Piper ARCHER II Pilot Operating Handbook page 144

SECTION 7 PIPER AIRCRAFT CORPORATION
DESCRIPTION & OPERATION PA-28-181, ARCHER I]
FUEL SELECTOR
Figure 7-7
The fuel drains should be opened daily prior to first flight to check for
water or sediment and proper fuel. Each tank has an individual drain at the
bottom, inboard rear corner.
A fuel strainer, located on the lower left front of the fire wall, hasa drain
which is accessible from outside the nose section. The strainer should also be
drained before the first flight of the day. Refer to paragraph 8.21! for the
complete fuel draining procedure.
Fuel quantity and pressure are indicated on gauges located in a cluster
on the left side of the instrument panel.
An engine priming system ts provided to facilitate starting. The primer
pump is located to the immediate left of the throttle quadrant (refer to
Figure 7-5).
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REPORT: VB-1120 ISSUED: JULY 2 1979
7-8
REVISED: JUNE 29, 1984