R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 57 1 1 Config-1 May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| | | |||| | |||| | | | | |||| | |||| |___ 8E.2.126.00 RH Pack Flow | | | | |||| | |||| 0 to .99 kg/sec.| | | | |||| | ||||_____ 29.1.001.00.18 RH Wing AI/V Pos| | | | |||| | ||| 29.2.001.00.18 Closed = 0 | | | | |||| | |||______ 5D.2.061.10.27 Eng.2 Nascelle | | | | |||| | || AI Pos. Open = 1| | | | |||| | ||_______ 6F.1.066.01.17 Eng.2 PRV Pos. | | | | |||| | | 6F.2.066.10.17 Fully Closed = 0| | | | |||| | |________ 6F.1.066.01.15 Eng.2 HPV Pos. | | | | |||| | 6F.2.066.10.15 Fully Closed = 0| | | | |||| |__________ 29.1.055.01.16 Cross Feed Valve| | | | |||| 29.2.055.01.16 Pos Fully Clo.=0| | | | ||||____________ 6F.1.067.01.15 Eng.1 HPV Pos. | | | | ||| 6F.2.067.10.15 Fully Close = 0 | | | | |||_____________ 6F.1.067.01.17 Eng.1 PRV Pos. | | | | || 6F.2.067.10.17 Fully Closed = 0| | | | ||______________ 5D.2.061.10.28 Eng.1 Nacelle AI| | | | | Pos. Open = 1 | | | | |_______________ 29.1.001.11.18 LH Wing AI/V Pos| | | | 29.2.001.11.18 Closed = 0 | | | |_________________ 8E.1.126.11 LH Pack Flow | | | 0 to .99 kg/sec.| |--------------|------------------------------------------------------| | APU | APU Bleed Valve State | | 1 | Bit Status 1 = APU Bleed Valve open | | | param. 7A.1.037.01.11 | |--------------|------------------------------------------------------| | TAT | Total Air Temperature | | X999 | Negative values are indicated by 'N' on the first | | | position (-60.0 to 99.9 C). | | | param. 06.1.211.01 | | | 06.2.211.10 | |--------------|------------------------------------------------------| | ALT | Standard Altitude | | X9999 | Negative values are indicated by 'N' on the first | | | position (-2000 to 50000 ft). | | | param. 06.1.203.01 | | | 06.2.203.10 | |--------------|------------------------------------------------------| | CAS | Computed Air Speed | | 999 | (20 to 450 kts) | | | param. 06.1.206.01 | | | 06.2.206.10 |
R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 58 1 1 Config-1 May 01/05 1 1 1CES 1 +---------------------------------------------------------------------+ | Value | Content Description | |--------------|------------------------------------------------------| |--------------|------------------------------------------------------| | MN | Mach Number | | 999 | (0.100 to 0.999) | | | param. 06.1.205.01 | | | 06.2.205.10 | |--------------|------------------------------------------------------| | GW | Gross Weight | | 9999 | (0 to 9000 * 10 kg) | | | param. 02.1.075.00 | | | 02.2.075.00 | |--------------|------------------------------------------------------| | CG | Center of Gravity | | 999 | (0 to 50.0% MAC) | | | param. 02.1.077.00 | | | 02.2.077.00 | |--------------|------------------------------------------------------| | DMU/SW | DMU Software Partnumber | | XXXXXX | X = Engine Type C = CFMI, I = IAE | | | X = Engine Version 1 ...8 | | | X = Hardware Vers. A100 or A200 | | | X | | | X = Database Vers. XX10-XXXX or XX20-XXXX | | | X | +---------------------------------------------------------------------+
K. DMU Programming Two different types of software packages are given. The DMU operational software and the DMU database software. These two software types have to be load into the DMU to give the complete functions. Only the DMU database software are subject of customer reprogramming. In addition a subset of the configuration data provided by the DMU database are reconfigurable on board the aircraft, via the MCDU.
(1) Operational Software Programming Reprogramming of the operational software is only necessary, if a new modified software version is required or due to recognized software faults or future sytem modifications. Configuring the DMU for the specific requirements and applications of a customer shall require only reprogramming of the database by the use of the GSE reconfiguration function. Modification of the microprocessor code of the DMU operationalsoftware is reserved to the DMU vendor.
R 1EFF : 001-049, 051-099, 101-105, 1 31-36-00Page 59 1 1 Config-1 May 01/05 1 1 1CES 1
(2)
Database Programming The DMU database is reprogrammable by the use of the GSE reconfiguration software. An initial DMU database software is provided by the DMU vendor. This initial database is provide the configuration data required for the AI defined standard reports. A lockout mechanism is provided for the GSE reconfiguration software, which prevents the AI reserved functions and constants from being modified by the customer. A subset of the configuration data of the AI standard DMU database is reprogrammable by the customer via the GSE. Furthermore the customer have the possibility to define additional trigger conditions, reports and global variables. Also the parameters recorded on the DAR or SAR are determined by the GSE programming.
