TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter71 Power Plant
Issue: 28.FEB 2017 Page 171
61 Propeller
The propeller used is the 3 blade, ground-adjustable, NEUFORM CR3-
65-(IP)-47-101.6. The blade angle of each propeller blade is 22° +/-
0,5° at 425 mm from blade foot.
NOTE The propeller is approved as part of aircraft. All maintenance, repair
and overhall must be coordinated with TOMARK.
For additional information see Chapter
01-30 Related Publications
of
this Manual for referenced NEUFORM Documents.
61-10-01 Propeller Blade
Blade Angle Measuring
▶ Ensure power and ignition off.
▶ Bring applicable blade to horizontal position.
▶ Measure blade angle at 425 mm from blade foot by placing a
conventional protractor from blade edge to edge (22° +/- 0,5°).
Adjusting the Blade Angle
Refer to NEUFORM-Adjustable Pitch Propeller Operating Manual,
Assembly instructions/Adjusting the blade angle. (
See Chapter
01-30
Related Publications
)
61-10-02 Spinner
The spinner is attached to the propeller with 6 screws.
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