This transcription has been completed. Contact us with corrections.
[[preprinted]] 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.]] 67 [[/preprinted]]