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FUEL PUMP AND XFEED CHECK
KIT1C is not installed or keyed

TM-1-1520-240-CL Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-CL P-8 5.  Remaining three AUX FUEL PUMP’s — Check as in step 4, except check R AUX PRESS light on, then off, for R AUX FUEL PUMP switches. 714A  FADEC  Reversionary  system  —  Check  First flight of the day. 1.  FADEC 1 and 2 PRI-REV switches — PRI. 2.  NR% switch — 100%. 3.  FADEC 1— Check as follows: a.   FADEC 1 PRI-REV switch — REV. b.   FADEC 1 INC - DEC switch — DEC. Check for decrease in No. 1 engine N1 and torque, and corresponding increase in No. 2 engine N1 and torque. c.   FADEC 1 INC - DEC switch — INC. Check for increase in No. 1 engine N1 and torque, and corresponding decrease in No. 2 engine N1 and torque. d.   FADEC 1 PRI-REV switch — PRI. 4.  Repeat check for FADEC 2. Transponder Check and Set. 1.  Move the MASTER switch from OFF to STBY. If the aircraft is so equipped, observe that the STBY light on the aircraft advisory panel comes on.  Also, note that the NO GO light is on. 2.  Allow 2 minutes for warmup. 3.  Select the codes assigned for use in modes 1 and   3/A   by   depressing   and   releasing   the pushbutton  for  each  switch  until  the  desired number shows. 4.  Operate  the  PRESS-TO-TEST  feature  of  the lamp indicators. 5.  Place the ANT switch BOT. 6.  Move   the   MASTER   switch   from   STBY   to NORM. 7.  Hold the M-11 switch to TEST, observe that the TEST/GO indicator lights.







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