each second 24 Engine thrust/ R Full range Each As installed 0.1% of full *Sufficient torque engine range parameters e.g. parameters each EPRN/N1 or required to second torque/Np as determine appropriate to the propulsive particular engine thrust/ power* be recorded to determine power in both normal and reverse thrust. A margin for possible overspeed should be provided. 25 Engine gas R 0-150% Each As installed 0.2% of full -- generator engine range speed (Ng) each second 26 Free R 0-150% Each As installed 0.2% of full -- turbine speed engine (Nf) each second 27 Coolant R Full range 1 As installed 1˚C -- temperature (±5˚C recommended) 28 Main voltage R Full range Each As installed 1 Volt -- engine each second 29 Cylinder head R Full range Each As installed 2% of full -- temperature cylinder range each second 30 position R Full range or 2 As installed 0.5˚ -- each discrete position 31 Primary flight R Full range 0.25 As installed 0.2% of full -- control surface range position 32 Fuel quantity R Full range 4 As installed 1% of full -- range 33 Exhaust gas R Full range Each As installed 2% of full -- temperature engine range each second
each second 24 Engine thrust/ torque parameters required to determine propulsive thrust/ power* R Full range Each engine each second As installed 0.1% of full range *Sufficient parameters e.g. EPRN/N1 or torque/Np as appropriate to the particular engine be recorded to determine power in both normal and reverse thrust. A margin for possible overspeed should be provided. 25 Engine gas generator speed (Ng) R 0-150% Each engine each second As installed 0.2% of full range -- 26 Free turbine speed (Nf) R 0-150% Each engine each second As installed 0.2% of full -- 27 Coolant temperature R Full range 1 As installed (±5˚C recommended) 1˚C -- 28 Main voltage R Full range Each engine each second As installed 1 Volt -- 29 Cylinder head temperature R Full range Each cylinder each second As installed 2% of full range -- 30 position R Full range or each discrete position 2 As installed 0.5˚ -- 31 Primary flight control surface position R Full range 0.25 As installed 0.2% of full range -- 32 Fuel quantity R Full range 4 As installed 1% of full range -- 33 Exhaust gas temperature R Full range Each engine each second As installed 2% of full range --
07_MCAR_Part-7_and_IS_V2.8.docx