135 Turbine Landing Limitations Question
10-26-2011, 01:43 PM
#11
New Hire
Joined APC: Oct 2008
Position: G200 Captain
Posts: 8
Also I found this in the 8900. This is an exact quote.
"E. Application of Flight Handbook Performance Limits. Many of the requirements of Subparts I of part 121 and part 135 apply only until the aircraft takes off from the departure point. Other requirements from these subparts apply at all times as do the AFM limitations. For example,§§ 121.195 and 135.385 prohibit a large, turbine airplane from takeoff unless, allowing for en route fuel burn, the airplane will be capable of landing on 60 percent of the available runway at the planned destination. The regulations do not, however, prohibit the airplane from landing at the destination when, upon arrival, conditions have changed and more than 60 percent of the runway is required. In this case, the airplane must only be able to land on the effective runway length as shown in the flight manual performance data."
"E. Application of Flight Handbook Performance Limits. Many of the requirements of Subparts I of part 121 and part 135 apply only until the aircraft takes off from the departure point. Other requirements from these subparts apply at all times as do the AFM limitations. For example,§§ 121.195 and 135.385 prohibit a large, turbine airplane from takeoff unless, allowing for en route fuel burn, the airplane will be capable of landing on 60 percent of the available runway at the planned destination. The regulations do not, however, prohibit the airplane from landing at the destination when, upon arrival, conditions have changed and more than 60 percent of the runway is required. In this case, the airplane must only be able to land on the effective runway length as shown in the flight manual performance data."
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