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XC Planning Checklist (Jeppeson GFM) Pilotage Navigation by reference to landmarks or checkpoints. Scalability and RF turn capabilities is mandatory in RNP AR DP eligibility. The separate Equipment Requirements box will list ground-based equipment and/or airport specific requirements. If an alternate is required, the alternate airport must have an instrument approach while meeting certain criteria: 800' ceiling, 2 miles visibility, if non-precision approach, 600' ceiling, 2 miles visibility, if precision approach, If no approach exists for the alternate runway, descent from cruising altitude must be possible under Visual Flight Rules, Note that minimums published for approaches may differ, Navigation can be accomplished in several ways, Two examples include pilotage and dead reckoning which, although different, are not mutually exclusive, Dead recokoning is navigation by planning, When track = course you are flying exactly where you intend, Various tools are necessary to complete a flight plan, Generally the most direct route is preferred but several considerations may require some deviation, Checkpoints allow you to follow the progress of your flight against your planning calculations, Landmarks can be checkpoints but may also inform a pilot where they are in relation to checkpoints. Preflight Planning - CFI Notebook Pilots are required to use SBAS to fly to the LPV or LP minima. RNP AR DP has lateral accuracy values that can scale to no lower than RNP 0.3 in the initial departure flight path. RF turn capability is optional in RNP APCH eligibility. When using full automation, pilots should monitor the aircraft to ensure the aircraft is turning at appropriate lead times and descending once established on-course, Pilots flying TSO-C129 navigation system equipped aircraft without full automation should use normal lead points to begin the turn. As wind gets factored in, even if a round trip with consistent winds, the time to fly becomes longer - headwinds/tailwinds will not cancel out (see: Suppose D = distance, TT = total time, AS = air speed, WS = wind speed, Then the equation for a direct headwind and tail wind is TT = D/(AS - WS) + D/(AS + WS) = 150/(100 - 50) + 150/(100 + 50) = 150/50 + 150/150 = 450/150 + 150/150 = 600/150 = 4, With WS = 0 the equation becomes TT = 150/100 + 150/100 = 300/100 = 3, You will travel 10% of speed in 6 minutes. Copyright 2023 CFI Notebook, All rights reserved. Navigation Systems and Radar Services Lesson Plan Introduction: To determine that the applicant exhibits satisfactory knowledge, risk management, and skills associated with a forward-slip to a landing References: FAA-H-8083-2, FAA-H-8083-3; POH/AFM; AIM Attention: Research a case study There are other objects or structures that could adversely affect your flight, such as construction cranes near an airport, newly constructed buildings, new towers, etc.