Garmin GNS 530 파일럿 매뉴얼 부록 - 페이지 10

{카테고리_이름} Garmin GNS 530에 대한 파일럿 매뉴얼 부록을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530 22 페이지. Supplement a21 to the airplane flight manual da 40 diamond com/nav/gps
Garmin GNS 530에 대해서도 마찬가지입니다: 파일럿 매뉴얼 (22 페이지), 사용 설명서 (6 페이지), 파일럿 매뉴얼 부록 (27 페이지), 파일럿 매뉴얼 부록 (4 페이지), 빠른 참조 (16 페이지), 브로셔 (1 페이지), 빠른 참조 (23 페이지), 설치 매뉴얼 (14 페이지), 매뉴얼 (35 페이지)

GTS 8XX Interface

1.4

AURAl AleRTS

A TA consists of a displayed traffic symbol (solid yellow circle) and an aural alert.

The aural alert announces "traffic", followed by the intruder aircraft' s position, altitude

relative to own aircraft ("high", "low", or "same altitude"), and distance from own

aircraft; e.g. "traffic, 12 o'clock, high, 3 miles".

1.5

The GTS 8XX automatically performs a self-test upon power up. The self-test

checks internal parameters and calibrates components of the GTS 8XX. The self-test

can also be initiated by the user during normal operation.

Check for the following test criteria on the Traffic Page during power-up:

• If the GTS 8XX passes the power-up test; and the aircraft both has a squat

switch and is on the ground, the Standby Screen is displayed (Figure 2).

• If the GTS 8XX passes the power-up test and the aircraft both has a squat

switch and is airborne, the Traffic Page is displayed on the 6-nm display range

and in the normal altitude display mode.

• If the GTS 8XX passes the power-up test and the aircraft does not have a squat

switch, the Standby Screen is displayed (Figure 2).

• If the GTS 8XX fails the power-up test (as indicated by a FAILED screen),

the GTS 8XX is inoperable, see the GTS 8XX Installation Manual for detailed

information on Failure Response.

NOTE: The FAILED message is displayed when the system detects an error

that prohibits further traffic display operation.

NOTE: When the system is in standby, the GTS 8XX does not transmit,

interrogate, or track intruder aircraft.

400/500 Pilot's Guide Addendum for GTS 8XX Interface

190-00140-78 Rev. A