Генераторы переменного Техническое описаниека LSA. Установка by Somer Leroy

By Somer Leroy

Leroy Somer. Генераторы переменного Техническое описаниека LSA. Установка и техническое обслуживание

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11. 12. 13. 14. 15. 16. 17. 18. 2) ATTITUDE INDICATOR 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 32. 33. 34. 35. 36. 37. 38. ,. • 32 INSTRUMENT PANEL F-86D-5 AND SUBSEQUENT AIRPLANES 3tl 1. 2. 3. 4. 5. 6. 7. B. 9. 10. 11. 12 13. 14. 15. 16. 26 25 24 23 20. 21. 22. 23. LOCKUP INDICATOR LIGHT' RIGHT INSTRUMENT SUBPANEL STAND-BY COMPASS FUEL FLOWMETER' VARIABLE-NOZZLE POSITION INDICATOR' 24. LOCKUP INDICATOR LIGHT' 25. CANOPY LOCK HANDLE' 26. FUEL QUANTITY GAGE TEST SWITCH' 27. FUEL QUANTITY GAGE 28.

10-10 Lynch removed aspirator, added ADB fillets, 11 ° cone, ,45UD. 10-10 Lynch none, broken microswitch on nose gear door. 10-10 Lynch removed vortex gen. from fus. and stabilizer. aborted-gear unsafe light flickering. 10-11 Lynch none, aborted-main gear door microswitch broke. 10-11 Lynch none, aborted-gear unsafe light on. 10-12 Lynch none, performance flight. 10-12 Lynch added vortex generators as on flight #46. 10-13 Baker none. 10-13 Darnell none. 10-15 Lynch replaced vortex gen. with 2"x25" vanes in same location.

Above, dual vortex generators fitted to the fuselage fillet saddle on 5-17-54. At left, dual short vortex generators were tried on 6-4-54. Below left, a single-row vortex generator was tried on 5-24-54. Below, the almost finalized vortex generator arrangement as tested during Phase III Stability and Control Tests. (all photos NAA via Bill Simone) Bottom, finalized vortex generator arrangement as utilized on all drag chute equipped F-86Ds. (Bob Stollof & USAF) 48 F-100 - STYLE LOW TAIL REAR Above, low-set horizontal tail on YF-86D, 50-577, also necessitated moving the speed brakes to the upper portion of the fuselage.

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