Use one part salt), and allowed to hang one week.

TAKEOFF WEIGHT ....... VARIABLE GROSS LANDING WEIGHT........ VARIABLE INERT WEIGHT (APPROX) ........ 74 844 kg (165 000 LB) MINIMUM GROUND CLEARANCES BODY FLAP Ex cen ELEVONS NOSE LANDING GEAR SUPPORT BEAMS MACHINED BULKHEAD (b) Structure. Figure 3-3.— Forward fuselage. 3-7.