from pivot point to wingip) 31.0
THREE VIEW
Figure l-l
REPORT: VB-940
1-2
ISSUED: NOVEMBER 30, 197t
PIPER AIRCRAFT CORPORATION
pn-zrnr-zolT, TURBO ARROW lv
SECTION I
GENERAL
I.3 ENGINES
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model Number
(d) Rated HorsePower
(e) Rated SPeed (rPm)
(f) Maximum Manifold
Pressure (in. Hg)
(g) Bore (in.)
(h) Stroke (in')
ii) Disptacement (cu. in.)
0) ComPression Ratio
(k) Engine TYPe
ISSUED: NOVEMBER 30, 1978
REVTSED: SEPTEMBER 14' 1979
I
Teledyne Continental
TSIO-360-FB
200 Sea Level to 12,000
Ft. DensitY Altitude
2575
4t
4.438
3.875
360
7.5:l
Six CYlinder, Direct
Drive, HorizontallY
Opposed, Air Cooled,
Turbosupercharged and
Fuel lnjected
l
Hartzell
F8459A-8R
2
BHC-C2YF-l( )F
7b
75
Constant SPeed,
HydraulicallY Actuated
REPORT: VB-940
l-3
I.5 PROPELLERS
STANDARD
(a) Number of ProPellers
(b) ProPeller Manufacturer
(c) Blade Model
(d) Number of Blades
(e) Hub Modcl
(f) Propellcr Diamcter (in.)
(l) Maximum
(2) Minimum
(g) ProPeller TYPc
SEC'I'ION I
GENERAI-
I'I I'ER A ITICTIA IIT' CORPOR A'TION
t,A-28I1't-201't, TURBO ARROW tV
ot,'l'toNAl_
(a) Nurnllcl ol' l)r'opcllcrs
(b) l'r'opcllcl N4arrrrlircturcr'
(c) lllatlc Motlcl
(d) Nunrbcr ol'llladcs
(c) Hub Motlcl
(l) l'ropcllcr I )ianrctcr (in.)
(l) Maxinrrrrn
(2) Mirrirrrunr
(g) l'ropc'llcl l ypc
I.7 FUEI,
AVCAS ONI.Y
(a) l"ucl Capacity (U.S. gal.) (total)
(b) tJsablc fjucl (U.S. gal.) (total)
(c) I;ucl Gradc. Aviation
(l) Minirnurn Crade
(2) Altcrnatc liucls
1.9 OlL
(a) Oil Capacity (U.S. qts.)
(b) Oil Spccilication
(c) Oil Viscosity
RIil'0ll'l': V8-940
l-4
I
l'l a rtzcll
Ir766l-2 tt
^t
PHC-C3YF-r( )F
t6
72
Constant Spced,
I lyd raulically Actuatccl
100 Grecn or l00l-t
lllue Aviation Gratte
Itefer to latest rcvision
o[ Continental Service
Ilulletin "Fuel and Oil
Grades"
IJ
M l.ts-244
llefer to Section 8 -
paragraph S.19.
ISSUED: NOVIiMBItR 30, 1978
REVISIID; Jl.Jl,Y 16, l9ll4
77
72
PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SECTION I
GENERAL
I.13 STANDARD AIRPLANE WEIGHTS
Refer to Figure 6-5 for the Standard Empty Weight and the Useful
Load.
1.I5 BAGGAGE SPACE
(a) Compartment Volume (cu. ft.)
(b) Entry width (in.)
(c) Entry Height (in.)
1.T7 SPECIFIC LOADINGS
r.1I MAXIMUM WEIGHTS
(a) Maximum Takeoff Weight (lbs.)
(b) Maximum Landing Weight (lbs.)
(c) Maximum Ramp Weight (lbs.)
(d) Maximum Weights in Baggage
Compartment
(a) Wing Loading (lbs. per sq. ft.)
(b) Power Loading (lbs. per hp)
ISSUED: NOVEMBER 30, 1978
REYISED: JULY 15, 1982
2900
2900
2912
200
l7
r4.5
REPORT: VB-940
1-5
24
22
20
PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SECTION 2
LIMITATIONS
SECTION 2
LIMITATIONS
2.I GENERAL
This section provides the "FAA Approved" operating limitations,
instrument markings, r:olor 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 (VNE) - Do not exceed
this speed in any operation.
Maximum Structural Cruising Speed
(VNO) - 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 movements
above this speed.
At 2900 lbs. G.W.
At 1893 lbs. G.W.
193
ls2
186
148
124
97
t2l
97
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. Maneuver-
ing speed should not be exceeded while opera-
ting in rough air.
ISSUED: NOVEMBER 30, 1978
REVISED: JULY 15, 19t2
REPORT: VB-940
2-l
SECTION 2
LIMITATIONS PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SPEED
Maximum Flaps Extended Speed (VFE) -
Do not exceed this speed with the flaps
extended.
Maximum Landing Gear Extension Speed -
Do not exceed this speed when extending
the landing gear.
Maximum Landing Gear Retraction Speed -
Do not exceed this speed when retracting
the landing gear.
Maximum Landing Gear Extended Speed
(VLE) - 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-940
2-2
KIAS KCAS
r08 104
133 130
ln 109
r33 130
IAS
I93 KTS
152 KTS to
I93 KTS
66 KTS to
I52 KTS
6l KTS to
108 KTS
ISSUED: NOVEMBER 30, 197t
PIPBR AIRCRAFT CORPORATION
PA-28RT.201T, TURBO ARROW IV
SECTION 2
LIMITATIONS
2.7 POWER PLANT LIMITATIONS
(a) Number of Engines
(b) Engine Manufacturer
(c) Engind Model No.
(d) Engine Operating Limits
(l) Maximum Horsepower
(2) Maximum Rotation Speed (RPM)
(3) Maximum Manifold Pressure
(ln. Mercury)
(4) Maximum Oil Temperature
(e) Oil Pressure
Minimum (red line)
Maximum (red line)
(0 Fuel Pressure
Maximum (red line)
(g) Fuel (AVGAS ONLY) (minimurn grade)
(h) Number of Propellers
(i) Propeller Manufacturer
CI) Propeller Hub and Blade Modbl
(l) Optional (Three Blade)
(2) Standard (Two Blade)
(k) Propeller Diameter
(l) Optional (Three Blade)
Minimum
Maximum
(2) Standard (Two Blade)
Minimum
Maximum
(l) Blade Angle Limits
(l) Optional (Three Blade)
Low Pitch Stop
High Pitch Stop
(2) Standard (Two Blade)
Low Pitch Stop
High Pitch Stop
ISSUED: NOVEMBER 30, 1978
REVISED: JULY 16, 1984
I
Teledyne Continental
TSIO-360-FB
200
2575
!,1
240"b
IO PSI
100 PSr
19 PSI
100 orl00LL
Aviation Grade
I
Hartzell
PHC-C3YF-r( )F I
F7663-2R
BHC-C2YF-r( )F/
F84594-8R
72
76
75
76
13.2 ! .2
33t lo
t4.4 ! ,2"
29!1"
REPORT: VB-940
2-3
SECTION 2
LIMITATIONS PIPER AIRCRAFT CORPORATION
PA-2ERT-201T, TURBO ARROW IV
(m) RPM Restrictions (Two Bladed
Propeller Only)
2.9 POWER PLANT INSTRUMENT MARKINGS
(a) Tachometer
Green Arc (Normal Operating Range)
Red Line (Maximum Continuous
Power)
(b) Oil Temperature
Green Arc (Normal Operating Range)
Red Line (Maximum)
(c) Oil Pressure
Green Arc (Itormal Operating Range)
Yellow Arc (Caution Range) (Idle)
Yellow Arc (Caution Range)
(Start and Warm-Up)
Red Line (Minimum)
Red Line (Maximum)
(d) Fuel Pressure
Green Arc (Normal Operating Range)
Red Line (Maximum)
(e) Exhaust Gas Temperature (EGT)
Green Arc (Normal Operating Range)
Red Line (Maximum)
(0 Manifold Pressure
Green Arc (Normal Operating Range)
Red Line (Maximum)
REPORT: VB-940
2-4
Avoid Continuous
Ground Operation
1700-2100 RPM In
Cross/Tail Wind Over
IO KTS.
Avoid Continuous
Operation 2000-2200
RPM Above 32 Inches
Manifold Pressure.
500 to 2575 RPM
2575 RPM
l00o to 240"F
2400F
30 PSI to 80 PSI
IO PSI tO 30 PSI
80 PSI to 100 PSI
IO PSI
100 PSt
3.5 PSI to 19 PSI
I9 PSI
1200'F to l650oF
16500F
l0IN. to 4l IN.
4I IN.
HG
HG
ISSUED: NOVEMBER 30, 1978
PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SECTION 2
LIMITATIONS
2.II WEIGHT LIMITS
(a) Maximum Weight
(b) Maximum Ramp Weight
(c) Maximum Baggage
29OO LBS
29I2 LBS
2OO LBS
NOTE
Refer to Section 5 (Performance) for maximum
weight as limited by performance.
2.13 CENTER OF GRAVIT'Y LIMITS
89.0
85.0
Weight
Pounds
2900
2400
93.0
93.0
Forward Limit
Inches Aft of Datum
Rearward Limit
Inches Aft of Datum
NOTES
Straight line variation between points given.
The datum used is 78.4 inches ahead of the
wing leading edge at the intersection of the
straight and tapered section.
It, is the responsibility of the airplane owner
and the pilot to insure that the airplane is
properly loaded. See Section 6 (Weight and
Balance) for proper loading instructions.
2.15 MANEUVER LIMITS
No acrobatic maneuvers including spins approved.
ISSUED: NOVEMBER 30, 1978
REVISED: JULY 15,1982
REPORT: VB-940
2-5