Cessna Cardinal RG 1974, Руководство пользователя, Страница: 133 / 226

Cessna Aircraft Company
Model 177RG Supplement No.
DP-014-22
Section 9
Supplements Page 9
Revision 0
developed under nonstandard conditions may be greater.
Errors that develop will be self corrected by the internal
erection system or manually corrected by the actuation of the
caging system.
- Acceleration & Deceleration Errors - Pitch indicating errors
may occur due to accelerations experienced during takeoff,
climb-out, descent, and landing. Errors that develop will be
self-corrected by the internal erection system or manually
corrected (in straight and level flight) by the actuation of the
caging system.
- Taxiing Errors - A pitch and roll indicator display error of
approximately 1° will occur during a sudden 90° gro und turn. A
pitch indicator display error of approximately 2° w ill occur
during a sudden 180° ground turn. Errors that devel op will be
self corrected by the internal erection system or manually
corrected by the actuation of the caging system.
- Pitch Indicator Fluctuation (Bar Jitter) - Vertical fluctuation (
⋅⋅⋅⋅⋅⋅⋅⋅
)
of the pitch indicator display will not exceed 0.012 inch total
when the range of indication is from 0° to ± 20°. W hen the
indicating range is beyond ± 20° the total fluctuat ion will not
exceed 0.08 inch.
SECTION 8
HANDLING AND MAINTENANCE
No Change.
UNCONTROLLED
COPY
WHEN
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