TM 1-1510-253-CL
SINGLE ENGINE LANDING
NOTE
Compute single engine landing dis-
tance by adding 66% to two engine
landing distance.
Turn engine anti-ice and/or bleed air off
as required to achieve single engine
go-around performance.
1. LANDING GEAR Handle -- RECHECK
DOWN
2. FLAPS -- CHECK Final Setting
SINGLE ENGINE GO AROUND
1. WATER INJECTION Switch -- SET As
Required
2. POWER -- SET Max Allowable
3. FLAPS -- SET 1/4
4. LANDING GEAR Handle -- UP
5. FLAPS (VREF + 5 KIAS & 500' AGL
Minimum) -- UP
6. Airspeed -- VYSE Minimum
7. WATER INJECTION Switch -- OFF
8. Exterior Lights -- SET As Required
O 9. CMWS -- SELECT ARM
NO RESPONSE TO POWER LEVER
MOVEMENT
NOTE
If either/both engine(s) exhibit a lack of
response to power lever after extended
operations at high altitude with OAT be-
low freezing, cause may be ice blockage
of P2T2 inlet sensor probe, the following
procedure should be accomplished and
normal power lever response should re-
turn within approximately 3 minutes.
E-6
