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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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3. After resloshing, reinspect as above at intervals of 100 hours. These inspections may be discontinued
after the second inspection if no peeling is discovered.
—NOTE—
The fuel tank should be replaced if the tank is damaged to the
extent it cannot be repaired by the above method.
INSTALLATION OF FUEL TANK.
1. Slide the tank partly into position and connect the sender wire and fuel line. On PA - 2 8 RT- 2 0 1 T
connect vapor return line.
2. Slide the tank completely into place and secure with screws around its perimeter.
3. Fill the fuel tank and check for leaks, unrestricted fuel flow and proper sender indications on the
quantity gauge. Refer to Fuel Quantity Sender/Gauge Check (Installed).
—NOTE—
Refer to latest revision of Piper Service Bulletin 625A; Fuel and
Vapor Return Lines Support.
DISASSEMBLY OF LOCKING FUEL CAP. (Refer to Figure 28-4.)
1. Remove two screws on back of fuel cap.
2. Remove screw which secures the pawl to the back of key lock assembly.
3. Remove pawl from back of key lock assembly.
4. Remove nut which secures key lock to cover.
5. Slide lock, gasket and spring over back of key lock.
6. The key lock may be removed by pushing key lock through cover.
ASSEMBLY OF LOCKING FUEL CAP.
1. Insert key lock through cover making sure that O-ring is installed under head of key lock.
2. Slide spring, gasket and lock over back of key lock.
3. Reinstall nut which secures key lock to cover.
4. Attach pawl to back of lock assembly with screw previously removed.
5. Apply Loctite 721 to threads of screws previously removed from back of fuel cap, then install screws
in back of fuel cap.
28-10-05
Page 28-08
Revised: July 13, 1983
2B3
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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