TM 55-1520-228-10
Change 11 3-32.1
3-67.4
. OPERATING PROCEDURES –
RADAR ALTIMETER.
NOTE
Refer to TM 11-5841-284-23&P for
additional operating instructions. Partic-
ular attention shall be given to “Obstacle
Avoidance” as follows: The altimeter
system tracks the terrain below the air-
craft and, therefore, will not provide use-
ful information to aid in obstacle
avoidance. By the time a sufficient area
of an obstacle is within the antenna
beams so the altimeter set can display
the near object, the aircraft probably
could not be maneuvered to avoid the
object.
a. Altimeter Operation.
(1)
LO SET control knob – Rotate clockwise
from OFF. Set low limit index as desired.
(2)
HI SET control knob – Set high limit index as
desired.
b. Self Test Operation.
(1)
Lower right knob – Press. The pointer and
digital display should read 1000 feet (
$
100). Also, the
HI indicator on the radar altimeter should be illuminated.
Release the knob. The reading should extinguish.
(2)
Lower left knob – Adjust clockwise until the
LO bug is positioned “above” (greater in altitude than)
the pointer. A periodic audio warning “ALTITUDE LOW-
TOO-LOW” should be heard in all headsets. Also, the
LO indicator on the radar altimeter should be illumi-
nated.
(3)
Master ICS volume control – Rotate on each
respective ICS unit. The audio warning volume should
fluctuate. The audio warning volume level can also be
altered by momentarily pressing the Push-To-Test
(PTT) knob (lower-right) on the radar altimeter itself af-
ter the voice warning has been initiated. Depress the
PTT knob once. The audio warning volume should be
1/2 the initial level. Depress the PT knob a second time.
the audio warning message should be disabled. Once
the volume level is reduced 1/2 initial level, the audio
warning volume level cannot be changed (except by
adjusting the master ICS volume control) or once dis-
abled it cannot be brought back.
(4)
Lower left knob – Adjust counterclockwise
until the LO bug is “below” the pointer, then adjust the
knob clockwise until the LO bug is positioned “above”
the pointer again. The “ALTITUDE LOW - TOO LOW”
audio warning should be again heard at its initial “FULL”
volume level.
(5)
Lower knob – Adjust counterclockwise until
the LO bug is “below” the pointer, (but not quite to the
OFF position). The warning audio should cease. The LO
indicator should be extinguished.
(6)
Lower right knob – Depress and hold to put
the Radar Altimeter into the test mode. A periodic “ALTI-
TUDE HIGH-CHECK ALTITUDE” should be heard in all
headsets. Also, the HI indicator on the radar altimeter
should be illuminated.
(7)
Push-To-Test knob – Release. The warning
audio message should cease. The HI indicator should
be extinguished.
c. Stopping Procedure. LO SET control knob –
Rotate counterclockwise from LO.
3-68. RADAR SIGNAL DETECTING SET
(AN/APR-39A(V)1).
Refer to TM 11-5841-294-12.
3-68.1
. DESCRIPTION – RADAR SIG-
NAL DETECTING SET (AN/
APR-39A(V)1).
a. Description. The radar signal detecting set AN/
APR-39A(V)1 provides the pilot with visual and audible
warning when a hostile fire control threat is encoun-
tered. The equipment responds to hostile fire-control
radars but non-threat radars are generally excluded.
The equipment also receives missile guidance radar
signals and, when the signals are time-coincident with
a radar tracking signal, the equipment identifies the
combination as an activated hostile surface-to-air mis-
sile (SAM) radar system. The visual and aural displays
warn the pilot of potential threat so that evasive maneu-
vers can be initiated.
b. Function.
(1)
The AN/APR-39A(V)1 receives, processes
and displays pulse type signals operating in the C-D and
H-M radio frequency bands. The emitters that it pro-
cesses and displays are derived from the emitter identi-
fication data (EID) contained in the user data module
(UDM) that is inserted in the top of the digital processor.
In normal circumstances the processor is classified con-
fidential if a classified UDM is installed.
(2)
The UDM contains the electronic warfare
threat data that makes up the specific library for a specif-
ic mission(s) or a geographical location (it is theater-
ized). When a match of the electronic warfare data
Summary of Contents for OH-58A
Page 2: ......
Page 5: ......
Page 6: ......
Page 10: ......
Page 12: ......
Page 18: ......
Page 19: ......
Page 20: ......
Page 21: ......
Page 22: ......
Page 23: ......
Page 24: ......
Page 26: ......
Page 28: ......
Page 30: ......
Page 32: ......
Page 34: ......
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 ...
Page 66: ......
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 ...
Page 116: ......
Page 133: ...TM 55 1520 228 10 Change 11 3 13 FIGURE 3 7 HAS BEEN DELETED ...
Page 146: ......
Page 152: ...TM 55 1520 228 10 FIGURE 3 15 HAS BEEN DELETED 3 30 Change 10 ...
Page 157: ...TM 55 1520 228 10 3 32 3 ...
Page 164: ......
Page 166: ......
Page 168: ...TM 55 1520 228 10 Figure 5 1 Instrument Markings A 5 2 Change 11 ...
Page 169: ......
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 ...
Page 186: ......
Page 187: ......
Page 188: ......
Page 190: ......
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 ...
Page 209: ......
Page 210: ......
Page 211: ...TM 55 1520 228 10 Change 10 7 59 Figure 7 13 Hover Chart Sheet 3 of 3 ...
Page 213: ......
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 ...
Page 224: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 10 of 13 7 72 ...
Page 225: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 11 of 13 7 73 ...
Page 226: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 12 of 13 7 74 ...
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 ...
Page 233: ......
Page 234: ......
Page 235: ......
Page 237: ...TM 55 1520 228 10 Figure 7 19 Idle Fuel Flow Chart 7 85 7 86 blank ...
Page 238: ......
Page 242: ...TM 55 1520 228 10 8 4 Change 10 Figure 8 1 Exterior Check Diagram ...
Page 256: ......
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 ...
Page 270: ......
Page 282: ......
Page 284: ......
Page 286: ......
Page 292: ...PIN 014142 000 ...