| |||||
|
STEEP SPIRALDescriptionA maximum performance maneuver that requires you to combine steep-spiraling descent with the basic elements of turns about a point. ObjectiveTo develop pilot techniques for airspeed control, wind drift control, planning, orientation, and division of attention, with practical application for emergency landings. Elements· Clear the area · Choose forced landing area (ideally adjacent to encircling point) · Configure aircraft: straight-and-level, altitude sufficient to allow three complete turns and still be ≥1000’ AGL, (C172RG: 5000’ AGL minimum), CCGUMPS (propeller to full), flaps 0º · Select outside references (point to encircle, ideally adjacent to a forced landing area) · Throttle to idle, propeller to full · Establish best glide speed (C172RG: 75 KIAS 0º Flaps) · Establish a constant radius circle allowing a bank of ≤60º about ground reference point o Close enough to allow no more than 60º of bank at the steepest point · Maintaining a constant airspeed by adjusting pitch and bank as necessary to correct for wind · Trim as necessary · Clear the engine when into the wind (advance throttle to normal cruise momentarily) · Complete at least three complete 360º turns, but do not descend below 1000’ AGL unless the maneuver is to be followed by an emergency landing · Maintain ball centered · Look for traffic
Objective with a 60º bank is to get down fast (high bank eliminates lift component) safely. Common Errors· Failure to clear area · Failure to maintain constant airspeed · Poor coordination, resulting in skidding and/or slipping · Inadequate wind drift correction · Failure to coordinate the controls so that no increase/decrease in speed result when straight glide is resumed · Failure to scan for other traffic · Failure to maintain orientation ReferencesFAA-H-8083-3A Airplane Flying Handbook p. 9-3 This document is provided as is. It is intended for use by authorized instructors only. Please double-check all content before using. © 2008
Derek W Beck. Some Rights
Reserved.
Licensed
under a US Creative
Commons Attribution-Noncommercial-Share Alike. |
||||
| |||||