Determine the length of the MAC, given:
Leading edge at wing root: STA 235
Trailing edge at wing root: STA 250
Leading edge at wing tip: STA 148
Trailing edge at wing tip: STA 212
Leading edge of MAC: STA 192
Trailing edge of MAC: STA 224
Note: Body stations are distances from the aircraft nose in 10-1 m.
- MAC = (224 – 192) = 32 m
Body stations are distances from the aircraft nose in 10-1 m
Therefore, MAC = 32 x 10-1 m = 320 cm
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