SECTION 9
SUPPLEMENT 21 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-140, 2 of 4 REVISED: SEPTEMBER 12, 2005
SECTION 1 - GENERAL
This supplement supplies information necessary for the operation of the airplane
when the optional Mid-Continent model 4300-XXX Electric Attitude Indicator
is installed in accordance with FAA Approved Piper data. For additional
information refer to the Mid-Continent Instruments Pilot’s Guide, manual
number 9015834, revision NR, or later revision.
SECTION 2 - LIMITATIONS
1. The emergency battery must be checked for proper operation prior to
flight.
2. Should the RED TEST annunciator illuminate any time during the self
test, this is an indication that the battery pack is in need of charging, or
possible replacement. Flight in Instrument Meteorological Conditions
(IMC) is prohibited.
3. Internal battery should be used for emergency use only.
SECTION 3 - EMERGENCY PROCEDURES
Loss of Aircraft Electrical System
Standby (STBY) Power Button........................................................SELECT
CAUTION
The STBY PWR annunciator will rapidly flash for
approximately one minute when aircraft power is lost.
STBY PWR must be selected, otherwise the gyro will auto
shutdown after approximately one minute.
Maintain attitude control using standby gyro.
SECTION 9
SUPPLEMENT 21 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-140, 2 of 4 REVISED: SEPTEMBER 12, 2005
SECTION 1 - GENERAL
This supplement supplies information necessary for the operation of the airplane
when the optional Mid-Continent model 4300-XXX Electric Attitude Indicator
is installed in accordance with FAA Approved Piper data. For additional
information refer to the Mid-Continent Instruments Pilot’s Guide, manual
number 9015834, revision NR, or later revision.
SECTION 2 - LIMITATIONS
1. The emergency battery must be checked for proper operation prior to
flight.
2. Should the RED TEST annunciator illuminate any time during the self
test, this is an indication that the battery pack is in need of charging, or
possible replacement. Flight in Instrument Meteorological Conditions
(IMC) is prohibited.
3. Internal battery should be used for emergency use only.
SECTION 3 - EMERGENCY PROCEDURES
Loss of Aircraft Electrical System
Standby (STBY) Power Button........................................................SELECT
CAUTION
The STBY PWR annunciator will rapidly flash for
approximately one minute when aircraft power is lost.
STBY PWR must be selected, otherwise the gyro will auto
shutdown after approximately one minute.
Maintain attitude control using standby gyro.
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