SECTION 9
SUPPLEMENT 22 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-146, 4 of 10 REVISED: SEPTEMBER 12, 2005
SECTION 4 - NORMAL PROCEDURES (continued)
To perform the preflight checklist and self test:
• After successful self test, press the mode control until ANT is displayed and
input a predetermined frequency to select a station in the immediate area.
Adjust the volume control as necessary to provide a comfortable listening
level.
• Press the ID button and observe that the station identification code becomes
louder (if the station is voice-identified, it is not necessary to press the ID
button).
• Press the ID button again to cancel the IDENT function and press the mode
control until ADF is displayed.
• Observe the IND-650A Indicator and note that the bearing pointer
indicates the relative bearing to the station.
• Push the TEST button while observing the indicator bearing pointer. The
bearing pointer will rotate 90° and stop.
• Push the TEST button again (to turn off test function). The bearing
pointer returns to the original relative bearing position.
• Switch to BFO mode, if appropriate, and verify a tone is present. Select the
appropriate operating mode when all checks have been completed.
SECTION 5 - PERFORMANCE
No change.
SECTION 6 - WEIGHT AND BALANCE
Factory installed optional equipment is included in the licensed weight and
balance data in Section 6 of the Pilot’s Operating Handbook and Airplane Flight
Manual.
SECTION 9
SUPPLEMENT 22 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-146, 4 of 10 REVISED: SEPTEMBER 12, 2005
SECTION 4 - NORMAL PROCEDURES (continued)
To perform the preflight checklist and self test:
• After successful self test, press the mode control until ANT is displayed and
input a predetermined frequency to select a station in the immediate area.
Adjust the volume control as necessary to provide a comfortable listening
level.
• Press the ID button and observe that the station identification code becomes
louder (if the station is voice-identified, it is not necessary to press the ID
button).
• Press the ID button again to cancel the IDENT function and press the mode
control until ADF is displayed.
• Observe the IND-650A Indicator and note that the bearing pointer
indicates the relative bearing to the station.
• Push the TEST button while observing the indicator bearing pointer. The
bearing pointer will rotate 90° and stop.
• Push the TEST button again (to turn off test function). The bearing
pointer returns to the original relative bearing position.
• Switch to BFO mode, if appropriate, and verify a tone is present. Select the
appropriate operating mode when all checks have been completed.
SECTION 5 - PERFORMANCE
No change.
SECTION 6 - WEIGHT AND BALANCE
Factory installed optional equipment is included in the licensed weight and
balance data in Section 6 of the Pilot’s Operating Handbook and Airplane Flight
Manual.
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