JF17 Thrust to weight ratio is 1.08 not 0.93.
Lets find the facts..
JF17
Aircraft weight, empty (kg)--- 6,586 kg
Aircraft weight, full fuel (kg)--- 08,886 kg
Engine (rd 93) thrust maximum (N)-- 81,402 (wet), 49.7 kN / 51.2 kN (DRY) (For WS 13 this would be 86.3 kn (wet) and 56.7 (dry) but reduced engine life.)
Aircraft weight, max take-off load (kg)-- 12,700
Total fuel weight (kg)- 2,300
T/W ratio (full fuel)--0.93
Now LCA
Aircraft weight, empty (kg)--- 6,560 kg
Aircraft weight, full fuel (kg)--- 9,080 kg
Engine (GE 404) thrust maximum (N)-- 84,000 (wet), 53.9 kN (DRY) (Govt. website says thrust is 889645 N or 20000 lbf)
Aircraft weight, max take-off load (kg)-- 13,300
Total fuel weight (kg)-2,458
T/W ratio (full fuel)--0.94..
The source you are quoting is Wikipedia and its reference is a YouTube video.. My source is government website..
Specifications | Tejas - India's Light Combat Aircraft
You can find that Max load of Tejas is 13300, about 600 kg more than JF 17 which has more internal fuel and wepons since emty weight is less than JF 17.. But then max engine power is 2500 N more than JF 17.. You need not be a rocket scientist to deduce facts from above specs...