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Section I. GENERAL
Up
TB-55-1500-334-25 Conversion of Aircraft to Fire Resistant Hydraulic Fluid Manual
Next
Availability of MIL-H-83282.
TB 55-1500-334-25
Section II. INITIAL CONVERSION OF HYDRAULIC SYSTEMS
AIRCRAFT
APPLICATION
2-1 Applications of MIL-H-83282.
CH-54A
First  Stage  Hydraulic  System,
The fire hazards of MIL-H-5606 are greatest in light
Second  Stage  Hydraulic  System
control systems which are under high pressure and which
Utility Hydraulic System Cargo Hoist
have a relatively large volume of fluid. At the present
Hydraulic System
time, only the following aircraft hydraulic systems and
CH-54B
First Stage Hydraulic System Second
components will be converted from MIL-H-5606 to MIL-H-
Stage  Hydraulic  System  Utility
83282.
Hydraulic System
AIRCRAFT
APPLICATION
NOTE
OH-58A
Flight Control System
UH-18B/D/H
Flight Control System Armament
CH-54B aircraft based in Alaska will
System M6 Additional Armament
retain MIL-H-5606.  All CONUS based
Systems for UH-IB, M16 and M21
CH-54 aircraft will be converted to MI L-
UH-IC/M
Hydraulic Systems No. 1and 2
H-83282.
Armament System M6, 16, 21
AH-1 Series
Hydraulic Systems No. 1 and 2
Servicing
Armament Turret System
Equipment
CH-47 A/B/C
Flight Control Systems No. 1 and 2
Utility Hydraulic System
AF5, D5
Hydraulic dispensers and
OV-l
Main Hydraulic System
Series,
test stands will be converted
UH-60A
Hydraulic Systems No. 1, 2, and 3
D6
to MIL-H-83282 to provide
MSU-I
ground support to aircraft converted
to MIL-H-83282.
2-2 Non-Applicability of MIL-H-83282.
limitations in Section III are exceeded, field personnel will
The following components will retain MIL-
be unable to change these components from MIL-H-
H5606 hydraulic fluid.  These components cannot be
83282 back to Ml IL-H-5606.
readily serviced by field personnel or have not been
tested for MIL-H-83282. In the event that the temperature
AIRCRAFT
COMPONENT
UH-1 B/C/D/H/M
Stabilizer-bar dampers
AH-1 Series
Pylon dampers
CH-47 A/B/C
Lag dampeners Landing gear shock struts
OV-1
Propeller control system and landing gear pneudraulic struts
CH-54A/B
Landing Gear Shock Struts
Rotor Brake System
Main Rotor Blade Damper System
NOTE
CH-54B aircraft based in Alaska will retain MIL-H-5606. All CONUS based CH-54 aircraft will be
converted to MIL-H-83282.
OH-6
Landing Gear Dampers Uni-lock
UH-60A
Landing Gear Struts, Wheel Brake System, Main Rotor Dampers
Change 6
2-1

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