Correct answer is (b) Nsc < 5×10^6 [(27/γmft)/γmt]^3
The explanation: Fatigue effect for light and medium duty cranes need not be checked if normal and shear design stress ranges f ≤ (27/γmft) or if actual number of stress cycles, Nsc < 5×10^6 [(27/γmft)/γmt]^3, where f = actual fatigue stress range, γmft = partial safety factor for strength, γmf = partial safety factor for material = 1.10.