Raytheon Beech Baron E55 - Page 434

OPEN
END
PRESSURE
WATER
REOULAfOR-~
MANOMETER
WE~
WING
IIP
CLEAN
COMPRESSED
AND/OR
FILTERED
AIR
PRESSURE
SOURCE
OF
PLUGS
3.13
f0.25
PSIO
FOR
5
MINUTES.
~crl
Figure
9-19.
Leak
Test
Sa-up (TH-669
and
after).
RUNNING
LEAK
1~3
I
f
3/4"
DIA.
I
o
4"c5"DIA.
STAIN
1
11/2"DIA.
o
i
i
6"
MAX.
SEEP
3
1/2"
-4"
DIA.(
O
I
J_i
AREA
WHERE
FUEL
APPEARS TO
FLOW
OR
RUN,
FOLLOWING
CONTOUR
Or
SKIN
WHEN THIS AREA
IS WIPED
DRY.
FUEL
WILL
USUALLY
BEGIN
TO
DRI
HEAVY SEEP
AFTER
REACHING
THIS
POINT.
~160-281-23
Figure
9-20.
Leekege
of
Wa
Wing np
Fuel
Ceil,
(TH-669
and
after).
923