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<strong>AC</strong> <strong>25</strong>.<strong>807</strong>-1 8/13/90<br />

Appendix 1<br />

(a) The length of the cabin is 880 inches (FS 970 - FS 90).<br />

(b)<br />

The number of exit units in each zone is as follows: <br />

Zone A: 1.<strong>25</strong>; <br />

Zone B: 2.<strong>25</strong> (1.<strong>25</strong> + 1.0);<br />

Zone C: 2.<strong>25</strong> (1.0 + 1.<strong>25</strong>); <br />

Zone D: 1. <strong>25</strong>; <br />

Airplane total: 7.0. <br />

(c) Fuselage length factor= 1<strong>25</strong>.8 inches (880"/7.0).<br />

(d)<br />

{e)<br />

(f)<br />

(g)<br />

Nominal exit location: <br />

Exit 1: FS 277.2 (120 + (1<strong>25</strong>.8 x 1.<strong>25</strong>)); <br />

Exit 2: FS 565.2 {277.2 + (1<strong>25</strong>.8 x 2.<strong>25</strong>));<br />

Exit 3: FS 843.3 (565.2 + {1<strong>25</strong>.8 x 2.<strong>25</strong>)). <br />

Exit offsets, proposed versus nominal: <br />

Exit 1: Offset= 57.2" (277.2 - 220); <br />

Exit 2: Offset - 60.2" (560.2 - 500);<br />

Exit 3: Offset= 6.7" {850 - 843.3). <br />

Percent of exit offset:<br />

Exit 1: 6.5% (57.2/880 X 100%);<br />

Exit 2: 6.8% (60.2/880 x 100%);<br />

Exit 3: 0.8% (6.7/880 x 100%);<br />

All exits are offset less than 15 percent from the nominal<br />

locations and are acceptable.<br />

By inspection, no two exits are closer together than the fuselage<br />

length factor of 121.4 inches.<br />

8<br />

,:, u.s.o.P.o., 1990. 717-ooo/27178

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