TM 1-1510-223-10 Change 3          9-3 setting that allows for normal torque increase during the takeoff roll and the ensuring climb. The static power is de- termined so that at some point during the climb to 500 feet, the torque or TGT will reach red line. (The TGT limit will only be reached on a minimum performance engine. A better than minimum engine will exhibit a positive TGT margin under these conditions.) Setting of a static power greater than that presented in Chapter 7 will result in an engine limit being exceeded prior to the aircraft reaching 500  feet,  necessitating  an  unscheduled  power  adjust- ment. Setting of a static power less than that presented in Chapter 7 will result in insufficient power available and failure of the aircraft to attain scheduled performance. 1.   Power — Maximum allowable. 2.   Gear — UP (two positive climb indications). 3.   Propeller — Verify feathered. 4.   Flaps — UP after V_enr (130 KIAS). 5.   Landing lights — OFF. 6.   Engine cleanup — Perform. 7.   Land as soon as practicable. NOTE Holding up to 5 degrees of bank and (1/2 ball width) toward the operating engine will assist in maintaining directional control and will improve aircraft performance. d.   Engine Malfunction During Flight. If an engine mal- functions during flight, perform the following: 1.   Autopilot/Yaw Damp — Disengage. 2.   Power — As required. 3.   Dead engine — Identify. 4.   POWER lever (dead engine) — IDLE. 5.   PROP lever (dead engine) — FEATHER. 6.   Gear — As required. 7.   Flaps — As required. 8.   Engine Cleanup — Perform. 9.   Power — Set for single engine cruise. 10.   Land as soon as practicable. e.   Engine Malfunction During Final Approach. If an engine malfunctions during final approach (after LAND- ING CHECK) the propeller should not be manually feath- ered unless time and altitude permit or conditions require it. Continue approach using the following procedure: 1.   Power — As required. 2.   Gear — DN. f.    Engine Malfunction (Second Engine). If the sec- ond  engine  fails,  the  airspeed  to  fly  will  depend  upon whether or not a restart will be attempted, and whether or not the restart attempt will be accomplished with or without starter assist. If no restart is to be attempted, use maximum glide speed from figure 9-2. Perform the fol- lowing procedure if the second engine fails during cruise flight. 1.   Airspeed — As required. 2.   POWER lever — IDLE. 3.   PROP lever — As required. 4.   Conduct engine restart procedure. 9-7. ENGINE SHUTDOWN IN FLIGHT. If it becomes necessary to shut an engine down dur- ing flight, perform the following: 1.   POWER lever — IDLE. 2.   PROP lever — FEATHER. 3.   CONDITION lever — FUEL CUTOFF. 4.   Engine cleanup — Perform. 9-8. ENGINE CLEANUP. The cleanup procedure to be used after engine mal- function, shutdown, or an unsuccessful restart is as fol- lows: 1.  CONDITION lever — FUEL CUTOFF. 2.  Engine AUTO IGNITION switch — Off. 3.  AUTOFEATHER switch — OFF. 4.  GENERATOR switch — OFF. 5.  Mission control switches — As required. 6.   PROP SYNC switch — OFF. 7.  BRAKE DEICE switch — Off. 9-9. ENGINE    RESTART    DURING    FLIGHT    (NO STARTER ASSIST). CAUTION The pilot should determine the reason for engine failure before attempting an airstart. Do not at- tempt an airstart if N₁ indicates zero.