TM 55-1520-228-10
SECTION XII.
LIGHTING
2-51.
POSITION LIGHTS.
The position lights consist of three lights (figure 2-1 and
figure 2-2). A green light is located on the right horizon-
tal stabilizer tip, a red light on the left horizontal stabilizer
tip, and a white light on the aft end of the tailboom. Elec-
trical power is supplied from the 28-volt DC non-essen-
tial bus. Circuit protection is provided by the POS LTS
circuit breaker on the overhead console. The position
lights are controlled by the POS LTS switch on the over-
head console (figure 2-12). The switch is a three-posi-
tion toggle switch with BRT (forward) DIM (center) and
OFF (aft) positions.
2-52.
NVG POSITION LIGHTS.
Five, white IR position lights (NVG position lights) are
mounted on the aircraft.
Two forward NVG position
lights (figure 2-2) are mounted forward of the FM hom-
ing antenna on both sides of the aircraft. Two lower
NVG position lights (figure 2-2) are mounted forward
of the APR-39 antenna support. One aft NVG position
light is located on top of the tail light support assembly.
Power for NVG position lights is provided by the NVG
POS LTS circuit breaker (figure 2-12).
Operation of
the NVG position lights is controlled by a five-position
rotary switch, NVG POS LTS, (figure 2-12) located on
the overhead console. In position 1, the lights are at
minumum intensity, in position BRT, the lights are at
maximum intensity.
2-53.
ANTI-COLLISION LIGHTS.
The anti-collision lights are located one on top of the en-
gine cowling and one centered at the lower section of
the fuselage aft of the avionics compartment. Electri-
cal power for the anti-collision lights is provided by the
28-volt DC electrical system essential bus. The anti-
collision light switch is located on the overhead con-
sole (figure 2-12). The switch is a two-position toggle
type labeled ANTI-COLLISION LTS and OFF. The for-
ward position energizes the anti-collision light circuit.
Float equipped helicopters have lower light relocated
from boom station 88.0 to boom station 103.0.
2-54.
LANDING LIGHTS.
IR/White (Dual) Landing/Searchlight.
A dual light as-
sembly with a white light on one side and IR light on the
other side is mounted in the lower nose section of the
helicopter (figure 2-2).
Do not illuminate IR light with light assembly
fully retracted.
Doing so may cause light to
overheat, resulting in damage to electrical com-
ponents of the helicopter.
Power for the light assembly is provided by the SRCH
LT CONT and SRCH LT PWR circuit breakers. One
three-position switch and one four-position switch, co-lo-
cated on the pilot collective lever (figure 2-4), are used
to operate the light assembly.
DELETED
The three-position switch LDG LT (ON-NVG-OFF) con-
trols illumination of the white light (ON position) and the
IR light (NVG position).
NOTE
White light will automatically extinguish when
light rotates 90° right or left of center, if extended
less than 60°.
The four-position switch LDG LT (EXT-RETR-L-R) pro-
vides extension, 360° rotation and retraction.
Change 12
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 ...