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Figure  5-5-2.  Airspeed Limitations Longitudinal Cyclic Trim Retracted
SECTION  VII.  ENVIRONMENTAL RESTRICTIONS

TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-10            5-6-1/(5-6-2 blank) SECTION  VI.  MANEUVERING LIMITS 5-6-1.  Aerobatics Prohibition Aerobatics are prohibited with this helicopter. Aerobatics is defined as intentional maneuvers beyond + 30_ pitch and/or 60_ roll. 5-6-2.  Bank Limitations The following bank angle limits apply: a. With  an  operative  cruise  guide  indicator,  bank angles are limited by the cruise guide indicator, but no greater than 60 degrees. When operating with altitude hold, limit bank angle limits to 45 degrees maximum. b. With an inoperative cruise guide indicator, use the bank angle limits defined by fig. 5-6-1. 5-6-3.   Landing Limitations. a. The maximum ground speed for running land- ings is 60 knots. b. The maximum nose–up attitude during landings is 20º. 5-6-4.  Ground Operation Limitations. a. To  prevent  droop  stop  pounding,  when  all  the landing  gears  are  in  contact  with  the  ground  and  the thrust is at ground detent flight control movements shall not exceed the floowong from the neutral position: Right or left directional pedal .75 inches Aft cyclic 2.00 inches Lateral cyclic 1.00 inches Thrust No lower than ground detent b. When ground taxiing less than 75 feet from an obstruction,  on  an  unimproved/unfamiliar  airfield  not designated for CH-47D helicopters, a blade watcher and taxi director shall be positioned as shown in figure 8-2-1. If the airfield is designated for CH-47D helicopter and taxi ways are in accordance with UFC 3-260-01, the above does not apply. Figure  5-6-1.  Bank Angle Limitations







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