Cessna T188C - Page 46

MODEL 188
& T188 SERIES
SERVICE MANUAL
I
SPECIAL INSPECTION ITEM
EACH 200 HOURS
EACH 100 HOURS
EACH 50 HOURS
21. Alternator,
belt,
support bracket
and electrical
connections
...........................
17
22. Alternator
brushes, brush
leads, commutator
or slip
rings............................
7
23. Voltage regulator mounting and electrical leads .....................................
24. Magnetos (external) and electrical
connections .....................................
25.
Magneto timing
................................................................
8
26. Carburetor and
drain plug .......................................................
·
27. Firewall
.......................................................................
28. Fuel injection fuel-air control
unit, fuel pump, fuel manifold valve, fuel lines
and nozzles .. ·
29. Fuel-air control unit screen ......................................................
30. Turbocharger.
...............................................................
·
31. All
oil lines to turbocharger .................
...............................
32. Turbocharger
pressurized vent
lines to fuel pump,
discharge nozzles and
fuel flow gage .
33. Turbocharger
mounting brackets ................................................
*
34. Turbocharger
oil
line check valves................................................
22
FUEL SYSTEM
1.
Fuel strainer, drain
valve and control
..............................................
2. Fuel strainer screen and bowl
....................................................
3. Fuel
tank/cell vents, caps
and placards ...........................................
0
4. Fuel tanks/cell, sump drains and fuel line drains ....................................
5. Drain fuel and
check tank/cell
interior, attachment
and outlet
screens ................
5
6. Fuel
vent valves ...............................................................
7. Vent
line drain .................................................................
8. Fuel
shut-off valve and
placards .................................................
e
9. Fuel quantity gage and transmitter
unit ............................................
10. Electric
fuel pump, throttle
switch and electric connections
...........................
·
11.
Engine primer ......... .. ..................
.............
12. Vapor return
line and check valve
................................
.. ...
13. Perform
a fuel quantity
indicating system
operational test.
Refer to Section
15
for detailed
accomplishment
instructions
........................................
24
14. Fuel
injection nozzles...........................................................
25
2-24
D2054-1-13 Temporary
Revision
Number 5 -
Apr 5/2004
© Cessna
Aircraft
Company