Figure 7-9.  Take-Off Weight - Flaps 0%, To Achieve Positive One-Engine Inoperative Climb at Lift-Off
Figure 7-11.  Wind Components

TM-55-1510-219-10 Army Aviation Maintenance Engineering Manual Weight and Balance
Page Navigation
  222    223    224    225    226  227  228    229    230    231    232  

Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved.

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business