search.noResults

search.searching

saml.title
dataCollection.invalidEmail
note.createNoteMessage

search.noResults

search.searching

orderForm.title

orderForm.productCode
orderForm.description
orderForm.quantity
orderForm.itemPrice
orderForm.price
orderForm.totalPrice
orderForm.deliveryDetails.billingAddress
orderForm.deliveryDetails.deliveryAddress
orderForm.noItems
MY 2 CENTS


aircraft, the engine will follow the rotor rpm and an overspeed of the engine might also occur using the power-on autorotative profile procedure. Is this preventable? Of course, with a qualified pilot or instructor who understands these variables and the


required corrective


actions, they can negate any overspeed issues. Training is key!


I offer an alternative solution: Utilize a qualified instructor pilot who has the skills and ability to conduct proper power-off training and not overspeed the helicopter. This


approach, utilized for decades,


provides the pilot with the additional experience to accurately perceive critical engine failure elements such as low rotor rpm, ability to vary glide distance, accurate flare altitudes and timing of pitch application for ground contact, and much, much more.


In early July 2024, I engaged the helicopter community via social media asking


their opinion regarding this


topic. Without question, the resounding response was that power-off autorotative training is the right way to go.


All the aspects of the pilots’ feel related to the energy of the autorotative maneuver is lost when the engine remains driving the


rotor system during the descent


profile. There is no correlation between a power-on and power-off autorotative descent profile other than you’re headed to the ground. To be more specific, the lifesaving skills that would be taught during autorotative descent training are not achievable when the throttle remains on. This dilutes the training effort.


It is important to note this discussion has nothing to do with power-on or power- off landings. We’re discussing only the descent profile prior to the flare of the maneuver.


I don’t know of any high-rotor RPM- related autorotative helicopter crashes, but I know of many helicopter crashes with


loss of life related to low-rotor


RPM. The use of power-on autorotative descent profiles eliminates the low-rotor rpm training opportunity, thus limiting the pilot’s ability to survive such an event, especially when survival is the goal.


Randy Rowles has been an FAA pilot examiner for 20 years for all helicopter certificates and ratings. He holds an FAA Gold Seal Flight Instructor Certificate, NAFI Master Flight Instructor designation, and was the 2013 recipient of the HAI Flight Instructor of the Year Award. Rowles is currently the owner of the Helicopter Institute. He can be reached at randyrowlesdpe@ gmail.com


rotorpro.com


9


Page 1  |  Page 2  |  Page 3  |  Page 4  |  Page 5  |  Page 6  |  Page 7  |  Page 8  |  Page 9  |  Page 10  |  Page 11  |  Page 12  |  Page 13  |  Page 14  |  Page 15  |  Page 16  |  Page 17  |  Page 18  |  Page 19  |  Page 20  |  Page 21  |  Page 22  |  Page 23  |  Page 24  |  Page 25  |  Page 26  |  Page 27  |  Page 28  |  Page 29  |  Page 30  |  Page 31  |  Page 32  |  Page 33  |  Page 34  |  Page 35  |  Page 36  |  Page 37  |  Page 38  |  Page 39  |  Page 40  |  Page 41  |  Page 42  |  Page 43  |  Page 44  |  Page 45  |  Page 46  |  Page 47  |  Page 48  |  Page 49  |  Page 50  |  Page 51  |  Page 52  |  Page 53  |  Page 54  |  Page 55  |  Page 56  |  Page 57  |  Page 58  |  Page 59  |  Page 60  |  Page 61  |  Page 62  |  Page 63  |  Page 64  |  Page 65  |  Page 66  |  Page 67  |  Page 68  |  Page 69  |  Page 70  |  Page 71  |  Page 72  |  Page 73  |  Page 74  |  Page 75  |  Page 76  |  Page 77  |  Page 78  |  Page 79  |  Page 80  |  Page 81  |  Page 82  |  Page 83  |  Page 84