Betekenis van:
engine failure

Voorbeeldzinnen

1. Engine failure;
2. engine failure;
3. an engine failure during take-off;
4. An engine failure during take-off;
5. consideration of engine failure in all flight phases.
6. Consideration of engine failure in all flight phases.
7. Assumed engine failure height above the runway versus RVR/Visibility
8. Assumed engine failure height above the take-off runway
9. When engine out manoeuvres are carried out in an aeroplane, the engine failure must be simulated.
10. Repairs to the components of an engine selected for testing over a service accumulation schedule other than the engine, emission control system or fuel system shall be performed only as a result of part failure or engine system malfunction.
11. The torque limiter shall be activated in accordance with section 6.5.5 if the failure is not remedied within 50 hours of engine operation.
12. Take-off in minimum authorised RVR conditions with an engine failure between V1 and V2, or as soon as safety considerations permit; and
13. The net flight path must have a positive gradient at 1500 ft above the aerodrome where the landing is assumed to be made after engine failure.
14. In the case of an engine equipped with a particulate filter, examples of monitoring for major functional failure are for major melting of the trap substrate or a clogged trap resulting in a differential pressure out of the range declared by the manufacturer, any electrical failure of a component (e.g. sensors and actuators, dosing control unit) of a particulate filter, any failure, when applicable, of a reagent dosing system (e.g. clogged nozzle, dosing pump failure).
15. ‘Auxiliary control device’ means a system, function or control strategy installed to an engine or on a vehicle, that is used to protect the engine and/or its ancillary equipment against operating conditions that could result in damage or failure, or is used to facilitate engine starting.