Appendix 1 to CS
CCD.200(b)(1) Aircraft difference table
ED Decision 2020/015/R
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Aircraft
difference table |
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Base aircraft |
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Candidate
aircraft |
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Determination elements |
Existing difference from base aircraft |
Description of identified differences |
Impact
assessment |
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(a) |
(b) |
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1. |
2. |
1. |
2. |
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Yes |
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AIRCRAFT CONFIGURATION |
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Single-aisled |
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Multi-aisled |
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Narrow-bodied |
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Wide-bodied |
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Single-passenger deck |
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Multi-passenger deck |
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DOORS AND EXITS |
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Number |
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Location |
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Features (e.g. door/exit assist handles) |
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Controls (e.g. door/exit locking indicators) |
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Electrical operation and malfunction |
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Direction of movement of the operating handle |
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Direction of the door/exit opening |
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Door/exit arming/disarming |
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Power assist mechanism and malfunction |
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Door/exit electrical warning system |
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Operation from inside in normal mode |
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Operation from inside in emergency mode |
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Operation from outside |
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Integral stair |
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Means assisting evacuation |
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Type, number and location of units (e.g. escape slide/slide raft/ramp slide) |
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Type and number of additional floatation means (e.g. life raft) |
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Single/multi-lane units |
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Life lines |
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Operation
(automatic/manual/ |
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Slide girt bar engagement (manual/automatic) |
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Means of signalling slide readiness (e.g. stop sign/barber pole) |
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Capacity and overload |
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Detaching and separating from aircraft |
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Slide/life raft survival kit (integral/separate) |
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Possibility to transfer slide/raft to another door/exit |
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Emergency
signalling system |
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AIRCRAFT SYSTEMS |
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(a)Â Â
emergency lighting system: |
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Controls |
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Interior emergency lighting |
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Exterior emergency lighting |
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(b)Â
evacuation alarm signal system: |
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Availability of an activation/indication panel (flight crew/cabin compartment) |
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Alert indications |
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(c)Â Â
smoke detection system: |
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Function and panels |
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Alert indications (aural/visual) |
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Availability of a smoke barrier |
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(d)Â
automatic fire‑extinguishing system: |
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Function of the built-in fire‑extinguishing system |
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(e)Â Â
drop-down oxygen system: |
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Type (e.g. gaseous, chemical) |
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Activation |
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Indications associated with the activation of the oxygen system (changes of cabin altitude); |
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(f)Â Â Â communication system: |
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Location of handset unit(s) |
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Possibility of interphone calls in normal and emergency circumstances between the different cabin compartments and between the cabin and flight crew compartments |
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Availability of aural/visual indications associated with interphone calls in normal and emergency circumstances |
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Signalling panels associated with the communication system |
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(g)Â Â public address system: |
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Location of the microphone unit when independent from the handset unit |
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Priority order of the public announcement system (flight crew handset/senior cabin crew member (SCCM) handset/any other cabin crew handset/evacuation signal alarm) |
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(h)Â control panels: |
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Cabin crew panel(s) — controls related to evacuation, lavatory smoke, emergency lights |
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(i)Â Â Â water system: |
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Availability of a manual water shut-off valve |
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(j)Â Â Â other systems as applicable: |
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NORMAL AND EMERGENCY PROCEDURES |
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Design-related element(s) impacting on either normal procedures or on emergency procedures or on both normal and emergency procedures that are relevant to the aircraft type |
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[Issue No: CCD/2]
EASA cabin crew regulations require an aircraft difference table to assess the impact of aircraft configuration, doors/exits, and systems on cabin crew procedures. This assessment covers elements like emergency lighting, communication, and evacuation systems, ensuring crew proficiency across different aircraft types for safety and emergency readiness.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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