Sunday, September 28, 2008 1:16:03 AM
See below:
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ED Decision 2003/14/RM
Final
14/11/2003
European Aviation Safety Agency
DECISION NO. 2003/14 /RM
OF THE EXECUTIVE DIRECTOR OF THE AGENCY
of 14 November 2003
on certification specifications, including airworthiness codes and acceptable means of
compliance for normal, utility, aerobatic and commuter category aeroplanes (« CS-23 »)
CS 23.1 Applicability
(a) This airworthiness code is applicable to –
(1) Aeroplanes in the normal, utility and
aerobatic categories that have a seating
configuration, excluding the pilot seat(s), of nine
or fewer and a maximum certificated take-off
weight of 5670 kg (12 500 lb) or less; and
(2) Propeller-driven twin-engined
aeroplanes in the commuter category that have a
seating configuration, excluding the pilot seat(s),
of nineteen or fewer and a maximum certificated
take-off weight of 8618 kg (19 000 lb) or less.
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Intergrity does not meet either category for applicablility!!
Sorry, your case and test pilot just went down in flames. Thanks for giving us the proof we need to write this one off.
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