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Piper TURBO ARROW III User Manual

Piper TURBO ARROW III
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SECTION III
INSPECTION
3-1. INTRODUCTION. This section provides instructions for conducting inspections. These inspections are
described in Paragraphs 3-4 and 3-5. Repair or replacement instructions for those components found to be
unserviceable at inspection may be found in the section covering the applicable aircraft system.
CAUTION
When working on engines, ground the magneto primary circuit before
performing any operation.
3-2. RECOMMENDED LUBRICANTS. Refer to Recommended Lubricants, Section II for Lubrication
Servicing Instructions.
3-3. INSPECTION PERIODS.
3-4. INSPECTION REQUIREMENTS. Required inspection procedures are listed in Table III-I. The
inspection procedure is broken down into eight major groups which are Propeller, Engine. Cabin, Fuselage and
Empennage, Wing, Landing Gear, Operational Inspection and General. The first column in each group lists the
inspection or procedure to be performed. The second column is divided into four columns indicating the
required inspection intervals of 50 hours, 100 hours, 500 hours, and 1000 hours. Each inspection of operation
is required at each of the inspection intervals as indicated by a circle (O). If an item is not entirely accessible or
must be removed, refer to the applicable section of this manual for instructions on how to gain access to
remove the item. When performing inspections, use the annual inspection form furnished by the Piper Service
Department, available through Piper Dealers or Distributors.
Revised: 10/18/83
1D2
* CHEROKEE ARROW III SERVICE MANUAL
INSPECTION

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Piper TURBO ARROW III Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelTurbo Arrow III
Horsepower200 hp
Max Takeoff Weight2, 900 lbs
Fuel Capacity72 gallons
Service Ceiling20, 000 ft
Seating Capacity4
TypeSingle-engine piston
PropellerConstant-speed
Landing Distance1, 200 ft

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