TM 1-1520-238-T-7
11–33
11–3.
EQUIPMENT DATA
11–3
DASE Equipment (force required to break SPAD and activate
BUCS)
Pilot’s pitch SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 to 52 lbs.
Pilot’s roll SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 to 32 lbs.
Pilot’s yaw SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 54 to 103 lbs.
Pilot’s collective SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 to 56 lbs.
CPG’s pitch SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35 to 80 lbs.
CPG’s roll SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 to 38 lbs.
CPG’s yaw SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 to 120 lbs.
CPG’s collective SPAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32 to 66 lbs.
Stabilator Wing Dimensions
Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.7 feet
Width at tipcord . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6 feet
Width at rootcord . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.5 feet
11–4.
EQUIPMENT CONFIGURATION
11–4
DASE (ACB) excitation transformers are housed in a LRU with four filters. The filters provide electro-magnetic
interference (EMI) hardening for the DASEC.
11–5.
SAFETY, CARE AND HANDLING OF EQUIPMENT
11–5
Not applicable.
11–6.
CONTROLS AND INDICATORS
11–6
The flight control system receives mode selects and remote switch inputs from various controls located in the pilot
station (fig. 11–12) and CPG station (fig. 11–13). Table 11–1 provides a listing of the controls, switches and
associated indicators pertaining to the flight control system along with a description of their function.
