SEGTIGN7
AI RPLANE&' SYSTEMS-DESCRIPTION
NOTE
CESSNA
MODEL
172S
i
I
When
.the
fuel .tanks
are
1/4'
'full" or . less,
prolonged'
uncoordinated
flight such as slips
or skids can uncover the
fuel tank outlets. Therefore,
if operating' with one fuel tank
dry or if operating on LEFT or RI~HT tank when
1/4
full or
less, do not allow the airplane to remain- in uncoordinated
flight for periods in excess of 30 seconds.
FUEL DRAIN VALVES
The fuel system 'is equipped with drain valves to provide a means
for the examination
of fuel in :the' system
for contamination
and
grade. The sYstem should be examined before each flight and after
each refueling, by 'using the sampler cup:provided
to drain fuel from
each wing tank sump, the fuel reservoir
sump, the fuel selector
drain . and
the
fuel
strainer,
sump.
If
any
evidence
of
fuel
contamination
is found, it must be eliminated
in accordance with the
Preflight Inspection checklist and the discussion
in Section 8 of this
publication .. If takeoff weight limitations for the next flight permit, the
fuel tanks should be filled after each flight to prevent condensation.
,
-
.'
7-28
July
8/98
:
;
Summary of Contents for Cessna 172S Skyhawk SP
Page 1: ...E c o q 9 E E t o c UF lrsBf II 8E r P c f r...
Page 5: ...j l 1 1 J i j...
Page 7: ...l...
Page 9: ...t I j j...
Page 29: ......
Page 35: ...1 I j...
Page 49: ...c i I II i i l j 1 1...
Page 73: ...i J j I 1...
Page 77: ...I r...
Page 111: ...1 t...
Page 133: ......
Page 135: ...i I i J...
Page 159: ...I J I I I...
Page 163: ...1...
Page 187: ...j J...
Page 239: ......
Page 257: ...I i II I j I I I I j ___ ill...
Page 267: ......
Page 277: ......
Page 287: ...I 1 I 1 i 1 I j I II I 1 j 1 j I 1 I...
Page 307: ...if f fC...
Page 323: ...I I...
Page 405: ......
Page 413: ......
Page 435: ......
Page 457: ...dt t q q...
Page 465: ......
Page 485: ......
Page 489: ...i...