Page 257 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 FIGURES

D. Downwind airspeed....................................................175 KIAS (PF)
ACAWS
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F. Final airspeed ....................................................................................
......................150 KIAS or Approach Speed (whichever is greater) (PF)
TAKEOFF
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G. Before Landing checklist................................................... Complete FIRE/SMK
NORM
H. Below 500 feet AGL.....................Slow toward threshold speed (PF)
PRES/OXY
NOT FOR FLIGHT
Once committed to land at 500 feet, slow toward threshold speed
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if available, to shorten the landing distance, but it can make lateral ENG/PROP
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light weight, power may have to be removed immediately at 500 FUEL
feet to slow down in time. Set rudder trim to zero when a power
increase before touchdown is no longer necessary.
AAR
I. Rudder trim.......................................Center, prior to touchdown (PF)
SPEC J. Brakes and nose wheel steering............................... As required (P) ELEC

WARNING
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Two-engine out landings result in long landing distances
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propeller drag in the ground range. Also, with the utility
hydraulic system inoperative, no anti-skid or nose wheel
steering is available. GEAR

CAUTION
DOR/RMP
PERF ‡ If both No. 1 and No. 2 propellers are feathered, nose
wheel steering is not available. Use differential power
and braking for directional control. Because normal and JETTISON
anti-skid braking is not available, any braking before the
aircraft slows 30 KIAS below touchdown speed may
cause tires to fail. LANDING

‡ Observe the 139 knot ground speed limit on the nose
tires, and the limit of 145 KTAS for moving the power DITCHING
levers below FLT IDLE.

NOTE BAILOUT

If anti-skid braking is available, heavy braking and nose
OPER wheel steering greatly increase directional control. FAULT LG

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