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4-1-37.  Adjustment  of  Barometric  Altitude,  Pitch, and Roll.
SECTION  II.  ARMAMENT

TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
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TM  1-1520-240-10 4-1-26            WARNING Do not attempt to egress the aircraft with- out performing disconnect as this may re- sult in neck injury. CAUTION Do not disconnect DU by pulling on the cable. To do so may damage the DU. 3.   Display Unit — Disconnect. Disconnect DU by   gasping   the   PSCU   and   rotating   the quick-release connector engagement ring and pull downward. Remove OU by loosen- ing  thumbscrew  on  OU  and  remove  OU from the ANVIS and place into protective storage case. 4.   Reattach neck cord to ANVIS. 4-1-40.  Emergency Egress. The quick-release feature allows you to exit quickly from the aircraft in an emergency without: a. Damaging or turning the unit off. b. Getting tangled in cords. c. Being restrained in the cockpit by hardwired con- nections. d. Removing ANVIS. It is up to the operator to determine the desired mode of disconnect based upon his evaluation of the emergency condition and whether or not the ANVIS goggles will be needed following egress. The available means of discon- nect are as follows. e. Release the ANVIS goggles from the helmet. f. Disconnect the OU from the ANVIS goggles via the thumbscrew. g. For routine disconnect, take hold of PSCU and rotate the quick-release connector engagement ring and pull downward. h. For emergency disconnect, take hold of PSCU pull down.







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