ATPL » Performance – Helicopter » Derivation of operational performance standards
51.6 Derivation of operational performance standards
51.6.2 Derive, from sample Company Operations Manual data, the following:
(a) the factors which limit the maximum take-off weight
(b) the maximum gross take-off weight limitation, for day VFR operations
(c) the en route performance capability, for day VFR operations
(d) the approach and landing performance capability, for day VFR operations
(e) the maximum gross take-off weight limitation, for IFR and night VFR operations
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