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[i]A docking test between the CSM and AM [Airlock Module]/MDA will be performed to verify the docking interfaces. The CSM is placed in the West Integrated Test Stand. The AM/MDA is removed from its mobile transporter and lowered, MDA down, to mate with the CSM. The CSM has a probe identical to that used in Apollo and the MDA docking port has a drogue similar to that used in the Apollo LM for docking. A leak check is performed to verify the mechanical docking interface. Electrical/communications tests are accomplished to validate all electrical connections. These tests are the only interface tests involving the flight CSM and the AM/MDA prior to launch. The next time these modules interface is following rendezvous maneuvers in earth orbit as earlier described.[/i]
[i]A requirement exists to electrically check out the DM [docking module] at the Salyut interface and the CSM at the CSM/DM interface. The checkouts will be accomplished ... utilizing ... the C54-035 at LC-39.[/i]
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