Supplement Airplane Maintenance Manual
Cessna 172 with TAE 125-02-99 / -114
AMM-20-02
Rev. No:
Rev. Date:
Chapter:
Issue:
Issue Date:
Page:
Content:
20-AMM-05-02
3
06.11.2013
3
8
1
25.08.2014
5.20.01
Checks dependent on engine operating time:
After initial 3rd - 6th operating hour
•
Further maintenance action according to Operation and
Maintenance Manual OM-02-02
Every 100 operating hours / Annual Inspection
•
Check engine mount for signs of corrosion (refer to Chapter
71, Section 71.20, Maintenance Practices)
•
Check coolant "WATER LEVEL" signal (refer to Chapter 31,
Section 31.60, Maintenance Practices) and perform
„coolant tank cap pressure relief test“ (refer to Chapter 75,
Section 75.00, Maintenance Practices)
•
Check if the turbocharger clamp can be moved easily and
inspect for cracks. Check turbocharger hoses for damages
(chafe marks, cracks, etc.), especially damaged fabric.
•
Visual inspection of the joints (e.g. hose connections)
•
Replace fuel filter (refer to Chapter 28, Section 28.20,
Maintenance Practices)
•
Check airplane fuel pump (Cessna R/S only, refer to
airplane manufacturer´s specifications)
•
Check electrical fuel pump (refer to manufacturer's
specifications)
•
Further maintenance action according to Operation and
Maintenance Manual OM-02-02
•
Inspect FADEC backup battery (refer to Chapter 24,
Section 24.30, Maintenance Practices)
Every 200 operating hours
•
Work as described for every 100 operating hours
•
Further maintenance action according to Operation and
Maintenance Manual OM-02-02
Every 300 operating hours
•
Work as described for every 100 operating hours
•
Further maintenance action according to Operation and
Maintenance Manual OM-02-02
•
Inspect the turbocharger clamp (refer to Chapter 71,
Section 71.60, Maintenance Practices)
Summary of Contents for Cessna 172
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