Supplement Airplane Maintenance Manual
Cessna 172 with TAE 125-02-99 / -114
AMM-20-02
Chapter:
Issue:
Issue Date:
Page:
Content:
20-AMM-71-02
3
06.11.2013
8
46
Rev. No:
Rev. Date:
1
25.08.2014
Valve spring installed height: ............ 32.5 mm (1.28 in)
Max. fuel pressure:............................ 1350 bar (19580 psi)
Oil system:
Oil pump: ........................................... 1 stage
Tappet clearance compensation: ...... Hydraulic
Type of cam timing drive: .................. Chain
TROUBLESHOOTING
To isolate a fault, proceed as follows:
"Sensor Properties" and "Actuator Control Signal" are separately
provided files. They contain information relevant to tasks in the
"corrective action" column.
Step
Action
1
Select the “Fault Isolation“ Tab
2
Find the heading appropriate to the fault
3
Find the symptom which best describes the
abnormality
4
Follow the instruction in the verify column
5
If the Item passes the check, proceed to the next line
6
If an item fails a check, perform the appropriate
corrective action
Note:
Always proceed from top to bottom, and perform checks and
corrective actions in the specified order.
Summary of Contents for Cessna 172
Page 8: ......
