• Home
  • Download PDF
  • Order CD-ROM
  • Order in Print
b. 714A  Autorotation RRPM Check
BEFORE LANDING - TM-1-1520-240-MTF_97

TM-1-1520-240-MTF Army Model CH-47D Heilcopter (EIC:RCD) Manual
Page Navigation
  84    85    86    87    88  89  90    91    92    93    94  
TM 1-1520-240-MTF 2-85 IN-FLIGHT (CONT.) (5)   Accomplish  Power  Recovery  prior  to 1000’ AGL. (a) Load Rotor by relaxing pressure on Thrust Control Lever allowing it to come  up  as  required  if  RRPM  is above 100%. (b) FADEC  NR%  rheostat  —  100% position. (c) Reestablish   100%   RRPM,   safe airspeed, and altitude. (d) Climb  back  to  altitude  where  PA was noted and record following: 1    Free Air Temperature. 2    Fuel Quantity. (e) Record  previously  noted:  RRPM. PA, Pedal Separation, and Unusual Vibrations (as applicable). (6)   Compare data to chart in Section V for proper RRPM. Ensure conversion from PA and FAT to DA. 13.    712   Engine TEAC check, if required. (Refer to Section IV.) 14.    714A    Power  Assurance  Check,  if  required. (Refer to Section IV.) 15.  Fuel consumption check — STOP. 16.  Navigation    and    Communication.    (Refer    to Section IV.) 17.  Miscellaneous (as required). a.   Vertical velocity indicators b.   Turn and slip indicators.







Western Governors University

Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved. Design by Strategico.