1.
Nurhalizah S, As’adi M, Sari S. Assembly Line Balancing on NC212 Aircraft Fuselage Components Using RPW and RA Methods at PT XYZ (Case Study: Nose Fuselage Components). j. optim. syst. ergon. implementation [Internet]. 2025 May 26 [cited 2025 Dec. 6];2(02). Available from: https://ejournal.upnvj.ac.id/joseon/article/view/7463