Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p98
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 335976–340173

grass surfaces;
        6.          limitations, such as those imposed by local noise abatement procedures and curfews;
        7.        operational hazards, which may include variable surfaces, loose objects, personnel, birds and propeller wash, rotor wash and jet blast;
        8.        simulated abnormal and emergency situations;
        9.          simulated hazardous weather.

 2.                     Underpinning knowledge of the following:
        1.        general aircraft data;
        2.        make, type and model of helicopter, designation of engines, take-off and rated power;
        3.         stated airspeed limitations including, but not limited to: VNE (at varying AUW and density altitudes) VH, configuration airspeed limits VLO, VTURB, maximum cross-wind;
        4.        low speed wind limits;
        5.        RRPM limits (Power ON and Power OFF);
        6.          engine, transmission and any other stated limits in the RFM;
        7.        slope landing limitations (if available);
        8.        emergency procedures for the following:
               1.          engine failure in the hover;
               2.         taxiing;
               3.       during transitions before and after take-off;
               4.       in the cruise;
               5.         on final approach before and after landing;
               6.       engine fire on the ground and airborne;
               7.      electrical fire on the ground and airborne;
               8.    cabin fire in flight;
        9.          N1, torque split indications;
       10.          identify malfunctioning governor in flight and manage the related engine;
       11.         corrective action to be taken when engine run-up or run-down has been diagnosed;
       12.          the following weight and balance topics:
               1.          weight, balance and performance;
               2.         permissible take-off weight;
               3.       maximum gross weight, landing weight, ramp weight and zero fuel weight;
               4.       centre of gravity position for any specified conditions;
               5.         centre of gravity limitations;
               6.       appropriate charts to determine centre of gravity;
               7.      calculated centre of gravity position and confirm it is within limits;
       13.      the following take-off and landing topics:
               1.          continuing and rejected take-off distances;
               2.         take-off decision point;
               3.       landing decision point;
       14.        climb performance, hover out of ground effect and height–velocity diagram charts;
       15.        failed engine operations;
       16.        the following aircraft systems:
               1.          fuel system;
               2.         hydraulic system;
               3.       electrical system;
               4.       oil system;
               5.         stability augmentation, AFCS and FDS (as applicable);
               6.       anti-icing and de-icing systems (as applicable);
               7.      heating and ventilation systems;
               8.    pitot and static system;
               9.       fire extinguisher system (as applicable);
              10.         engine systems;
              11.       transmission and rotor systems;
              12.      display systems (as applicable);
              13.    undercarriage system (fixed or retractable as applicable);
       17.        the following key hazards including, for each, the typical causal factors and contributing operational situations, avoidance and recognition of symptoms and recovery techniques:
               1.          vortex ring state;
               2.         ground resonance;
               3.       loss of tail rotor effectiveness (LTE);
               4.       low 'g' and mast bumping;
               5.         overpitching or low RRPM – rotor stall;
               6.       retreating blade stall;
               7.      recirculation;
               8.    dynamic rollover.

TR-MEH Type rating – multi-engine helicopter

 1.                     Unit description
This unit describes the skills