Workshop Manuals Factory service & repair Land Rover
01 Engine - Td402 Engine - K Series 1.803 Engine - K Series KV604 Emission control - Td405 Emission control - K Series 1.806 Emission control - K Series KV607 Engine management system - EDC08 Engine management system - MEMS09 Engine management system - siemens (all except NAS)10 Engine management system11 Fuel delivery system - Td412 Fuel delivery system - K Series 1.813 Fuel delivery system - K Series KV614 Cooling system - Td415 Cooling system - K Series 1.816 Cooling system - K Series KV617 Manifold and exhaust system - Td418 Manifold and exhaust system - K Series 1.819 Manifold and exhaust system - K Series KV620 Clutch21 Manual gearbox - Getrag22 Intermediate reduction drive23 Automatic gearbox - Jatco24 Driveshafts25 Rear axle and final drive26 Steering27 Front suspension28 Rear suspension29 Brakes30 Restraint systems31 Heating and ventilation32 Air conditioning33 Wipers and washers34 Control units35 Communication data buses36 Security37 Windows38 Navigation system39 Instruments
Land Rover Freelander System Description and Operation (UK)30 · Restraint systems
30 · Body & interior

Restraint systems (Operation): Description and operation

Make
Land Rover
Model
Freelander System Description and Operation (UK)
Section
Description and operation › Operation
Restraint systemsOperation

Operation

General

When the ignition is switched on, the airbag DCU performs a bulb check of the SRS warning lamp as part of the power up procedure. The lamp should be extinguished after approximately 5 seconds, indicating that the system is fully operational. If the lamp remains illuminated, a fault has been detected and repair action is required.

While the ignition is on, data from the single point sensor is continuously monitored by the airbag DCU. If the data from the single point sensor indicates vehicle deceleration is at or above the preset limit, and the mechanical safing sensor is closed, the DCU interprets this as a collision that requires deployment of the airbags and retraction of the seat belt pretensioners. It then activates transistors to send fire signals to the airbag modules and the seat belt pretensioners. On pre 2002 MY vehicles, the airbag DCU simultaneously records in memory the following information: l The error code of the last permanent fault (if any) detected before the collision. l Internal program information about the collision as seen by the airbag DCU. l The diagnostic status of the airbag and seat belt pretensioner circuits before deployment. l The voltage of each power backup capacitor before deployment. l Information on the airbag DCU internal program status.

NOTE: If external power is lost during the collision, recording of the last three above items only occurs if there is sufficient power in the backup capacitors after outputting the fire signals.

After deployment, the airbag DCU enters a crash locked mode and illuminates the SRS warning lamp. In the crash locked mode the airbag DCU is permanently disabled and must be replaced during subsequent repair action. Crash locked mode cannot be cleared using TestBook/T4.

Diagnostics

While the ignition is on the diagnostic function of the airbag DCU monitors the SRS for faults. If a fault is detected, the airbag DCU stores a related fault code in memory and switches the earth output to illuminate the SRS warning lamp. With a supply voltage range fault, the warning lamp is illuminated only for the duration of the fault. With all other faults, including intermittent faults, the warning lamp is illuminated for the remainder of the drive cycle. At the next ignition on, if the fault is still present the warning lamp remains illuminated after the lamp check; if the fault does not recur, the warning lamp extinguishes but the fault code remains stored in memory. On pre 2002 MY vehicles, an intermittent fault will be cleared from memory if 40 drive cycles are completed without its recurrence.

After detecting a fault, the system may retain some operational capability. If a fault is detected in an airbag or pretensioner circuit, the circuit may be disabled, depending on the fault; the other airbag and pretensioner circuits remain operational and their related components will still be deployed in a collision. If an internal or power supply fault is detected, the complete system will be disabled. If a fault exists in the SRS warning lamp circuit, the lamp will not illuminate during the lamp check at ignition on, but, provided there are no other faults, the system will otherwise be fully operational.

Fault code retrieval and fault diagnosis of the SRS can only be done using TestBook/T4. Additional SRS information that can be read using TestBook/T4 is the: l Airbag DCU bar code. l Evolution number of the hardware and software, and the algorithm level. l Status of the crash locked mode. l Vehicle Identification Number (VIN) data.

Diagnostic checks performed by the airbag DCU include: l Monitoring of the airbag and pretensioner circuits for open/short circuits. l Internal errors. l Supply voltage (limits are: 8.6 to 19.0 V at power up, 6.0 to 19.0 V during drive cycle up to 2002 MY; 10.0 to 16.5 during normal operation from 2002 MY onwards).

Parts & tools for this job For Land Rover Freelander

Links open Amazon search results in a new tab. As an Amazon Associate I earn from qualifying purchases.