ARROW II
FUEL SYSTEM
The fuel system was designed with simplicity in mind. It incorporates two fuel tanks, one
in each wing containing twenty-five (25) U.S. gallons, giving a total of 48 usable gallons. The
tanks are attached to the leading edge of the wing with screws and are an integral part of the
wing structure. This allows for easy removal for service. An auxiliary electric fuel pump is
provided in case of a failure of the engine driven pump. A rocker type switch for controlling the
electric pump is located on the switch panel above the throttle quadrant. The electric pump
should be on for take-off, switching tanks and during landing.
The fuel tank selector, which allows the pilot to control the flow of fuel to the engine, is
located on the left side wall below the instrument panel. It has three positions: OFF, LEFT
TANK and RIGHT TANK. The arrow on the handle of the selector points to the tank which is
supplying fuel to the engine. The valve also incorporates a safety latch which prevents
inadvertently selecting the "OFF" position.
Each tank has an individual quick drain located at the bottom inboard rear comer. The
fuel strainer also incorporates a quick drain which is located in the left front comer of the
firewall. The quick drain protrudes from the cowling to allow easy draining of the fuel strainer.
All three drains should be drained before every flight and checked for contamination.
The fuel tanks are vented individually by a vent tube which protrudes below the bottom of
the wing at the rear outboard corner of each fuel
tank.
The vent should be checked periodically
to ascertain that the vent is not obstructed and allows free passage of air.
Fuel quantity and pressure are indicated on gauges located in the instrument cluster to the
left of the switch panel.
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AIRPLANE AND SYSTEMS
ISSUED: November 15, 1971
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Fuel Selector
N16422 POH
Содержание Cherokee Arrow II
Страница 34: ...ARROW II OVERRIDE LATCH 2 4 Throttle Quadrant Console AIRPLANE AND SYSTEMS REVISED August 30 1973 N16422 POH...
Страница 37: ...AIRPLANE AND SYSTEMS ISSUED Novemoer 15 1971 Main Wheel Assembly ARROWil BRAKE HOUSING 2 7 N16422 POH...
Страница 47: ...AIRPLANE AND SYSTEMS ISSUED November 1s 1971 Static System ARROW IT 2 17 _ I N16422 POH...
Страница 52: ...ARROW II 2 22 THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED November 15 1971 N16422 POH...
Страница 100: ...ARROW TIDS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE S 30 MODEL PA 28R 200 l UED October 14 1971 N16422 POH...
Страница 112: ...ARROW II 6 8 THIS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED November 15 1971 N16422 POH...
Страница 113: ...THJS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 ARROW 11 6 9 N16422 POH...
Страница 114: ...ARROWD 6 10 Tms PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 N16422 POH...
Страница 138: ...ARROW II 9 10 THIS PAGE INTENTIONALLY LEFT BLANK a I l j I HANDLING AND SERVICING ISSUED November 15 1971 u J N16422 POH...