المجموعات الإجتماعية |
البحث |
مشاركات اليوم |
ملتقى الطيارين Aviator forums ملتقى خاص بالطيارين العاملين بمختلف الشركات وطلاب الطيران والأطقم الجوية يناقش مسائل الطيران ،الحلول والنصائح |
إضافة رد |
|
أدوات الموضوع |
مشاركة [ 1 ] | ||||
|
||||
|
INTRODUCTION As the airplane climbs to a higher altitude; a higher thrust is required to maintain that altitude. When an engine failure occurs during cruise at high altitudes, the thrust available becomes suddenly less than the thrust required to maintain that altitude. As a result, the airplane must descent to a lower altitude, where the available thrust is equal to the required thrust to allow the airplane to level off. GROSS LEVEL OFF ALTITUDE It is the actual altitude flown by the aircraft after the engine failure. It is calculated based on: weight, altitude, ambient temperature, unfavorable CG, critical engine, and continuous thrust rating (FAR25.123). NET LEVEL OFF ALTITUDE It is the gross level altitude degraded by 1.1%, which is used by regulations for flight planning and terrain clearance. ROUTE STUDY: For any new route, a engine failure study must be made in order to ensure its safe operations or define the critical points in case of engine failures during cruise. Within five statue miles of the intended track: Condition 1 The net level altitude for the most conservative weight is higher than the highest obstacle enroute +1000 ft. not then condition 2 takes place. Condition 2 Identify the critical points on the route where level altitude for the most conservative weight clear all obstacles enroute by a minimum of 2000 ft. critical points can be: a) no return point: passing this point, the turn clear the obstacles by 2000 ft. b) continuing point: passing this point, the continuation possible to clear all obstacles by 2000 ft. In case the no return point is located continuing point, the area bet be used to return or to continue the flight But in case the no return point is located before the continuing point, a diversion route or procedure must be established, less weight is considered, or route is to be considered ” F.O HASHIM HASHIM |
|||
مشاركة [ 2 ] | ||||
|
||||
|
شكرا لك كابتن خالد على المعلومات القيمة
تحياتي |
|||
مشاركة [ 3 ] | ||||
|
||||
|
الشكر لله ثم للكابتن هاشم فقد زودني بهذه المعلومات اشكر لك طلتكم الحلوة ياكابتن.
|
|||