Part 2 builds on the climb session. The same performance formula applies — we
just change the power and attitude inputs to produce a descent rather than a
climb. Introduce the three types of descent with the same pattern used for the
three types of climb.
Mirror the structure from Part 1 where possible — students find it easier to
learn new content that follows a familiar pattern.
Return to these at the recap. Ask the student to answer each from memory before revealing.
Click Direct-To to advance to Forces in the Descent.
Key concept: the energy exchange in a glide — the aeroplane is converting potential energy (altitude) into kinetic energy (airspeed) to overcome drag. This is why best glide speed is not "as slow as possible".
**Actions**
- Reduce power from 60 to 50% and watch thrust reduce while drag stays
- Reduce attitude from 4 to 1.5 and watch drag increase
- Reduce the attitude to -8 degrees to show the components of the weight contributing to:
- Forward speed
- Balancing the lift
- **Still in balance** - not accelerating down or forward, just constant speed.
Reinforce the symmetry with the climb: the formula doesn't change, only the inputs. This is the core of attitude flying.
Click Direct-To to advance to Descent Entry and Exit.
PAT gets you into the descent; ALAP keeps you there. Same work cycle as the climb — three steps outside, one quick glance inside.
The contrast with the climb level-off (APT) is worth highlighting. In a descent, adding power first arrests the sink rate; then the attitude is raised to level. If you raise the nose first without adding power, the airspeed bleeds off rapidly.
Click Direct-To to advance to Types of Descent.
The table values are Warrior 151 examples — check the equivalent power settings and speeds for your training aeroplane before the lesson.
Mirror the three-types pattern from Part 1. Students can now see the parallel: three types of climb, three types of descent, each with its own use case.
Know the best glide speed and approximate glide ratio for your training aeroplane — for the Warrior 151 that's approximately 73 KIAS at max gross weight and a 10:1 glide ratio (for every 1000 ft, approximately 1.7 nm of range).
This is a critical airspeed to know — it will come up again in the engine failure forced landing lesson.
The "power = rate of descent, attitude = airspeed" rule is counterintuitive at first. Use this as a preview — they will practise it in earnest during circuits. Don't dwell too long here.
Click Direct-To to advance to Instrument Indications.
Emphasise that the instruments confirm what the attitude is producing — don't fly the VSI. The primary reference is always the nose position relative to the horizon.
Click Direct-To to advance to the recap.
Ask one at a time. End the session positively. The student now has the full picture for climbing and descending — ready to take it to the aeroplane in the flight brief.