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The final report of the Spacecraft and Ground Support Equipment Configuration Panel (No. 1) was accepted by the Apollo 204 Review Board.
The panel had been assigned the task of documenting the physical configuration of the spacecraft and ground support equipment immediately before and during the January 27 fire, including equipment, switch position, and nonflight items in the cockpit. The panel was also to document differences from the expected launch configuration and configurations used in previous testing (such as altitude-chamber testing). During the investigation the panel had discovered a number of items which might have had relevance to flame propagation: - An engineering order, released at North American Aviation's Downey facility on January 20, provided direction to inspect the polyurethane foam in specified areas and coat the silicone rubber to meet flammability requirements. The direction was not recorded in the configuration verification record as of the start of the Space Vehicle Plugs-Out Integrated Test and was not accomplished on spacecraft 012. This item was considered as possibly significant in terms of fuel for the fire and a medium for flame propagation. The panel's summary of findings and determinations included: Finding Eighty engineering orders effective for spacecraft 012 had not been carried out at the time of the accident. Of these, twenty were specified to be completed after the test; four did not affect configuration. Determination Test requirements had no defined relationships with the open status of 56 engineering orders. The reason not all work items and engineering orders were closed was late receipt of changes or further work scheduled to be completed before launch. Finding Items not documented by quality inspection records had been placed on board the spacecraft during preparation for the Space Vehicle Plugs- Out Integrated Test. Determination Procedures for controlling entry of items into the spacecraft were not strictly enforced.
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