Title: EASA Rulemaking Group CS 25.045
1- EASA Rulemaking Group CS 25.045
- Access through Bulkheads
2EASA CS 25.045 - Access Through bulkheads
In August 1985 a B737-200 at Manchester
Airport, UK, suffered an uncontained engine
failure while on the ground that resulted in fire
rapidly penetrating the cabin with subsequent
loss of life. In the UK-AAIB accident report
(Ref. AAIB 8/88), it was highlighted that the
relatively narrow aisle width (22 ½ inches)
between monuments (toilets, galley, stowage
compartments, etc) in combination with the panic
induced competitive behaviour of passengers
trying to evacuate, caused blockage of the aisle
leading to the front and overwing exits
3EASA CS 25.045 - Access Through bulkheads
The former JAA Cabin Safety Study Group (CSSG)
got the task to develop a NPA to address this
Issue An analysis was carried out in 1996, under
the auspices of the JAA CSSG, of accident data
over a 10-year period between 1984 and 1993 for
large, western built, commercial jet and
turboprop aeroplanes, and an ANPA 25D-224
developed.
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- Following the Manchester accident regulatory
action has been taken by many Airworthiness
Authorities. - The purpose of the EASA NPAs is to propose an
amendment to CS 25.813 (a) and CS 25.815, if
necessary, to improve safety standards. - EASA established a Working Group (25-045) with
the following TOR tasks - Review of JAA ANPA and comments
- Develop RIA, based on that
- View the need of rulemking, both CS 25 and JAR
26.
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GROUP MEMBERS John MAYDEW BAE Systems Jan VAN
DE MAAT KLM Royal Dutch Airlines (AEA) Alfred
AULETA FUTURA International (IACA) Jürgen
FELDHAUS Airbus Deutschland GMBH (Airbus) Jan
NOVAK EASA - EASA Focal Point Ray
CHERRY R.G.W (EASA) Group Secretary Carmela
TRIPALDI ENAC Josef MAURER CSA Czech Airlines
(ETF) Jeff GARDLIN FAA Claude
LEWIS Transport Canada Michael MARKUS Austro
Control Peter CHITTENDEN EASA Enrique
NIN DGAC Spain
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MEETINGS HELD DURING 2006 Meeting no 1 held
30th March 2006 Meeting no 2 held 1st June
2006 Meeting no 3 held 7th September
2006 Meeting no 4 held 15th November
2006 MEETINGS HELD DURING 2007 Meeting no 5
to be held 25th January 2007
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- GROUP WORKING PROCEDURES
- EASA Rulemaking Procedures
- EASA Rulemaking Process
- Determination of the Membership of Rulemaking
Groups -
- Terms of Reference, Definition and Timescales.
- Rulemaking Group T reference
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- GROUP EXPECTED OUTPUTS
- RIA for (JAR 26 and CS-25).
- NPA to be presented.
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- THE FOLLOWING APPROACH HAS BEEN TAKEN BY THE EASA
WORKING GROUP - Review analyses ( Accident data) from JAA, where
are the numbers in respect of fatalities are
coming from? - Review of test done ( Cranfield). Have all
variants been approached ( as thickness, height,
single aisle / multiple aisle,etc) ? - Review of recent accident data.
- Consultation of NTSB, Canadien Accident
Investigation Board and British Accident
Investigation Board on new investigations,
recommendations, look on cabin Safety
improvements (as seats , heat release, smoke
density, etc). - Investigation on foreign Authorities intentions
in respect of potential rulemaking. -
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MAIN DOCUMENTATION
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SUPPORTING DOCUMENTATION
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TEST HARMONISATION DOCUMENTATION
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- GROUP CONCLUSIONS (1)
- From 1985, new aircraft designs and existing
aircraft modified by retroactive rules, resulting
in significant cabin safety improvements
including the following - Seat fire blocking layers
- Floor proximity lighting/marking
- Enhanced Fuselage Burnthrough protection
- Reduced heat release of cabin interior materials
- Reduced smoke emission from cabin interior
materials - Improved access to Type III exits
- In addition Enhanced Fuselage Burnthrough
protection from pool fires is an FAA regulation
and is under consideration by EASA.
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- GROUP CONCLUSIONS (2)
- The proposed regulatory action would have a
neligible benefit in improving occupant
survivability. - Main arguments to adopt this position are
- Accidents analysis during this period of time, in
terms of incidents and accidents by flight/
hours - Balance between Extremely remote risk and
related costs - Experimental trials results
- Specific scenario improved by new CS 25 and FAR
25 standards, since 1985 - No enough evidences had been found in test and
supporting documentation to ensure an
improvement in evacuation conditions.
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GROUP CONCLUSIONS (3) The FAA and Transport
Canada have stated that, based on the information
currently available they have no regulatory
activity planned in this area. Hence, if EASA
decided to proceed with rulemaking it would not
be harmonised with other major Airworthiness
Authorities.
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ACTUAL STATUS Draft A-NPA has been drafted and
is under consideration at EASA. Finally it
will be distributed within the working group for
concurrence and then provided to EASA for public
consultation.