| A | B |
|---|
| Subsonic stalls are always caused by | Excessive angle of attack |
| Supersonic stalls are caused by | Shock Waves |
| Power-Off stall | Landing configuration |
| Power-On stall | Occur during take-off & climb |
| Accelerated stall | Occur during steep turns |
| Cross-controlled stall | Usually occur during overshoots of the runway. |
| Secondary stall | Caused by poor stall recovery technique |
| 1st step in stall recovery | Decrease angle of attack |
| 2nd step in stall recovery | Apply maximum power |
| 3rd step in stall recovery | Adjust power as required |
| Prerequisite for a spin | Stall |
| Most dangerous spin | Flat Spin |
| Most common spin | Erect spin |
| 1st step in spin recovery | Throttle to idle |
| 2nd step in spin recovery | Neutralize the ailerons |
