Classic "Missing Rivet" Airworthiness Scenario

Posted by squawk1018@reddit | flying | View on Reddit | 30 comments

I was always under the impression that an aircraft was airworthy strictly based on the definition in 14 CFR 3.5(a): "the aircraft conforms to its type design and is in condition for safe operation," plus compliance with applicable inspections/maintenance under parts 91 and 43. Thus, a "missing screw" would disqualify an aircraft from "conforming to its type design," rendering it unairworthy.

However, this belief changed when I stumbled upon the Witkowski LOI. Apparently, the FAA acknowledges an aircraft that has “accumulated a certain amount of wear and minor defects," and asserts that an "airplane that has been in service a number of years clearly is not in exactly the same condition as when it left the factory. Nevertheless, if the airplane has been properly inspected and maintained in accordance with 14 CFR parts 91 and 43, it should substantially conform to its type certificate to the extent that it will provide a level of safety that conformity with its type certificate is intended to ensure. The determination of when a mechanical, electrical, or structural discrepancy is sufficiently serious to render an aircraft unairworthy is, in many cases, a judgment call."

So, a missing screw is a pilot's judgment call? I am preparing for my CFI checkride, and if this scenario is presented, do I state this?

In this case, I would state the above information while also stating that I would consult an A&P mechanic to determine airworthiness. Is this an appropriate answer? Also, how would a mechanic make this call?