environments with nominal atmospheric pressure variation fig1 shows the conduit and brush assembly 1020 having rotated approximately 90 degrees causing the piercing aperture 1022 to pierce the seal 1011 of the liquid adhesive reservoir 1010 and set up a path for the adhesive to flow to the bristles or filaments of the brush 1140 fig1 a shows the liquid adhesive reservoir 1010 and the conduit and brush assembly portion 1020 are stowed parallel to one another within a portion of an aircraft fuselage 1200 having fixed pedestal legs 1211 1212 and that the conduit and brush assembly portion 1020 may rotate to a position orthogonal and extending from the fuselage 1200 the conduit and brush assembly portion 1020 may rotate before or after the aircraft lands on a contact surface fig1 b shows an example of the brushes of the assembly in contact with the contact surface 1220 fig1 a shows another embodiment of the liquid adhesive storage and deployment assembly 1300 having a spring loaded conduit and brush assembly portion 1320 having a loaded spring 1321 that may be held in place by a pin 1322 and solenoid or servo actuated 1323 the brush assembly may be further bundled via a brush filament conduit such as a silicone conduit having a distal end for example a brush tip for some embodiments the brush filament conduit may be comprised of a wrapped kevlar tube fig1 b shows that with the pin 1322 retracted the conduit and brush assembly 1320 has been thrust into and has penetrated the liquid adhesive reservoir seal 1011 fig1 c shows the liquid adhesive reservoir and the conduit and brush assembly portion of the embodiment 1301 of fig1 b rotated to extend the brush portion.