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TM 55-1520-228-10
switch (figure 2-19) controls the brightness of the cau-
tion panel lights and the MASTER CAUTION light. The
INST LTS switch must be moved from the DIM position
before the caution panel lights can be dimmed. The
system is so designed that after each initial application
of power, the lamps will illuminate in the bright condition.
c. Warning System. The warning system consists
of five individually illuminated warning light segments
mounted in the MASTER CAUTION and warning light
panel (figure 2-19) on the instrument panel. The pur-
pose of this system is to provide visual indication for day
or night operation that any of the five conditions or com-
binations thereof has occurred. Each fault condition as
it occurs is indicated by a steady illumination of the let-
tering on the particular segment. In addition, an audio
signal sounds when the ENGINE OUT or ROTOR RPM
segment is illuminated and the collective pitch is not in
the full down position. The warning indicator segment
remains illuminated until the fault condition is corrected.
ENGINE OUT
Engine N1 speed below
55
$
3%
XMSN OIL PRESS
Transmission oil pressure
below 30
$
2 psi
XMSN OIL HOT
Transmission above
110
_
C
ROTOR RPM
Rotor rpm below 95%
$
1.4%
MASTER CAUTION
Fault condition in caution
panel
The WARNING LTS TEST switch (figure 2-13 and figure
2-14) is pressed to check for illumination of all the warn-
ing lights.
SECTION XIV. SERVICING, PARKING, AND MOORING
2-73. SERVICING.
a. Servicing Diagram. Refer to figure 2-20 and fig-
b. Fuels, Oils, Fluids, Specifications, and Ca-
pacities. Refer to table 2-1.
2-74. APPROVED FUELS, OILS, AND
FLUIDS.
a. Fuels. Refer to table 2-2.
b. Oils. Refer to table 2
c. Fluids. Refer to table 2-4.
2-75. FUEL TYPES.
a. JP-4. This fuel contains icing inhibitor lended at
the refinery. Commercial Jet B is a JP-4 type fuel; its
mixture may or may not contain icing inhibitors.
b. JP-5 and JP-8. These fuels contain icing inhibi-
tors blended at the refinery. Jet A and Jet A1 are JP-5
type fuels without icing inhibitors.
c. Emergency Fuel. Aviation gasolines
(MIL-G-
(
5572)
without Tricresyl Phosphate (TCP) are
desig-
nated as the emergency fuels to be used in this
air-
craft.
2-76. USE OF FUELS.
a. JP-4. There is no special limitation on the use of
JP-4 fuel, but limitations are imposed when fuels other
than JP-4 are used.
b. JP-5, JP-8, Jet A, and Jet A1. These fuels may
be added to JP-4 and to each other in any quantities.
c. Emergency Fuels. Aviation gasoline may also
be added to turbine engine fuels in any quantity. Fuel
mixtures containing any amount of Aviation Gasoline
must be recorded in the Remark Section of DA Form
2408-13-1 as an emergency fuel, noting the type of fuel,
additives, and duration of operation. The 6 hour total
engine operation limitation applies.
d.
Refer to fuel operation limits, Chapter 5, when
fuels other than JP-4 are used.
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Страница 57: ...TM 55 1520 228 10 Figure 2 8 Locking Devices for Doors 2 15 ...
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Страница 62: ...TM 55 1520 228 10 2 20 Change 11 Figure 2 11 Engine ...
Страница 64: ...TM 55 1520 228 10 Figure 2 12 Overhead Console 2 22 Change 10 ...
Страница 65: ...TM 55 1520 228 10 Figure 2 12 1 Overhead Console with AN ARC 201 Typical Change 10 2 22 1 2 22 2 blank ...
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Страница 70: ...TM 55 1520 228 10 2 26 Change 11 Figure 2 14 Instrument Panel and Console Typical C ...
Страница 71: ...TM 55 1520 228 10 Figure 2 14 1 Instrument Panel and Console with AN ARC 201 A Typical Change 10 2 26 1 ...
Страница 75: ...TM 55 1520 228 10 Figure 2 15 Auxiliary Fuel System 2 29 ...
Страница 84: ...TM 55 1520 228 10 Figure 2 17 Heater Control and Vent Pull Knobs 2 38 Change 12 ...
Страница 92: ...TM 55 1520 228 10 Figure 2 18 1 AAU 32 A Altitude Encode Pneumatic Altimeter 2 46 Change 4 ...
Страница 95: ...TM 55 1520 228 10 Change 11 2 47 Figure 2 19 Warning and Caution Panels ...
Страница 98: ...TM 55 1520 228 10 Figure 2 20 Servicing Diagram Sheet 2of 2 2 50 Change 11 ...
Страница 107: ...TM 55 1520 228 10 Figure 2 22 Gravity Refueling With Closed Circuit Receiver 2 59 ...
Страница 109: ...TM 55 1520 228 10 Change 11 2 61 Figure 2 23 Refueling Receptacle ...
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Страница 229: ...TM 55 1520 228 10 DRAG CALIBRATED TORQUE Q Figure 7 16 Drag Chart Change 10 7 77 DRAG OH 58A C T63 A 720 ...
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Страница 259: ...Figure 9 1 Emergency Exits and Equipment Sheet 1 of 2 Change 14 9 3 TM 55 1520 228 10 ...
Страница 260: ...Figure 9 1 Emergency Exits and Equipment Sheet 2 of 2 9 4 Change 14 TM 55 1520 228 10 ...
Страница 261: ...Figure 9 2 Autorotational Glide Characteristics Chart Change 14 9 5 TM 55 1520 228 10 ...
Страница 262: ...Figure 9 3 Minimum Height for Safe Landing After Engine Failure Chart 9 6 Change 14 TM 55 1520 228 10 ...
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Страница 292: ...PIN 014142 000 ...