SECTION 9
PA-28-181, ARCHER III SUPPLEMENT 23
ISSUED: JULY 12, 1995 REPORT: VB-1611
REVISED: FEBRUARY 14, 2006 7 of 36, 9-159
SECTION 2 - LIMITATIONS (continued)
C. CMAX CHART PAGE Limitations
The geographic referenced aircraft symbol must not be used for navigation.
NOTE
The aircraft symbol displayed provides supplemental
aircraft situational awareness information. It is not intended
as a means for navigation or flight guidance. The airplane
symbol is not to be used for conducting instrument
approaches or departures. Position accuracy, orientation,
and related guidance must be assumed by other means or
required navigation.
Operators with the optional CMax Chart Page must have back-up charts
available. Do not rely upon CMax charts as your sole source of navigation
information.
D. STANDBY ALTERNATOR Limitations
The standby alternator system is used in the event of primary alternator failure
and not for normal operations.
The standby alternator is limited to 20 amperes continuous output. Transient
operations of greater than 20 amperes for no more than 5 consecutive minutes
may be conducted.
NOTE
Certain flight maneuvers such as climbs and lower power
settings will result in an engine RPM less than 2500. Flight
conditions resulting in less than 2500 engine RPM will
reduce the standby alternator system capability and possibly
require load shedding to maintain a system voltage above 25
volts.
SECTION 9
PA-28-181, ARCHER III SUPPLEMENT 23
ISSUED: JULY 12, 1995 REPORT: VB-1611
REVISED: FEBRUARY 14, 2006 7 of 36, 9-159
SECTION 2 - LIMITATIONS (continued)
C. CMAX CHART PAGE Limitations
The geographic referenced aircraft symbol must not be used for navigation.
NOTE
The aircraft symbol displayed provides supplemental
aircraft situational awareness information. It is not intended
as a means for navigation or flight guidance. The airplane
symbol is not to be used for conducting instrument
approaches or departures. Position accuracy, orientation,
and related guidance must be assumed by other means or
required navigation.
Operators with the optional CMax Chart Page must have back-up charts
available. Do not rely upon CMax charts as your sole source of navigation
information.
D. STANDBY ALTERNATOR Limitations
The standby alternator system is used in the event of primary alternator failure
and not for normal operations.
The standby alternator is limited to 20 amperes continuous output. Transient
operations of greater than 20 amperes for no more than 5 consecutive minutes
may be conducted.
NOTE
Certain flight maneuvers such as climbs and lower power
settings will result in an engine RPM less than 2500. Flight
conditions resulting in less than 2500 engine RPM will
reduce the standby alternator system capability and possibly
require load shedding to maintain a system voltage above 25
volts.
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