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NOTE
Use of the TAS self-test function in flight will inhibit TAS operation for up to eight
seconds.
PERFORMANCE
No change.
S7-6 S7-AB 510FM-S7-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 7
FAA APPROVED
Configuration U.S.
HONEYWELL KTA 870 TRAFFIC ADVISORY SYSTEM
(TAS)
INTRODUCTION
This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for airplanes equipped with the Honeywell KTA 870 Traffic Advisory System (TAS). The information
contained herein supplements the information of the basic FAA Approved Airplane Flight Manual.
For limitations, procedures, and performance information not contained in the supplement, consult
the basic FAA Approved Airplane Flight Manual.
OPERATING LIMITATIONS
Evasive traffic avoidance maneuvers must not be based solely on the traffic display or a Traffic
Advisory from the KTA 870 TAS. These displays and advisories are intended to assist the flight crew
in visually locating traffic.
OPERATING PROCEDURES
The operating procedures are the same as those in the basic FAA Approved Airplane Flight Manual
except as follows:
EMERGENCY PROCEDURES
No change.
ABNORMAL PROCEDURES
ALT MISCOMP (ALTITUDE MISCOMPARE)
O IF ABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE
5. Use SENSOR REVERSION to select most accurate ADC on both PFD’s.
6. If ADC1 is determined to be the most accurate altitude source, select TAS to
STANDBY.
7. Land as soon as practical.
Procedure Completed
PIT / ROL / HDG MISCOMP (PITCH / ROLL / HEADING
MISCOMPARE)
• HEADING MISCOMP
8. AIR SOURCE SELECT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
NOTE
• The magnetic compass is influenced by windshield heat, the cockpit fan, and
fresh air fan. These items must be turned OFF prior to referencing magnetic
compass heading then may be reselected ON. The items must then be reselected
OFF prior to each referencing of the magnetic compass.
• TAS traffic bearings will be inaccurate with a heading miscompare.
Procedure Completed
510FM-S7-01 S7-AC S7-5.1
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 7
FAA APPROVED
U.S. Configuration
NORMAL PROCEDURES
BEFORE TAXI
1. Pilot Initiated Self-Test . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
a. Traffic Advisory (Yellow Circle) . .9 o’clock, range 2 miles, 200 feet below and climbing
b. Proximity Traffic (Solid White Diamond). . .1 o’clock, range 3.6 miles, 1000 feet below
and descending
c. Non-Threat Traffic (Open White Diamond)11 o’clock, range 3.6 miles, 1000 feet above
d. Voice Annunciation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . “TAS SYSTEM TEST OK”
2. TAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPERATE (Recommended range 10 nm)
AFTER TAKEOFF
CLIMB
1. Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Recommend 10 nm or greater)
2. ALT MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .(Recommend ABOVE)
CRUISE
1. Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Recommend 10 nm or greater)
2. ALT MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Recommend NORMAL)
DESCENT
1. Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Recommend 10 nm or less in terminal area)
2. ALT MODE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Recommend BELOW)
NOTE
Use of the TAS self-test function in flight will inhibit TAS operation for up to eight
seconds.
PERFORMANCE
No change.
S7-6.1 S7-AC 510FM-S7-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 7
FAA APPROVED
Configuration U.S.
DESCRIPTION
The Honeywell KTA 870 Traffic Advisory System (TAS) is an airborne system used for detecting and
tracking aircraft near your own airplane. The KTA 870 processor and antennae detect and track
other aircraft by interrogating their transponders. Aircraft tracked and displayed by the KTA 870 TAS
are referred to as intruders.
NOTE
• The KTA 870 is unable to detect an intruding aircraft if the intruder is not equipped
with an operating transponder. TAS can detect and track aircraft with either Mode
A, Mode C, or Mode S transponders.
• Due to aircraft geometry, the relative bearing to a Mode A (Non-Altitude
Reporting) aircraft may appear erratic when the intruding aircraft is at close
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