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At 07:47 04 November 2013, Chris Rollings wrote:
One source of confusion on cockpit loads is that the airworthiness requirement for certification under JAR 22 was (and I think still is under the current regulations) that, with basic instrumentation, the minimum cockpit load must be not more than 70 Kg/154 lbs and the maximum not less than 110 Kg/ 242 lbs. Most gliders, if weighed and weight and balance calculations done, will have limits wider than this, in some cases much wider. Some time back, the major German manufacturers developed the practice of sending new gliders out of the factory placarded with the 70/110 kg limits, checking their weight and balance and calculating cockpit loads on delivery usually enabled the re-placarding of wider limits. This was a common practice in the UK, not sure if it was much done in the USA. I think you will find that the upper cockpit seat limit is fixed by the certification of the harness/attachment points which is why most gliders have 110kg (242lbs) as the seat limit. |
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