Figure 7A-37. Climb - One Engine Inoperative

Figure 7A-36. Climb - Two Engines - Flaps Approach

Figure 7A-38. Service Ceiling - One Engine Inoperative

TM-1-1510-224-10 Army RC-12P Aircraft and Army RC-12Q Aircraft Manual
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TM 1-1510-224-10 CLIMB - ONE ENGINE INOPERATIVE ASSOCIATED CONDITIONS: POWER...................................................MAXIMUM CONTINUOUS FLAPS.....................................................UP LANDING GEAR.....................................UP INOPERATIVE PROPELLER..................FEATHERED CLIMB SPEED........................................VYSE EXAMPLE: FAT.................................................................-4C PRESSURE ALTITUDE..................................9000 FT WEIGHT..........................................................15,500 LBS RATE-OF-CLIMB ............................................358 FT/MIN CLIMB GRADIENT..........................................2.0 %. Figure 7A-37. Climb - One Engine Inoperative 7A-55

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