NET TAKE-OFF FLIGHT PATH - FIRST SEGMENT - FLAPS APPROACH ONE ENGINE INOPERATIVE

ACCELERATE-GO - FLAPS APPROACH OVER 50-FOOT OBSTACLE

NET TAKE-OFF FLIGHT PATH - SECOND SEGMENT - FLAPS APPROACH ONE ENGINE INOPERATIVE

TM-1-1510-223-10 Army RC-12 Aircraft Manual
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TM 1-1510-223-10 NET TAKE-OFF FLIGHT PATH - FIRST SEGMENT - FLAPS APPROACH ONE ENGINE INOPERATIVE ASSOCIATED CONDITIONS: POWER ..........................STATIC TAKE-OFF POWER SET BEFORE BRAKE RELEASE INOPERATIVE PROPELLER .............FEATHERED LANDING GEAR ................................DOWN CLIMB SPEED....................................V2 NOTE: FOR OPERATION WITH ICE VANES EXTENDED, DECREASE NET CLIMB GRADIENT BY 1.0 PERCENTAGE POINT. EXAMPLE: FAT ................................................................15C FIELD PRESSURE ALTITUDE ......................3499 FT WEIGHT .........................................................16,000 LBS HEADWIND COMPONENT ............................10 KTS NET CUMB GRADIENT .................................0.00 % * CA Decrease net climb gradient by 0.1 percentage points. Figure 7-31. Net Take-off Flight Path - First Segment - Flaps Approach IR 7-42 Change 2

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