What's the legal eagle speak for accepting these? I've come to believe that any component that has either of these is perfectly acceptable (along with an S tag) to be fitted to a UK registered aircraft.
A colleague of mine believes that the FAA form is not acceptable and there needs to be a Form 1 before fitment can take place.
Is there anywhere it's laid down outside company procedures which is acceptable and which is not? (ie CAA or EASA regs).
Also, where is the critieria for raising Form 1's to be found. I've scoured the EASA site but no joy as it hasn't improved much and is still a nightmare to navigate.
Fargoo
