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Figure 3–11. Wheel Brake Assembly and Brake Disc | Up
TM-1-1520-238-T-4 Army Model AH-64 Helicopter (NSN
1520-01-106-9519) (EIC: RHA) Manual | Next
Table 3–1. Landing Gear System Controls and Indicators |
TM 1-1520-238-T-4
3–12
3–3.
EQUIPMENT DATA
3–3
MLG
Helicopter turning radius . . . . . . . . . . . . . . . . . . . . . . . . . . 37 ft. 6 inches
MLG shock strut hydraulic fluid capacity . . . . . . . . . . . . . 3.8 U.S. qts.
MLG shock strut weight . . . . . . . . . . . . . . . . . . . . . . . . . . . 42.9 lbs.
Tire (MLG) type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 ply tubeless
Tire (MLG) size . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.5x10 inches
TLG
Tail wheel lock relay (electrical requirements) . . . . . . . . 28 VDC
Wheel width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.75 inches
Wheel diameter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.50 inches
Tire (TLG) type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 ply tubeless
MLG Brake System
Gross weight capability . . . . . . . . . . . . . . . . . . . . . . . . . . . 17,650 lbs.
Master cylinder weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 lb.
3–4.
EQUIPMENT CONFIGURATION
3–4
Not applicable.
3–5.
SAFETY, CARE AND HANDLING OF EQUIPMENT
3–5
a. Tires must be deflated before wheel removal. Pressure on loosened nuts can result in separation of wheel
halves.
b. Wheels must be chocked before system maintenance.
c. Shock strut system contains high pressure nitrogen. Strut must be bled off prior to system servicing.
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