In case the certification basis is CS-25 Amdt 5 (or later) according to part 21A.101 (i.e. STC is a significant change related to EWIS aspects or new product), will the EWIS ICA discriminant (>30 pax or >7,500 lb) still apply?
Would EASA recommend to STC applicants to elect to comply with CS-25 Amdt 5 (or later) on a voluntary basis?
Are all the EWIS ICA from the TC holders’ affected aeroplanes available by now (status July 2010)?
Does a STC with an "EWIS limitation" still present affect the entry into service of an A/C it is fitted to?
When is the Special Condition SC H-01 “Enhanced Airworthiness Programme for Aeroplane Systems - ICA on EWIS” applicable to the Non-EU STCs to be validated by EASA?
What is the Special Condition H-01 “Enhanced Airworthiness Programme for Aeroplane Systems - ICA on EWIS”?
On which basis / requirement the Agency has requested TC holders to develop EWIS ICA?
On which basis / requirement the Agency is requesting a STC Applicant to evaluate if a revision to EWIS ICA is necessary?
Are these requirements applicable to any major design change or only to significant or substantial change where the latest requirements must be considered (according to Part 21A.101)?
The letter dated 07.01.2009 (the letter sent by DOA Section) specifies certain aircraft class in the footer. Where can we find this specified in a current regulation?
Some aeroplane types are explicitly excluded from the similar FAA rule (FAR 26.11(g)). Are these types also excluded from EASA requirements?
How can we as DOA identify if an aircraft model is applicable or otherwise has been made compliant (by means of a retroactive requirement) to this rule? Will it be entered into the TCDS or will there be an AD requiring that or does each individual DOA has to find its own way through it by going through the ICA documentation?
How will the EWIS/EZAP assessment affect minor modifications and repairs for TCs/STCs and if the requirements are found to be applicable would this affect their classification (e.g. minor becomes major)?
We anticipate that a CRI may be needed for each STC because of the need to at least have the applicants use the checklist. Has EASA considered the effect on the hours to be allocated for each task to include the extra work? In addition may this not also affect the classification of an STC from Simple to Standard because of the need to include an electrical specialist each time?
To avoid the extra workload would it not be an idea to have EU DOAs include consideration of the ICA requirements as part of their procedures? This would make EWIS part of their normal practises?
Will we need to amend the TC basis for each type to include this CS-25 requirement and publish in amended TCDSs?
The 07/06/10 deadline date for STC applicants - how will this be managed by EASA if the STC has already been issued. Will a new project be needed to allow the teams to review the ICAs?
Once a STC holder has applied for a Major Change to the STC to remove the limitation stating that the STC holder shall provide the final EWIS ICA for the STC by 7th of June 2010, what is the expected timeframe for the EASA acceptance?
If there are two or more modifications being embodied at the same time - e.g. cargo conversion - how will EASA ensure that each applicant checks the effect of their design change on the aircraft and on each others modification's?
Can an applicant use FAA’s AC 25-27A, notably Appendix B for the handling of design changes?
For STC to be certified after the 7th of June 2010, what are the dates EASA would require EWIS ICA to be available?
What documents need to be transmitted by the STC applicant to EASA for the aspect of EZAP/EWIS ICA?
Which are the CS-25 affected aircrafts for which the Special Condition SC H-01 "Enhanced Airworthiness Programme for Aeroplane Systems – ICA on EWIS" is applicable?
What is the official letter sent by EASA regulating the European EWIS Rules for the STC Holders?