HI.V.C.R3
Risk managementLimitations during starting.
From the FAA library
- Chapter 7: Aircraft Systems › Turbine Engines › Foreign Object Damage (FOD)
utilized. Preflight procedures include a visual inspection for any sign of FOD. Turbine Engine Hot/Hung Start When the EGT exceeds the safe limit of an aircraft, it experiences a “hot start.” This is caused by too much fuel entering…
- Chapter 9: Basic Flight Maneuvers › Hovering—Rearward Flight › Technique
hovering height. 4. Failure to maintain proper rpm. 5. Failure to make sure the area is clear prior to starting the maneuver. Hovering—Rearward Flight Rearward hovering flight may be necessary to move the helicopter to a specific area when ... heading. Due to the limited visibility behind a helicopter, it is important that the area behind the helicopter be cleared before beginning the maneuver. Use of ground personnel is recommended. Technique Before starting rearward hovering flight, pick out two reference…
- Chapter 9: Basic Flight Maneuvers › Hovering Turn › Technique
right turn can be successfully controlled. The opposite applies to helicopters with clockwise rotor systems. In this case, start the turn to the right. Hovering turns should be avoided in winds strong enough to preclude sufficient aft cyclic control ... selected surface reference point when headed downwind. Check the flight manual for the manufacturer’s recommendations for this limitation…
- Chapter 9: Basic Flight Maneuvers › Normal Takeoff from a Hover › Technique
takeoff, the pilot should ensure that the proper checklist has been completed and the helicopter systems are within normal limits. During the takeoff, fly a profile that avoids the cross-hatched or shaded areas of the height/velocity diagram. Technique Refer ... from neutral. Flight controls must move freely, and the helicopter should respond normally. Then, visually clear the surrounding area. Start the helicopter moving by smoothly and slowly easing the cyclic forward (position 2). As the helicopter starts to move forward…
- Chapter 7: Aircraft Systems › Electrical System
charge in the battery. Electrical energy stored in a battery provides a source of electrical power for starting the engine and a limited supply of electrical power for use in the event the alternator or generator fails. Most DC generators ... aircraft have receptacles to which an external ground power unit (GPU) may be connected to provide electrical energy for starting. These are very useful, especially during cold weather starting. Follow the manufacturer’s recommendations for engine starting using…
- Chapter 6: Weight and Balance › Weight
following terms are used when computing a helicopter’s weight: • Basic Empty Weight • Maximum Gross Weight • Weight Limitations Basic Empty Weight The starting point for weight computations is the basic empty weight. This is the weight of the standard helicopter…