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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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J. Pass the lead through the proper hole in outlet plate. Position the Bendix l l-9596 or equivalent
Braid Cutting Back-up Tube between the braided shielding and insulation to protect the insulation.
Cut enough braid from the lead to have 1-1/4 inch of insulation extending from end of braid.
—CAUTION—
Be sure the cutting back-up tube is completely under the point at
which the cut is to be made to prevent cutting or nicking
insulaton.
K. Slide inner ferrule under the braid. The braid should cover approximately two-thirds of the ferrule
taper. Remove the blue silicone coating from the end of the braid over ferrule by lightly scraping
with a knife or wire brush.
—CAUTION—
When removing silicone coating, care should be taken not to
damage the braided wire shielding.
L. Pull the lead assembly through cable outlet plate until cleaned braid binds in the outlet well.
Position the Bendix ll-7074 Ferrule Seating Tool (Figure 74-15) over the insulation and firmly seat
the ferrule by tapping the seating tool with a hammer or by using an arbor press.
M. Measure l /2 inches from tapered ferrule and strip remaining insulation from wire. (Refer to Figure
74-16.)
N. Insert Bendix 11-7073 Needle (Figure 74-17) through the small hole of the grommet and over the
stripped end of the wire. (Refer to Figure 74-18.) Slide grommet down needle until it seats tightly
against the tapered ferrule.
O. Cut the wire 3/8 inch from the top of the grommet outlet. (See Figure 74-l9.) Double the wire over
as shown in A of Figure 74-20. Slide the eyelet over the doubled wire until it is firmly seated in
the recess of the grommet outlet.
THIS SPACE INTENTIONALLY LEFT BLANK
Effectivity 74-21-02
PA-28RT-201T Page 74-15
December 1, 1978
3E1
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

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Piper Arrow IV Turbo Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelArrow IV Turbo
Horsepower200 hp
Seating Capacity4
Landing GearRetractable tricycle
Range773 nautical miles
Service Ceiling20, 000 ft
Fuel Capacity72 gallons
Propeller2-blade constant speed
Max Takeoff Weight2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)55 knots
Rate of Climb1, 000 ft/min

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