Piper Lance II User Manual

SECTION IX
FUEL SYSTEM
Aerofiche
Grid No.Paragraph
9-1. Description
..................
9-2. Troubleshooting
..................................
9-3. Fuel Tanks ................ .. .. .......... .
9-4. Inspection and Repair
of Fuel Tanks ................
9-5. Removal of Inboard Fuel Tank ...................
9-6. Installation of Inboard Fuel Tank ..................
9-7. Removal of Outboard Fuel Tank ..................
9-8. Installation of Outboard Fuel Tank .................
9-9. Inspection of Fuel System ............................
9-10. Fuel
Quantity Sender Unit ............................
9-11. Fuel
Quantity Sender/Gauge Check
(Installed) ................
9-12. Fuel
Selector Valve and Filter ..........................
9-13. Fuel Selector Valve Operation ....................
9-14. Removal of Fuel Selector Valve and Filter .............
9-15 Cleaning Filter Assembly .......................
9-16. Installation of Fuel Selector and Filter Valve ...........
9-17. Cleaning
Fuel System ...............................
9-18. Electric Fuel Pump ......... ......................
9-19. Removal and
Installation of Electric Fuel Pump
..........
2D13
2D13
2D16
2D16
2D16
2D17
2D17
2D17
2D17
2D18
2D18
2D20
2D20
2D20
2D21
2D22
2D22
2D22
2D22
Revised:
9/2/78
2D12

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers