It means that there is probably some structural integrity. If it had crashed and completely broken up they would not try to re-establish contact.
Let's think logically
comms stopped while the lander was still descending
Due to inappropriate functioning of the thrusters the lander was most probably subjected to high G forces and related stress and strain while still in flight when the comms snapped.
this means some components inside lander were subjected to higher than rated g forces.
So as i previously alluded lander must have landed , but there was comms failure due to possible malfunction of some comms equipment . Higher that expected G forces might have induced anomalous behaviour in the comms component like displaced linkages or unintended transient voltage transfer / voltage spike causing shut down. unfortunately I have no understanding of the working of the same in space systems. So not 100% sure.but Similar power failures happened with isro satellites power bus.
The onboard TX/RX system requires the onboard data processing package to process data and format it for transmission over the same and vice versa after receiving the data. TX/RX system is working but the backend system which processes the data to be sent or be received seems not to be working at the moment.
Communication link is open but no data is being sent or received at the landers end atleast for now.
The power supply from battery if bypassed for the secondary power source the solar panels , then there exists a possibility that the anomalous condition with the effected components of the comms system might get resolved and the system might reboot.
Eg in a normal oscilloscope if it is subjected to out of range voltage beyond instrumented range , the output readings flatlines and shuts down to recover and then reboots if the surge voltage is no longer present.
So same recovery can happen with the landers malfunctioning components provided the anomalous cause ceases to exist .