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TM 55-1520-228-10
Change 11 8-17/(8-18 blank)
8-40. ICING CONDITIONS.
a.
Intentional flight in any icing condition is prohib-
ited. If icing conditions are encountered during flight,
effort should be made to vacate the icing conditions.
b.
If icing conditions become unavoidable, the pilot
should turn on pitot heat, windshield defroster and the
engine anti-ice system.
c.
During flights in icing, the following conditions
may be experienced:
(1)
Obscured forward field of view due to accu-
mulation on windscreen and chin bubbles. If windshield
defrosters fail to keep windshield clear of ice, side win-
dows may be used for visual reference during landing.
(2)
One-per-rotor-revolution vibrations, from mild
to severe, caused by asymmetrical ice shedding on
main rotor system. Severity of vibration will depend on
temperature and amount of accumulation on blades
when ice shed occurs. Possibility of asymmetrical ice
shed occurring increases as outside air temperature
decreases.
(3)
An increase in torque required to maintain a
constant airspeed and altitude due to ice accumulation
on the rotor system and possible degradation of the
ability to maintain autorotational rotor speed within oper-
ating limits.
d.
Control activity cannot be depended upon to re-
move ice from the main rotor system. Vigorous control
movements should not be made in an attempt to reduce
low frequency vibrations caused by asymmetrical shed-
ding of ice from main rotor blades. These movements
may induce more asymmetrical shedding of ice, further
aggravating helicopter vibration levels.
WARNING
Ice shed from rotor blades and/or other
rotating components presents a
hazard to personnel during landing
and shutdown. Ground personnel
should remain clear of helicopter
during landing and shutdown;
passengers/crew members should not
exit aircraft until rotor has stopped
turning.
8-41. SAND AND DUST OPERATION.
Efficiency of the particle separator is directly related to
the amount of engine bleed air available. Bleed air is
used to operate the particle separator, and remove
sand/dust particles before they enter the engine plenum
chamber.
a. Ground Operations. At ground idle, with heater
on, particle separator with improved nozzles has a
cleaning efficiency of approximately 53%; with heater
off, cleaning efficiency is approximately 75%.
b. Extended Ground Operations. If extended
ground operations are expected, it is recommended
heater be turned off. Should environmental conditions
require use of heater, it is recommended OH-58 be op-
erated close to 100% N2 with blades in flat pitch. This
condition should permit particle separator to function at
a cleaning efficiency of over 70%.
Содержание OH-58A
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Страница 53: ...TM 55 1520 228 10 Change 13 2 11 Figure 2 5 Principal Dimensions Sheet 1 of 2 ...
Страница 56: ...TM 55 1520 228 10 Figure 2 7 Float Gear Equipped Helicopter 2 14 ...
Страница 57: ...TM 55 1520 228 10 Figure 2 8 Locking Devices for Doors 2 15 ...
Страница 59: ...TM 55 1520 228 10 2 17 Figure 2 9 WSPS Configuration ...
Страница 61: ...TM 55 1520 228 10 Change 11 2 19 FIGURE 2 10 HAS BEEN DELETED ...
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 69: ...TM 55 1520 228 10 2 25 Figure 2 13 Instrument Panel and Console Typical A ...
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 ...
Страница 115: ...TM 55 1520 228 10 Change 11 2 67 2 68 blank Figure 2 25 Paved Surface Mooring Configuration OH 58A C ...
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Страница 170: ...TM 55 1520 228 10 Figure 5 2 Instrument Markings Sheet 1 of 3 5 3 blank 5 4 Change 14 ...
Страница 171: ...TM 55 1520 228 10 Change 11 5 5 Figure 5 2 Instrument Markings Sheet 2 of 3 ...
Страница 175: ...TM 55 1520 228 10 Change 11 5 9 T63 A 720 Figure 5 3 Airspeed Operating Limits Chart ...
Страница 181: ...TM 55 1520 228 10 Change 11 6 3 MS019072 FWD FWD 3000 Figure 6 2 Center of Gravity Limit Chart ...
Страница 182: ...TM 55 1520 228 10 6 4 Change 10 Figure 6 3 Cargo Space ...
Страница 183: ...TM 55 1520 228 10 Change 11 6 5 Figure 6 4 Fuel Loading Chart ...
Страница 184: ...TM 55 1520 228 10 6 6 Figure 6 5 Personnel Loading ...
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Страница 200: ...TM 55 1520 228 10 Figure 7 11 Maximum Torque Available 30 Minute Operation Chart Sheet 1 of 4 7 48 ...
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Страница 204: ...TM 55 1520 228 10 Figure 7 12 Torque Available Continuous Operation Chart Sheet 1 of 4 7 52 ...
Страница 205: ...TM 55 1520 228 10 Figure 7 12 Torque Available Continuous Operation Chart Sheet 2 of 4 7 53 ...
Страница 206: ...TM 55 1520 228 10 Figure 7 12 Torque Available Continuous Operation Chart Sheet 3 of 4 7 54 ...
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Страница 211: ...TM 55 1520 228 10 Change 10 7 59 Figure 7 13 Hover Chart Sheet 3 of 3 ...
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Страница 215: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 1 of 13 7 63 ...
Страница 216: ...TM 55 1520 228 10 Figure 7 15 Cruise Chart Sheet 2 of 13 7 64 ...
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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 ...
Страница 231: ...TM 55 1520 228 10 7 79 Figure 7 17 Climb Descent Chart C ...
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Страница 237: ...TM 55 1520 228 10 Figure 7 19 Idle Fuel Flow Chart 7 85 7 86 blank ...
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Страница 242: ...TM 55 1520 228 10 8 4 Change 10 Figure 8 1 Exterior Check Diagram ...
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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 ...
Страница 268: ...SECTION II MISSION EQUIPMENT NOT APPLICABLE 9 12 Change 14 TM 55 1520 228 10 ...
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Страница 292: ...PIN 014142 000 ...