APPENDICES
4 OPC and AMI FILES
4.2. AMI FILE
Description Range Unit Default
SW_OPTIONS
CO RTE retention
Y : Manual deletion only, N : Deleted automatically
after landing
Y / N
(Y=manual
deletion)
Y
Default Speed limit (250 kts/10000') Enforced Y/N Y
DIR TO page default selection
Y/N
(N=without abeam)
N
Default Intercept Angle for OFFSET path 20° / 50° deg 30
POLICY_OPTIONS
Airline Ident - A/C type - Engine type
Thrust Reduction Height 400 / 5000 ft AGL 1500
All Engines Acceleration Height 400 / 10000 ft AGL 1500
Engine Out Acceleration Height 400 / 10000 ft AGL 1500
Performance Factor -9,9 / +9,9 % 0
Idle Factor -9,9 / +9,9 % 0
Performance Adjustement Code 3 characters ARM
Fuel for taxi 0 / 2000 kg 200
Percentage of trip fuel for route reserves 0 / 15 % 5
Upper limit for route reserves quantity 0 / 10000 kg 10000
Lower limit for route reserves quantity 0 / 10000 kg 0
Compute route reserve during flight Y / N Y
Alternate trip included in route reserve Y / N N
Time in which final holding pattern supposed to be
flown (Used for fuel prediction)
0 / 90 mn 30
Time final holding pattern supposed to be flown
Used for fuel planing
0 / 90 mn 30
Fuel burned for the final holding pattern.
Used for fuel prediction
0 / 10000 kg 0
Altitude at which the final holding pattern is
supposed to be flown
1500, 5000, 10000,
15000, 20000
ft AGL 1500
Final holding pattern is flown at primary or alternate
destination
P / A A
J43126AA 00
© THALES AVIONICS S.A.
AIRBUS A318/319/320/321
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