TM 55-1520-228-10
Change 11 3-5
SECTION I. COMMUNICATIONS
3-6. COMMUNICATIONS SYSTEM CON-
TROL, C-6533/ARC.
3-7. DESCRIPTION – COMMUNICATIONS
SYSTEM CONTROL.
The communications system control, C-6533/ARC (fig-
ure 3-2) provides an intercommunicates capability and
control of radio communications. Two of the control pan-
els are installed on the instrument panel, one each for
the pilot is installed on the right side overhead in the
passenger compartment. The control panels may be
used in any one of three different modes as determined
by the setting of switches and controls on the panel.
3-8. CONTROLS AND FUNCTIONS – COM-
MUNICATIONS SYSTEM CONTROL.
3-9. OPERATING PROCEDURES – COM-
MUNICATIONS SYSTEM CONTROL.
a. Modes of Operation. The three modes of op-
eration are two-way radio communication, radio receiv-
er monitoring, and intercommunications within the
helicopter.
b. Operation.
(1)
Receiver switches - As desired.
(2)
VOLume control - Adjust.
(3)
HOT MIKE switch - As desired.
(4)
Transmit-Interphone Selector - As required.
3-10. VHF/FM RADIO SET.
3-11. DESCRIPTION – VHF/FM RADIO
SET.
The AN/ARC-114 and AN/ARC-114A radio sets provide
two-way frequency modulated (FM) narrow band voice
communications and homing capability (Number one
unit only) within frequency range of 30.00 to 75.95 MHz
on 920 channels for a 50-mile distance as limited by line
of sight. A guard receiver incorporated in the set is fixed
tuned to 40.50 MHz. Retransmission of voice, CW or
X-mode communications is possible when a second set
is installed in the helicopter. The radio sets are marked
VHF/FM COMM and are installed in the center console.
Antenna location is located as shown in figure 3-1.
3-12. CONTROLS AND FUNCTIONS – VHF/
FM RADIO SET.
NOTE
When transmitting and/or receiving on
VHF (FM) in secure mode, do not key or
transmit simultaneously on any other
transmitter.
3-13. OPERATING PROCEDURES – VHF/
FM RADIO SET.
a. Transmit/Receive.
(1)
Function selector - As desired.
(2)
Frequency - Select.
(3)
RCVR TEST - Press to test.
(4)
AUDIO - Adjust.
(5)
Transmit.
(a)
Transmit-Interphone selector - Number
1 position (Number 5 position for second FM set).
(b)
RADIO transmit switch - Press.
b. Homing.
NOTE
FM homing capability is not provided for
ATAS equipped helicopters.
(1)
Function selector - HOMING.
(2)
AUDIO - Adjust.
(3)
Observe homing indications on the radio
bearing heading indicator.
c. Retransmission.
NOTE
Crew transmission may also be made
while in RETRAN mode.
(1)
Frequencies - Select (Both FM sets).
NOTE
Frequencies must have a minimum of
five MHz difference, such as 30.00 MHz
and 35.00 MHz.
(2)
Communications - Establish with each facili-
ty by selecting number 1 position and then number 5
position on the Transmit-Interphone selector.
Summary of Contents for OH-58A
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Page 53: ...TM 55 1520 228 10 Change 13 2 11 Figure 2 5 Principal Dimensions Sheet 1 of 2 ...
Page 56: ...TM 55 1520 228 10 Figure 2 7 Float Gear Equipped Helicopter 2 14 ...
Page 57: ...TM 55 1520 228 10 Figure 2 8 Locking Devices for Doors 2 15 ...
Page 59: ...TM 55 1520 228 10 2 17 Figure 2 9 WSPS Configuration ...
Page 61: ...TM 55 1520 228 10 Change 11 2 19 FIGURE 2 10 HAS BEEN DELETED ...
Page 62: ...TM 55 1520 228 10 2 20 Change 11 Figure 2 11 Engine ...
Page 64: ...TM 55 1520 228 10 Figure 2 12 Overhead Console 2 22 Change 10 ...
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Page 69: ...TM 55 1520 228 10 2 25 Figure 2 13 Instrument Panel and Console Typical A ...
Page 70: ...TM 55 1520 228 10 2 26 Change 11 Figure 2 14 Instrument Panel and Console Typical C ...
Page 75: ...TM 55 1520 228 10 Figure 2 15 Auxiliary Fuel System 2 29 ...
Page 84: ...TM 55 1520 228 10 Figure 2 17 Heater Control and Vent Pull Knobs 2 38 Change 12 ...
Page 92: ...TM 55 1520 228 10 Figure 2 18 1 AAU 32 A Altitude Encode Pneumatic Altimeter 2 46 Change 4 ...
Page 95: ...TM 55 1520 228 10 Change 11 2 47 Figure 2 19 Warning and Caution Panels ...
Page 98: ...TM 55 1520 228 10 Figure 2 20 Servicing Diagram Sheet 2of 2 2 50 Change 11 ...
Page 107: ...TM 55 1520 228 10 Figure 2 22 Gravity Refueling With Closed Circuit Receiver 2 59 ...
Page 109: ...TM 55 1520 228 10 Change 11 2 61 Figure 2 23 Refueling Receptacle ...
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Page 168: ...TM 55 1520 228 10 Figure 5 1 Instrument Markings A 5 2 Change 11 ...
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Page 170: ...TM 55 1520 228 10 Figure 5 2 Instrument Markings Sheet 1 of 3 5 3 blank 5 4 Change 14 ...
Page 171: ...TM 55 1520 228 10 Change 11 5 5 Figure 5 2 Instrument Markings Sheet 2 of 3 ...
Page 175: ...TM 55 1520 228 10 Change 11 5 9 T63 A 720 Figure 5 3 Airspeed Operating Limits Chart ...
Page 182: ...TM 55 1520 228 10 6 4 Change 10 Figure 6 3 Cargo Space ...
Page 183: ...TM 55 1520 228 10 Change 11 6 5 Figure 6 4 Fuel Loading Chart ...
Page 184: ...TM 55 1520 228 10 6 6 Figure 6 5 Personnel Loading ...
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Page 204: ...TM 55 1520 228 10 Figure 7 12 Torque Available Continuous Operation Chart Sheet 1 of 4 7 52 ...
Page 205: ...TM 55 1520 228 10 Figure 7 12 Torque Available Continuous Operation Chart Sheet 2 of 4 7 53 ...
Page 206: ...TM 55 1520 228 10 Figure 7 12 Torque Available Continuous Operation Chart Sheet 3 of 4 7 54 ...
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Page 211: ...TM 55 1520 228 10 Change 10 7 59 Figure 7 13 Hover Chart Sheet 3 of 3 ...
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Page 215: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 1 of 13 7 63 ...
Page 216: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 2 of 13 7 64 ...
Page 217: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 3 of 13 7 65 ...
Page 218: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 4 of 13 7 66 ...
Page 219: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 5 of 13 7 67 ...
Page 220: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 6 of 13 7 68 ...
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Page 227: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 13 of 13 7 75 ...
Page 231: ...TM 55 1520 228 10 7 79 Figure 7 17 Climb Descent Chart C ...
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Page 237: ...TM 55 1520 228 10 Figure 7 19 Idle Fuel Flow Chart 7 85 7 86 blank ...
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Page 242: ...TM 55 1520 228 10 8 4 Change 10 Figure 8 1 Exterior Check Diagram ...
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Page 259: ...Figure 9 1 Emergency Exits and Equipment Sheet 1 of 2 Change 14 9 3 TM 55 1520 228 10 ...
Page 260: ...Figure 9 1 Emergency Exits and Equipment Sheet 2 of 2 9 4 Change 14 TM 55 1520 228 10 ...
Page 261: ...Figure 9 2 Autorotational Glide Characteristics Chart Change 14 9 5 TM 55 1520 228 10 ...
Page 268: ...SECTION II MISSION EQUIPMENT NOT APPLICABLE 9 12 Change 14 TM 55 1520 228 10 ...
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Page 292: ...PIN 014142 000 ...