Cal.load analysis and the weight and balance of this aircraft-as a result of-this change vas negligible and no changes to either report vere'made. ArialionailloitaAni AttaCted , • . 2 : • a t 41,— :an ts . SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00241193 EFTA01326786 F