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┃      A~7-~'M" A321             ┃FLIGHT GUIDANCE ┃SEQ 001 ┃REV 35  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━┻━━━━┛
Engagement conditions of LOC and G/S modes
When ILS capture conditions are fulfilled :
- LOC* mode engages, and
- G/S* mode engages. No radio altimeter validity is required with this FMGC standard for
   G/S engagement. The FMA displays "LOC*", or "G/S*", or both, in green.
Nevertheless, the G/S* mode cannot engage, if :
- LOC* mode is not engaged, or
- The aircraft is above the glide path and its trajectory does not cross the ILS G/S beam.
When the aircraft is established on the LOC axis, the LOC mode engages.
When the aircraft is established on the G/S axis, the G/S mode engages.
The FMA displays "LOC" and "G/S" in green. The AP/FD guides the aircraft along the G/S
down to 30 feet, and along the LOC during the flare and rollout.
Disengagement conditions of LOC and G/S modes
If the aircraft is above 400 feet, the (ILS) APPR mode disengages when the pilot :
- Presses the APPR pushbutton, HDG V/S or TRK FPA engages.
- Presses the LOC pushbutton, the LOC mode remains engaged. The system reverts to V/S
   (FPA), if G/S was engaged.
- Pulls out the V/S FPA selector knob, the system reverts to basic modes (HDG V/S or TRK
   FPA engages).
- Pulls out the HDG/-rRK selector knob, HDG V/S or TRK FPA engages.
- Engages the go-around mode.
CCM ALL
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┃                                ┃                            ┃1.22.30     P 52      ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃l          AFLIGHTIGUIDANCE ┃SEQ 001 1 ┃I REV 35  ┃
┃ aw aw ,, ~e~ A319              ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
Note: G/S* or G/S modes may be engaged above the operating range of the radio
       altimeters (8000 feet for TRT, and 5000 feet for Collins and Honeywell RA). The
       landing capability displayed on the FMA will reflect the lack of RA validity (CAT I)
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual2(62)