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

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

SECTION 2
LIMITATIONS PIPER AIRCRAFT CORPORATION
PA,2tRT-201T, TURBO ARROW IV
2.I9 TYPES OF OPERATIONS
The airplane is approved for the following operations when equipped in
accordance with FAR 9l or FAR 135.
2.T7 FLIGHT LOAD FACTORS
(a) Positive Load Factor (Maximum)
(b) Negative Load Factor (Maximum)
(a) Day V.F.R.
(b) Night V.F.R.
(c) Day I.F.R.
(d) Night I.F.R.
(e) Non Icing
2.2I FUEL LIMITATIONS
(a) Total Capacity
(b) Unusable Fuel
The unusable fuel for this airplane has
been determined as 2.5 gallons in each
wing tank in critical flight attitudes.
(c) Usable Fuel
The usable fuel in this airplane has
been determined as 36.0 gallons in each
wing tank.
(d) Fuel remaining when the quantity indi-
cators read zero cannot be used safely
in flight.
REPORT: VB-940
2-6
3.8 c
No inverted maneuvers
approved
77 U.S. GAL.
5 U.S. GAL.
72 U.S. GAL
2.23 OPERATING ALTITUDE LIMITATIONS
- Flight above 20,000_feet is not approved. Flight up to and including
10:q00 feet is approved if equipped-with oxygän in accordance with
FAR 23.lzl4l and avionics in accordance with FAR 9l or FAR 135.
ISSUED: NOVEMBER 30, t9Z8

PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SECTION 2
LIMITATIONS
2.25 NOISE LEVEL
The noise level of this aircraft is 69.4 d B(A) for two bladed propeller
installations and 72.8 d B(A) for three bladed propeller installations.
No determination has been made by the Federal Aviation Administra-
tion that the noise levels of this airplane are or should be acceptable or
unacceptable for operation at, into, or out of, any airport.
The above statement not withstanding the noise level stated above has
been verified by and approved by the Federal Aviation Administration in
noise level test flights conducted in accordance with FAR 36, Noise
Standards - Aircraft Type and Airworthiness Certification. This aircraft
model is in compliance with all FAR 36 noise standards applicable to this
type.
REPORT: VB-940
2-7
ISSUED: NOVEMBER 30, 1978

SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-28RT.2OIT, TURBO ARRO1V IV
2.27 PLACARDS
In full view of the pilot:
THIS AIRCRAFT MUST BE OPERATED AS A NOR-
MAL CATEGORY AIRPLANE IN COMPLIANCE
WITH THE OPERATING LIMITATIONS STATED
IN THE FORM OF PLACARDS, MARKINGS AND
MANUALS.
THIS AIRCRAFT APPROVED FOR NIGHT I.F.R.
NON-ICING FLIGHT WHEN EQUIPPED IN
ACCORDANCE WITH FAR 9I OR FAR I35.
In full view of the pilot, the following Takeoff Check List and one of the
following Landing Check Lists will be installed:
TAKEOFF CHECK LIST
Fuel on Proper Tank
Auxiliary Fuel Pump Off
E4gine Gauges Checked
Alternate Air Closed
Seat Backs Erect
Mixture Set
Propeller Set
Fuel on Proper Tank
Seat Backs Erect
Fasten Belts/ Harness
Aux. Fuel Pump Off
Mixture Rich
Fasten Belts/ Harness
Flaps Set
Trim Tab Set
Controls Free
Doors Latched
Air Conditioner Off
LANDING CHECK LIST
REPORT: VB-940
2-8
Propeller Set
Gear Down (133 KIAS Max.)
Flaps Set (108 KIAS Max.)
Air Conditioner Off
ISSUED: NOVEMBER 30, 1978
REVISED: SEPTEMBER 14, 1979

PIPER AIRCRAFT CORPORATION
PA-28RT-201T, TURBO ARROW IV
SECTION 2
LIMITATIONS
LANDING CHECK LIST
Fuel on Proper Tank
Seat Backs Erect
Fasten Belts/ Harness
Aux. Fuel Pump Off
Mixture Rich
ISSUED: NOVEMBER 30, l9lt
REVISED: SEPTEMBER 14, 1979
Propeller Set
Gear Down
Flaps Set (White Arc)
Air Conditioner Off
The "Air Conditioner Off item in the above Takeoff and Landing
Check Lists is mandatory for air conditioned aircraft only.
On the instrument panel in full view of the pilot:
MANEUVERING SPEED I24 KIAS
AT 2900 LBS. (SEE A.F.M.)
or
vA t24 AT 2900 LBS. (SEE P.O.H.)
On the instrument panel in full view of the pifot:
DEMONSTRATED CROSSWIND COMPONENT 17, KTS
or
DEMO. X-WIND 17 KTS
In full view of the pilot:
NO ACROBATIC MANEUVERS,
INCLUDING SPINS, APPROVED
On the instrument panel in full fiew of the pilot:
GEAR DOWN 133 KIAS (MAX.)
GEAR UP III KIAS (MAX.)
EXTENDED 133 KIAS (MAX')
or
VLO I33 DN, III UP VLE I33 MAX.
REPORT: Y&,9a0
'"9

SECTION 2
LIMITATIONS PIPER AIRCRAFT CORPORATION
PA.28RT.2O1T, TURBO ARROW IV
Near emergency gear lever:
EMERGENCY DOWN
Near emergency gear lever (aircraft equipped with backup gear
extender):
OVERRIDE ENGAGED AUTO-EXT-OFF
LOCK PIN ON SIDE
TO ENGAGE OVERRIDE:
PULL LEVER FULL UP, PUSH LOCK PIN
TO RELEASE OVERRIDE:
PULL LEVER FULL UP & RELEASE
Near gear selector switch
GEAR UP
DOWN II I KIAS MAX.
I33 KIAS MAX.
ISSUED: NOVEMBER 30, 197t
REVISED: AUGUST 15, I9t5
Adjacent to upper door latch:
ENGAGE LATCH BEFORE FLIGHT
In full view of the pilot
WARNING
TURN OFF STROBE LIGHTS WHEN IN
CLOSE PROXIMITY TO GROUND OR
DURINC FLIGHT THROUGH CLOUD,
FOG OR HAZE,
In full view of the pilot, in the area of the air conditioner controls when
the air conditioner is instailed:
WARNING
AIR CONDITIONER MUST BE OFF TO
INSURE NORMAL TAKEOFF CLIMB
PERFORMANCE.
REPORT: VB-940
2-10

PIPER AIRCRAFT CORPORATION
PA.2!RT.2OIT, TURBO ARROW IV
SECTION 2
LIMITATIONS
On insidc ol' baggage compartment door:
BAGGAGE MAXIMUM 2OO LBS. SEE WEIGHT AND
BALANCE DATA FOR BAGGACE LOADINC BE-
TWEEN I50 LBS. AND 2OO LBS.
ln lull view of the Pilot
FUEL REMAINING WHEN QUANTI-I-Y INDICATOR
READS ZERO CANNOT BE USED SAFELY IN
FLIGHl"
On the instrument panel in full view of the pilot in aircraft with two
bladed propeller installations only:
AVOID CONTINUOUS GROUND OPERATION ITOO-
2IOO RPM IN CROSS;TAIL WIND OVER IO KTS.
AVOID CONTINUOUS OPERATION 2OOO-2200 RPM
ABOVE 32" MANIFOLD PRESSURE.
On the aft baggage closeout:
MAXIMUM BAGGAGE 2OO LBS. NO HEAVY
OBJECTS ON HAT SHELF.
ISSUED: NOVEMBER 30' 1978
REVISED: AUGUST t, l9t3
REPORT: VB-940
2-ll

SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-28RT.2OIT, TURBO ARROW IV
Adjacent to fuel tank filler caps (Prior to serial number 28R-8031031)
FUEL - l00l130 AVTATTON GRADE - MIN. USABLE
CAPACITY 36 GAL.
USABLE CAPACITY TO BOTTOM OF FILLER
NECK IIT"DICATOR 25 GAL.
Adjacent to fuel tank filler caps (Serial numbers 28R-8031031 and up):
FUEL - IOO OR IOOLL AVIATION GRADE
(Serial numbers 28R-8331015 and up)
AVGAS OI{LY
ss
GRADE
rooLt GBADE
roo
REPORT: VB-940
2-12
ISSUED: AUGUST 8, 1983

PIPER AIRCRAFT CORPORATION SECTION 3
PA-28RT-201T, TURBO ARROW tV EMERGENCY PROCEDURES
SECTTON 3
EMERGENCY PROCEDURES
3.T GENERAL
The recommended procedures for coping with various types of
emergencies and critical situations are provided by this section. All of the
required (FAA regulations) emergency procedures and those necessary for
operation of the airplane as determined by the operating and design features
of the airplane are presented.
Emergency procedures associated with those optional systems and
equipment which require handbook supplements are provided in Section 9
(Supplements).
The first portion of this section consists of an abbreviated emergency
check list which supplies an action sequence for critical situations with little
emphasis on the operation of systems.
The remainder of the section is devoted to amplified emergency
procedures containing additional information to provide the pilot with a
more complete understanding of the procedures.
These procedures are suggested as a course of action for coping with the
particular condition described, but are not a substitute for sound judgment
and common sense. Pilots should familiarize themselves with the
procedures given in this section and be prepared to take appropriate action
should an emergency arise.
Most basic emergency procedures, such as power off landings, are a
normal part of pilot training. Although these emergencies are discussed
here, this information is not intended to replace such training, but only to
provide a source of reference and review, and to provide information on
procedures which are not the same for all aircraft. It is suggested that the
pilot review standard emergency procedurer periodically to remain
proficient in them.
ISSUED: NOVEMBER 30, 197t
REVISED: JULY 16, tr9t4
REPORT: Y&9a0
9r

SECTION 3 PIPER AIRCRAFT CORPORATION
EMERGENCY PROCEDURES PA-2tRT-20IT, TURBO ARROW IV
3.3 EMERGENCY PROCEDURES CHECK LIST
ENGINE FIRE DURING START
Starter. crank engine
. idle cut-offMixture
Throttle olrcn
Primer. ..... oFF
Fuel sclcctor OFF
Abandon if lire continues.
ENGINE POWER LOSS DURING TAKEOFF
If sufficient runwsy remains for a normal landing, lcarr gcardown and land
straight ahead.
If area ahead is rough, or if it is neccssary to clear obstructions:
Gear selector switch ..... uP
Emcrgcncy gcar levcr (aircraft cquippcd
with backup gcar extendcr).... locked in OVERRIDE
ENGAGED position
If suflicient altitude has been gained to attempt a restart:
Maintain safe airspeed.
Fuel selcctor . . . switch to tank
containing fucl
Auxiliary fuel pump... unlatch, HI
chcck RICHMixture
Altcrnate air OPEN
.. as requircdEmergcncy gear lever
If power is not rcgained, procced with power off landing
ENGINE POWER LOSS IN FLIGHT
Fuel selector switch to tank
containing fuel
Auxiliary fuel pump ..... unlatch, Hl
Mixture .. RICH
Alternate air ... . OPEN
Engine gauges ... check for indication
of cause of power loss
If no fuel pressure is indicated, check tank selector position to be surc it is on
a tank containing fuel.
REPORT: VB-940
3-2
ISSUED: NOVEMBER 30, 1978
REVISED: AUGUST 15, 1986

PIPER AIRCRAFT CORPORATION SECTION 3
PA-2IRT.2OIT, TURBO ARROW IV DMERGENCY PROCEDURES
When powcr is restored:
Alternatc air CLOSED
Auxiliary fucl pump. OFF
If powcr is not restored prepare for powcr off landing.
Trim for 97 KIAS.
POWER OFF LANDING
On aircraft cquippcd with thc backup gcar extender, lock emergency gear
lcvcr in OVERRIDE ENGAGED position beforc airspced drops to 106
KIAS to prevcnt the landing gcar from frcc falling.
Trim for 97 KIAS.
Locatc suitsblc lield.
Establish spiral pattcrn.
1000 ft. above ficld at downwind position for normal landing approach.
When ficld can easily bc easily rcached slow to 75 KIAS for shortcst landing.
GEAR DOWN EMERGENCY LANDING
Touchdowns should normally be made at lowest possible airspeed with full
flaps.
Whcn committcd to landing:
Landing gcar sclector
Throttlc
Mixturc ....
Ignition
Mastcr switch
Fucl sclcctor
Scat bclt and harncss.,..
GEAR UP EMERGENCY LANDING
In thc evcnt a gcar up landing is required, procced as follows
Flaps . . .
'Ihrottlc
Mixturc
lgnition switchcs
Master switch
Fuel selector
Seat bclt and harness
Contact surface at minimum possible airspeed.
ISSUED: NOVEMBER 30, l97E
REVISED: AUGUST 15, l9t6
. Down
.. close
.. idle cut-off
. OFF
. OFF
. OFF
.... as desired
. . close
... idle cut-off
.. OFF
tight
OFF
tight
.... oFF
REPORT:940
3-3