The following minimum information should be provided in the AFM:
- (a) the approved limits established as a result of consideration of any other factor that the certification has shown to be appropriate; - (b) the normal and abnormal procedures, including airspeeds; - (c) the minimum required equipment; - (d) any additional aeroplane performance limitations; - (e) if appropriate, the type of approaches and the xLS navigation means (facilities external to the aircraft) and associated limitations (if any) which have been used as the basis for certification; - (f) any related limitations and/or assumptions on the runway or aerodrome conditions that are affected by the use of the EFVS; for EFVS-L, this should also consider: - (1) runway elevation, - (2) approach path slope, - (3) touchdown zone slope, - (4) ground profile under the approach path; - (g) the type and mode of operation/configuration of the approach lights (i.e. LED or incandescent) that have been used or assumed during the certification demonstration of the EFVS; - (h) the demonstrated performance in accordance with CS AWO.A.EFVS.109; - (i) wind speed limitations that are affected by the use of the EFVS; - (j) any applicable assumptions that have been made during the certification demonstration of the EFVS.
[Issue: CS-AWO/2]
Appendix 1 to the AMC to Section 3 of Subpart A
EFVS compliance
The following is a non-exhaustive list of certification specification in CS-25 that could be affected by an EFVS installation.
Applicants for normal-category aeroplanes (CS-23) can use the list below to establish whether the equivalent aspects in CS-23 are affected and address them accordingly.
Note: As of Amendment 5 to CS-23, the referenced CS-23 requirement numbers are reflected in the AMC to CS-23.
| Certification specification | Description |
|---|
| 25.251 | Vibration and buffeting |
| 25.301 | Loads |
| 25.303 | Factor of safety |
ED Decision 2022/007/R
ED Decision 2022/007/R
Easy Access Rules for All-Weather Operations (CS-AWO)
| Certification specification | Description |
|---|
| 25.307 | Proof of structure |
| 25.561 / 25.562(c)(5) | Emergency landing conditions; head injury criterion (HIC) |
| 25.571 | Damage-tolerance and fatigue evaluation of structure |
| 25.581 | Lightning protection |
| 25.601 | Design and construction - General |
| 25.603 | Materials |
| 25.605 | Fabrication methods |
| 25.609 | Protection of structure |
| 25.611 | Accessibility provisions |
| 25.613 | Material strength properties and material design values |
| 25.619 | Special factors |
| 25.625 | Fitting factors |
| 25.629(d)(8) | Aeroelastic stability |
| 25.631 | Bird strike damage |
| 25.771 | Pilot compartment |
| 25.773 | Pilot compartment view |
| 25.777 | Cockpit controls |
| 25.1301 | Function and installation |
| 25.1309 | Equipment, systems, and installations |
| 25.1316 | Electrical and electronic system lightning protection |
| 23.1308 and 25.1317 | High-intensity radiated fields (HIRF) protection |
| 25.1321 | Arrangement and visibility |
| 25.1322 | Flight crew alerting |
| 25.1323 | Airspeed indicating systems |
| 25.1329 | Flight guidance system |
| 25.1353 | Electrical equipment and installations |
| 25.1357 | Circuit protective devices |
| 25.1381 | Instrument lights |
| 25.1419 | Ice protection |
| 25.1431(a)(c) | Electronic equipment |
| 25.1459(e) | Flight data recorders |
| Certification specification | Description |
|---|
| 25.1501 | Operating limitations and information - General |
| 25.1523 | Minimum flight crew |
| 25.1525 | Kinds of operation |
| 25.1529 | Instructions for Continued Airworthiness |
| 25.1581 | Aeroplane flight manual - General |
| 25.1583 | Operating limitations |
| 25.1585 | Operating procedures |
[Issue: CS-AWO/2]
SECTION 4 -SYNTHETIC VISION GUIDANCE SYSTEMS (SVGSS)
GENERAL