Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p101
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 346594–350629

failure;
                2.        maintain RRPM within the prescribed limits and control of the helicopter;
                3.         correctly identify and confirm the failed engine(s) and at the appropriate time, complete the engine failure shutdown checklist for the following situations:
                       1.          engine failure prior to reaching take-off decision point:
                              1.       conduct the rejected take-off procedure in accordance with AFM and POH;
                              2.       apply the appropriate power within the AFM limits for the configuration being flown;
                              3.       perform a controlled landing in the rejected take-off distance available;
                       2.         engine failure after take-off:
                              1.       maintain control of the helicopter;
                              2.       set maximum contingency power on serviceable engine;
                              3.       accelerate to VTOSS (if applicable);
                              4.       identify and confirm failed engine;
                              5.       at the appropriate time, complete the engine failure shutdown checklist;
                              6.        climb multi-engine helicopter not below VYSE;
                              7.       land helicopter at nearest appropriate landing area.
     3.               TR-MEH.3 – Control helicopter in normal flight
Set power and maintain attitude to establish and maintain the following manoeuvres with the helicopter in balanced flight and trimmed (as applicable) within prescribed tolerances as follows:
 1.        straight and level:
        1.          straight and level flight at normal cruise;
        2.         maintains heading;
        3.       maintains nominated altitude;
 2.        straight climbs and descents:
        1.          maintain IAS for best angle of climb (VX);
        2.         maintain IAS for best rate of climb (VY);
        3.       maintain IAS for cruise climb;
        4.       maintain IAS for cruise descent;
        5.         maintain correct power setting as applicable to the rotorcraft;
        6.       maintain heading;
 3.         turn onto specific headings (using magnetic compass) or geographical feature within the flight tolerances for the following:
        1.          level turn
        2.         climbing turn, rate 1 or 20° bank;
        3.       powered descending turn, 30° bank.
 1.               TR-MEH.4 – Control helicopter during advanced manoeuvres
        1.        perform steep turns (45º) within the flight tolerances as follows:
               1.          level turn altitude;
               2.         exits on specified heading or geographical feature;
        2.        perform autorotative flight:
               1.          enters and maintains autorotative flight at nominated speed in balanced flight for the following profiles:
                      1.       descend at nominated heading and manufacturer's recommended speed;
                      2.       conduct 180o autorotations using up to 45o angle of bank;
                      3.       autorotative flight at best range speed and minimum descent rate speed;
                      4.       maintains RRPM within limitations;
        3.         perform power termination:
               1.          maintain RRPM within limitations;
               2.         ensure throttle(s) is at 100% (or the equivalent terminology) prior to the commencement of the flare;
               3.       commence flare at appropriate height for the prevailing conditions and reduce ground speed and rate of descent;
               4.       control attitude to achieve a decreasing closure rate and reducing rate of descent;
               5.         control yaw, engine and RRPM;
               6.       terminate the helicopter to a hover or hover taxi within tolerances of termination point without lateral or rearward drift.
 2.               TR-MEH.5