TM 1-1510-224-10
CLIMB - TWO ENGINES - FLAPS APPROACH
ASSOCIATED CONDITIONS
POWER...................................................MAXIMUM CONTINUOUS
LANDING GEAR.....................................UP
EXAMPLE:
FAT.................................................................-4C
PRESSURE ALTITUDE..................................9000 FT
WEIGHT..........................................................15,500 LBS
RATE-OF-CLIMB ............................................2053 FT/MIN
CLIMB GRADIENT..........................................10.7 %
Figure 7A-36. Climb - Two Engines - Flaps Approach
7A-54
