Originally Posted By: Brons2
surprised at the level of non-automation of the creation and assembly.
GE does it the same way, I've seen it first hand many times with just about every engine they build. I assume P+W does it the same.
The process is broken down into operations, which when complete, is signed of by each operator. Specific work instructions are provided for each operation, from which you are not allowed to deviate. After each operation, there is some type of inspection or verification that the operation is done correctly, which also must be signed off. Only the specified tooling and fasteners required for a specific operation are allowed to be in use, and must be accounted for prior to the next operation, FOD is not good. Tooling for example, torque wrenches are of course calibrated, traceable to each engine and operation. All traceable to NIST (National Institute for Standards and technology) among others. All records are kept for at least 20 years, with your name on it and the date you did it. Suppliers of each nut, hose, bearing, sensor, raw materials, everything must operate under this same quality system. Deviations from qualified hardware are under strict quality, and configuration management. This is one contributor to the high cost of aviation hardware, but the stakes are high. I've worked under this system for nearly 30 years and have participated in some crash hardware investigations that had my name all over the paperwork. In these cases the problem was elsewhere, but it still puts a big lump in your throat, but you then appreciate the quality system. In spite of this system, we have problems like those on the 787. I'll be intersted to read where things broke down.
Sorry about being long winded.