Figure 1-17.
TM 55-2840-231-23
Section V. PREVENTIVE MAINTENANCE INSPECTIONS
P a g
e
Pressurized Container - Inspection
Engine Container - Internal Pressure and Humidity Check
Special Inspections
Turbine Overtemperature - Inspection
Compressor - Special Inspection
Abnormal Flight Maneuver Inspection
Inspection After Inflight Auto Reignition Operation
1-52
1-55
1-56
1-57
1-59
1-63
1-65
1-40. Pressurized Container - Inspection
INITIAL SETUP
Applicable Configuration
References
All
TB 55-8100-200-25
Para 1-36
Table 1-5
LOCATION/lTEM
REMARKS
ACTION
ENGINE CONTAINER/
Immediately upon receipt of an engine
at an activity and every 90 days (or more
frequently) thereafter, check the relative
humidity indicator and the internal pres-
sure of the container in accordance with
table 1-5.
1-52
