ad8261p2000a

Auto pilot system (APS) diagnosis, advanced information

Type ad · topic 82.61 · version 0100 · 2003-06-13

Applies to: MODEL 140 as of 1.12.96 up to 31.12.97, 210.0 as of 1.6.96 up to 31.12.97 with CODE (351) auto pilot system (APS)

Where it sits

Function group 3 Body › 82 Electrical system, body › 82.61 Auto Pilot System (APS), Audio 30 APS — Series 140 · Series 210 (models 0**)

AD82.61-P-2000A

Auto pilot system (APS) diagnosis, advanced information

20.8.97

MODEL 140 as of 1.12.96 up to 31.12.97,
210.0 as of 1.6.96 up to 31.12.97 with CODE (351) auto pilot system (APS)

Connection and use of test equipment

AD00.00-P-1000AZ

Auto pilot system (APS), location of components

Model 140

GF82.61-P-0001-01D

Model 210.0

GF82.61-P-0001-01B

Location and assignment of connectors and plug connections

Model 140: Group 00

Model 210

GF00.19-P-1000A

Summary of electric wiring diagrams

Model 140: Group 82

Model 210

PE82.00-P-1100A

Diagnostic tools, auto pilot system (APS)

AD82.61-P-2000-01A

Coupling assignment, navigation processor (APS)

AD82.61-P-2000-02A

Coupling assignment, radio with navigation operating unit

AD82.60-P-2000-07A

Fuses in order

Battery voltage 11-14 V

To prevent damage to the control modules, couplings should only be disconnected or connected with "terminal 15R: OFF".

Auto pilot system (APS), notes on operating and calibrating

The complete operation of the APS system can be found in the Owner's Manual.

GF82.61-P-0001-03B

Notes on testing on the APS test program

After the navigation processor (APS) (A2/30) is replaced, the system is to be commissioned using the APS test program.

AD82.61-P-2000-03A

Auto pilot system (APS), fault messages on the APS test program

If faults occur during calibration:

AD82.61-P-4001A

With wheel and tire combinations which differ from production, the auto pilot system (APS) must be adapted to the revised values (track width and rolling circumference). The calibration is carried out in the test program of the radio and navigation operating unit (APS) (A2/29)

The radio code must also be entered after the voltage supply to the navigation processor (APS) (A2/30) is interrupted (increased anti-theft measure).

Interference with radio or satellite reception may occur due to local and atmospheric influences.

Satellite reception is only possible in the open air.

The location is determined using the Global Positioning System data (degrees of longitude and latitude) between 2 and 30 minutes after "ignition ON".

Referenced documents