Which items must be verified when executing the Go-Around Procedure?

Prepare for the Delta 737 PA-LOD Exam with flashcards and multiple choice questions. Each question includes hints and explanations, ensuring you're ready for exam day!

Multiple Choice

Which items must be verified when executing the Go-Around Procedure?

Explanation:
When you initiate a go-around, you’re making a deliberate transition from landing configuration to a positive climb, and you need coordinated control inputs and correct guidance display to ensure safety. The rotation to the go-around pitch attitude sets the airplane up for a proper climb rather than continuing toward the runway; it provides the immediate nose-up cue necessary to start gaining altitude without stalling. The thrust setting must be advanced to the go-around power (TO/GA or the designated go-around thrust) so the airplane has the required climb performance and steering authority. Finally, the proper FMA mode annunciation confirms the flight guidance system and autopilot are in the go-around mode, directing the aircraft along the intended climb path with the correct pitch and flight-path guidance. Putting these together, all of these aspects need to be verified to ensure a safe, controlled go-around: appropriate pitch, correct thrust, and correct automation guidance. If any one of these is out of alignment, the aircraft can fail to climb as required, or guidance can be lost or misinterpreted.

When you initiate a go-around, you’re making a deliberate transition from landing configuration to a positive climb, and you need coordinated control inputs and correct guidance display to ensure safety. The rotation to the go-around pitch attitude sets the airplane up for a proper climb rather than continuing toward the runway; it provides the immediate nose-up cue necessary to start gaining altitude without stalling. The thrust setting must be advanced to the go-around power (TO/GA or the designated go-around thrust) so the airplane has the required climb performance and steering authority. Finally, the proper FMA mode annunciation confirms the flight guidance system and autopilot are in the go-around mode, directing the aircraft along the intended climb path with the correct pitch and flight-path guidance.

Putting these together, all of these aspects need to be verified to ensure a safe, controlled go-around: appropriate pitch, correct thrust, and correct automation guidance. If any one of these is out of alignment, the aircraft can fail to climb as required, or guidance can be lost or misinterpreted.

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