TM 1-1500-204-23-2
Table 4-44. Non-Applicability of MIL-H-83282
Aircraft
Application
Aircraft
Component
UH-1/H/M
Stabilizer Bar Dampers
AH-1 Series
Pylon Dampers
CH-47 C/D
Lag Dampers
Landing Gear Shock Struts
OV-1
Propellor Control System and Landing Gear
Pneudraulic Struts
OH-6
Landing Gear Struts
UH-60A
AH-64A
Landing Gear Shock Struts Brake System
Table 4-45. Operating Temperature Limitations of MIL-H-83282
Aircraft
Minimum temperature
UH-1
-30°F (-35°C)
OH-58
-25°F (-32°C)
CH-47
-50°F (-46°C)
OV-1
-40°F (-40°C)
AH-1
-50°F (-46°C)
AH-64
-25°F (-32°C)
UH-60A
-40°F (-40°C)
Servicing Equipment
D5A, D5B, D6
-20°F (-29 C)
MSU-1
-25°F (-29°C)
Change 2
4-169/(4-170 blank)
