SAFEDOCK®
Safegate Group
Manual
Date: 6 February 2015
Chapter: 3A Operating Procedures
Version: 2.7
Page 19 of 30
2.5
FAILED AIRCRAFT VERIFICATION (ID FAIL)
Description
Position
After capture of the aircraft, its geometry is checked against a stored
profile. If, for any reason, aircraft verification is not confirmed 15m
before the stop-position, the Pilot Display will show
STOP
followed by
ID
FAIL
.
Below there is a list of errors that can be displayed on the Operator
Panel and a short description:
Geometry failed
- Geometry check failed within ID Fail limit
Nose height failed
- Nose height check failed
Engine verification
- Engine verification failed
Profile failed
- Profile check failed
Lost track
- Lost track close to stop
Note
: (option) Dockings can be resumed without verification; however it
is important to follow the information below. Alternatively, the aircraft
shall be marshalled-in or towed-in to the gate.
WARNING! THE PILOT MUST NOT PROCEED
BEYOND THE BRIDGE WITHOUT MANUAL
GUIDANCE, UNLESS THE WAIT MESSAGE HAS
BEEN SUPERSEDED BY THE CLOSING RATE BAR.
Note
: This may be a system event or a fault (to analyse the possible
cause of the incident, see § 2.5.2 Event or Fault Diagnosis in this
Chapter).
Gate area: Empty
(aircraft is on the ground en
route to gate).
Image
Operator Panel
Image Pilot Display
T1-42
T2-18
T2S-24
T3-9
T3-15
2.5.1
Override ID FAIL
The override function is designed to resolve an aircraft verification problem during an
active docking procedure.
WARNING! THE OVERRIDE FUNCTION GIVES THE OPERATOR
RESPONSIBILITY FOR AIRCRAFT VERIFICATION, AS A TEMPORARY
SOLUTION TO AN EVENT/FAULT RECOGNISED BY THE SYSTEM.
When using the override function, these instructions must be followed:
Make sure the stand area is clear of any obstructions such as vehicles, apron or
other objects which may obstruct the aircraft, including wings or engines.
Check for the correct stop-position (ground markings).
<Aircraft type> <Flight>
ID FAIL
Shut
down
Over
ride
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