4.1 Aircraft Performance

4.1.1 Flight Crew is able to determine

  • Maximum structural weight

  • Takeoff performance

  • Maximum brake energy and cooling time

  • Climb Performance (Distant obstacle)

  • Landing performance

  • Determine performance for emergency alternate


4.1.2 Flight Crew able to determine performance in regards to the following

  • Flight Crew is able to determine performance that is affected by


4.1.3 Flight Crew is able to determine eroute engine out performance

  • Service Ceiling

  • Drift down altitude

  • Terrain clearance along route to destination or alternate


4.1.4 PIC is able to determine if all-engine Climb Gradient is adequate

  • An one of the following


4.2.1 Flight will not commence unless the ground facilities are acceptable for operations

  • Such as


4.2.2 Analysis of new route/Airport

  • Analysis is done on


4.2.3 En route airport for emergency on remote routes

  • Identified and described for PIC to use


4.2.4 Guidance, data and procedure to determine minimum safe altitudeMinimum

  • Minimum safe altitude data and procedure

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