Tailwinds Flying Club Spring Safety Session - 2007

1. Tailwinds Flying Club Spring Safety Session - 2007

2. Take-Off Accidents* Take-off accidents accounted for 18.4% (227) of all accidents for 2005. Single-Engine fixed-Gear Aircraft take-off accidents accounted for 15.3% (122). Of these, 13.2% (20) were fatal. The leading cause list found Takeoff/Climb to be number three in fatal accidents during 2005. * Based on the 2006 Nall Report - AOPA Air Safety Foundation.

3. Scenario Cherokee Six – PA32-300 Maximum Takeoff Weight (lbs) – 3400 Normal Take-Off Performance - Take-off Distance - 1,200 Ft. (69 KIAS, 10 Degree Flaps) Best Rate of Climb Speed - 89 KIAS Best Angle of Climb Speed - 79 KIAS Best Gliding Angle - 87 KIAS

4. Scenario Lake Elmo Airport (21D) Rwy. 04/22 - 2497’ X 75’ Asphalt Rwy. 14/32 - 2850’ X 75’ Asphalt Field Elevation – 932 MSL

5. Scenario Conditions Standard Temperature - 60 Degrees Dew Point - 40 Degrees No Wind Clear Sky Runway Dry

6. Scenario Cherokee Six Performance Landing Distance Over 50’ Barrier – 1050’ Landing Ground Roll (40 degree Flaps) – 675’ Glide Performance with no flaps, propeller windmilling, full decrease, airspeed 87 KIAS From 500’ AGL - 4,200’ From 200’ AGL - 1,200’

7. Cherokee Six ProceduresEngine Power Loss During Takeoff The proper action to be taken if loss of power occurs during takeoff will depend on the circumstances of the particular situation. If sufficient runway remains to complete a normal landing, land straight ahead. If the area ahead is rough, or if it is necessary to clear obstructions, maintain a safe airspeed and maneuver gently to avoid obstacles, making only shallow turns if necessary. Use of flaps depends upon circumstances. Normally, flaps should be fully extended for touchdown. If sufficient altitude has been gained to attempt a restart, maintain a safe airspeed and switch the fuel selector to another tank containing fuel. Check the electric fuel pump to insure that it is “ON” and that the mixture is “RICH”. The alternate air should be “OPEN”. If engine failure was caused by fuel exhaustion, power will not be regained after switching fuel tanks until the empty fuel lines are filled. This may require up to ten seconds. If power is not regained proceed with the Power Off Landing procedure.

8. Cherokee Six Procedures - Power Off Landing If loss of power occurs at altitude, trim the aircraft for best gliding angle (87 KIAS) and look for a suitable field. If measures taken to restore power are not effective, and if time permits, check your charts for airports in the immediate vicinity; it may be possible to land at one if you have sufficient altitude. At best gliding angle, with the engine windmilling, and the propeller control in full “DECREASE” rpm, the aircraft will travel approximately 1.5 miles for each thousand feet of altitude. If possible, notify the FAA by radio of your difficulty and intentions. If another pilot or passenger is aboard, let him/her help. When you have located a suitable field, establish a spiral pattern around this field. Try to be at 1000 feet above the field at the downwind position, to make a normal landing approach. When the field can easily be reached, slow to 80 KIAS with flaps down for the shortest landing. Excess altitude may be lost by widening your pattern, using flaps or slipping, or a combination of these. When committed to landing, close the throttle control and shut “OFF” the master and ignition switches. Flaps may be used as desired. Turn the fuel selector valve to “OFF” and move the mixture to idle cut-off. The seat belts and shoulder harness should be tightened. Touchdown should be normally made at the lowest possible airspeed.

10. Pilot’s view departing 04 @ 200’ AGL

11. Pilot’s view departing 04 @ 400’ AGL

12. Pilot’s view departing 04 @ 600’ AGL

14. Pilot’s view departing 22 @ 200’ AGL

15. Pilot’s view departing 22 @ 500’ AGL

18. Announcements MAC Town Hall Meeting – June 18 Garmin 430 GPS Questions Hangar Roof Repair and Office Construction

19. Thank You!