AUTO GYRO Cavalon Maintenance Manual page 251

62-11-00 6-2 INSPECTION: ROTOR BLADES
GENERAL, REFERENCES AND REQUIREMENTS
Basic operational task, which can be performed by a licensed pilot or instructed personnel!
Rotor system must be disassembled, see
SPECIAL TOOLS AND CONSUMABLE MATERIALS
85-00-00-S-35077 Aluminium ruler 1000mm
PRECAUTIONS AND SAFETY MEASURES
WARNING: Do not use permanent marker on anodized (eloxated) parts!
CAUTION: Do not use sticky labels on aluminium or composite parts as they may be difficult to remove!
PROCEDURES
1 Inspect for cracks in the blade root area, especially in the area of the inner attachment bore (see Fig. 1
"Critical Area"). In case of any cracks the complete rotor system must be replaced.
2 Check each rotor blade in its root section for linearity. In order to do place each rotor blade with the nose
section facing down on the support stands and measure gap with an aluminium ruler in 1 meter distance from
the inner end (see Fig. 2). Maximum allowed gap (dimension A) is 0.5 mm (LTA DULV-2010-004).
IMPORTANT NOTE: In order to avoid measuring errors draw a straight and parallel line 200
mm from the trailing edge. Use a lead pencil. Do not use permanent marker on anodized
(eloxated) parts!
AMM-CV-915iS/916iS-EN-
E-2023-12
Aircraft
Maintenance Manual
62-11-00 4-2
Part E - 62-11-00 6-2
AutoGyro
Cavalon 915 iS / 916 iS
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