Piper ARCHER III Pilot Operating Handbook page 235

PA-28-181, ARCHER ill
•
7.19 FUEL SYSTEM (continued)
.......----
-----
-
•
-::::---
,---
,---_,..;:-�
An auxiliary electric fuel pump is provided in case of failure of the engine
driven pump. The electric pump should be on for all lakeoffs and landings, and
when switching tanks. The pump switch is located in the switch panel above the
throttle quadrant.
The fuel drain is provided at the lowest, inboard corner of each wing
lank. An engine fuel strainer is accessible through the exterior, lower, left nose
section. Each fuel drain and strainer should be opened and the fuel checked for
•
contamination prior to the first flight of the day or after each refueling. Refer to
paragraph 8.21 e for fuel draining procedure .
ISSUED: December 22, 2017
L_
1
-
-
�
�J
�\
--
�
FUEL SELECTOR
DESCRIPTION & OPERATION
-
-·
,;,-
---
::::----
Figure 7-5
SECTION 7
�
;::;,-:_
�
7_;..,-
/
'./"'l
-�
/'/
---
;,/
----
- �
REPORT: VB-2749
7-47