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It is good to know that the FAA Legal team has given the heavy aircraft a outlet to avoid useless SID's. Unfortunately in the FAA world this has not been applied to C337's, C402's, C414's, at this point in time. Is this by accident or neglect? Has Textron/Cessna attempted to clarify this to customers? I believe it's time to heavily publicize Textron/Cessna's ability to foresee fatigue failure of Cessna manufactured aircraft by Using "advanced systems and techniques" as described at length by Doug Oliver Textron/Cessna mouthpiece. What fool would by a Cessna product after examining Cessna's/FAA cozy relationship after this fiasco? I know one individual who was in the market for a nice new Citation. After explaining Cessna's style of doing business and their expertise with "advanced systems and techniques he has chosen a used G3. He looked into Cessna's SID formulation after i explained Cessna's actions. No way would he buy a Cessna. . Owners and Buyers become very attentive when the specter of wing/fuselage de-mateing is spoken. Especially when the trigger for this very expensive endeavor is "advanced system and techniques" along with a phantom plane with no investigatory history as the #1 reason for the very, very, very expensive maintenance or potential scrapping of a a expensive airframe prematurely.. Cessna 's Citation assembly line could loss a few sales very easily. I'm waiting for a Citation X SADASS ( Special Advanced Design Aeroknowledge Symptom Schedule) to be posted for a wing/fuselage removal and replacement. Of course predicated upon "Advanced Systems and Techniques", being used as the justification for the 8 million dollar MX.
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