TM 55-1520-228-10
occurs the processor generates the appropriate threat
symbology and synthetic audio. It is important therefore
that the correct theaterized EID and UDM are installed
for the mission or geographic location.
(3)
Symbol generation and position relative to
the center of the CRT shows the threat lethality, it does
not show or represent any liability of range, but of condi-
tion/mode of the emitter. Highest priority threats (most
lethal) are shown nearest the center. Each symbol de-
fines a generic threat type, symbols are modified to
show change in the status of the emitter. The symbols
are unclassified, the definitions of what the symbols
mean are classified. The complete set of symbols and
definitions are contained in TM 11-5841-294-30-2. Each
theaterized library EID has a specific classified pilot
kneeboard produced with it. The unit electronic warfare
officer (EWO) should contact PM-ASE if sufficient cards
are not available within his unit for the installed EID.
3-69. CONTROLS AND FUNCTIONS – RA-
DAR SIGNAL DETECTING SET (AN/
APR-39A(V)1).
3-70. OPERATING PROCEDURES – RA-
DAR SIGNAL DETECTING SET (AN/
APR-39A(V)1).
a. Self-Test Mode.
(1)
After power up, the AN/APR-39A(V)1 syn-
thetic voice will announce “APR-39 POWER UP” and
the (+) symbol will stabilize in the center of the CRT. Self
test should be initiated after approximately one minute.
Self test can be performed in MODE ONE or MODE
TWO. In MODE ONE the synthetic voice will announce
“SELF TEST SET VOLUME, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10,
11, 12”. In MODE TWO the synthetic voice will an-
nounce “SELF TEST SET VOLUME, 5, 4, 3, 2, 1”.
(2)
The CRT will display specific software ver-
sion numbers (i.e., operational flight program (OFP)) at
the 12 o’clock position and the emitter identification data
(EID) at the 6 o’clock position.
(3)
After the software version numbers have
been displayed the test sequence checks the receivers.
A good visual self test will show two triangles, one at the
6 o’clock and one at the 12 o’clock position on the CRT.
Snowflake symbols (*) will appear at the 2, 4, 8, and 10
o’clock positions and will flash if the AN/AVR-2 laser
detecting set is not installed. This is a normal indication
and does not effect system performance.
(4)
A good self test (no faults detected) ends
with the message “APR-39 OPERATIONAL”. A bad self
test (faults detected) ends with the “APR-39 FAILURE”.
b. MODE 1 Operation. Selecting MODE ONE the
operator will hear all the normal synthetic voice audio
when an emitter has been processed (e.g., the AN/
APR-39A(V)1 will announce; “SA, SA-18 12 O’CLOCK
TRACKING”). Selection of this mode does not have any
effect on emitters received, processed or displayed. It
only affects synthetic voice audio.
c. MODE 2 Operation. Selecting MODE TWO the
operator will hear an abbreviated synthetic voice audio
(e. g., the AN/APR-39A(V)1 will announce, “MISSILE 12
O’CLOCK TRACKING”).
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 ...
Page 221: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 7 of 13 7 69 ...
Page 222: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 8 of 13 7 70 ...
Page 223: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 9 of 13 7 71 ...
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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 ...