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APPENDIX A  MANUAL 51 - 11

42. Normally, what is the first indication when approaching a critical high speed? What are recovery procedures?
^[[Aileron buzz. Speed brakes]]

43. What is the stall speed of the aircraft (weight 12,000 lbs) with full flaps, gear down, no bank at idle power?
^[[95 Kts.]]

44. List the steps for normal spin recovery.
^[[Throttle - Idle ailerons neutral Stick aft. Retract gear flaps. Rudder against spin, then neutral. Stock forward after rotation has stopped & nose is well down.]]

45. Should the leading edge and main wing booster pumps be turned "OFF" when the respective tanks become empty? Why?
^[[Yes. No more fuel to lubricate pumps.]]

46. If the emergency fuel system selector switch is in the "TAKE OFF AND LAND" position, when will be emergency system be actuated?
^[[When NORMAL system pressure drops below certain limits. 35 PSI]]

47. List the normal sequence of fuel tank use.
^[[Tips, Mwg, L. E. Fus Locally?]]

48. List the minimum time between landings when excessive brake use has been necessary.
^[[15 min if gear is in slipstream]]
^[[30 " " " " [[dittos for min if gear is in]] retracted]]

49. What angle of bank is used in the penetration turn during a typical ADF letdown?
^[[30 [[degree symbol]] ]]

50. What danger exists in landing with structural ice?
^Increased stalling speeds. Sluggish acft control.]]

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