Cessna 182 1978 - Page 105

MODEL 182 & T182 SERIES SERVICE MANUAL
CESSNA PROGRESSIVE CARE
MODEL 182 & T182
OPERATION NO. 4
MECHANIC INSPECTOR REMARKS
10. Alternator and Electrical Connections - Check condi-
tion and security.
Check alternator
belts for condi-
tion
and proper
adjustment.
11. Alternator Control Unit - Inspect wiring, mounting,
condition,
and wire
routing.
12. Firewall
Structure - Inspect for
wrinkles, damage,
cracks,
sheared
rivets, etc.
Check
cowl shock
mounts
for condition
and security.
13. Engine
Shock Mounts,
Engine
Mount Structure,
and
Ground
Straps - Check
condition, security,
and
alignment.
14. Exhaust System
(normally aspirated
engine) - In-
spect for cracks and
security. Air leak check
exhaust
system.
15. Exhaust System
(turbocharged engine)
- Inspect
couplings, seals,
clamps, and expansion
joints for
cracks,
condition, and
security. Air leak
check
exhaust system.
16.
Turbocharger
(if applicable)
-
a. Inspect
mounting
brackets,
ducting,
linkage,
and
attaching parts for
general condition,
leak-
age or
damage,
and security
of attachment.
b. Check waste
gate, actuator, controller,
oil and
vent lines, overboost
relief valve,
and compres-
sor housing for leakage,
apparent damage,
se-
curity of
attachment, and evidence
of wear.
Check waste gate
return spring for
condition
and security.
17. Turbocharger
(if
applicable)
-
a. Remove heat shields and inspect for burned
areas,
bulges or cracks.
Remove tailpipe and
ducting
-- inspect
turbine
for coking,
carboniza-
tion,
oil deposits, and turbine
impellers for
damage.
18.
Heater Components
-
Inspect all
components
for
condition and security.
19. Vacuum
Pump - Check for condition
and security.
Check vacuum system breather line for obstruc-
tions, condition,
and
security.
Sheet 7 of 14
Revision
1
2-73