TM 55-1520-228-10
2-86.1
.
ROTOR BLADE TIE-DOWN.
CAUTION
Secure the tie-down ropes carefully.
Do not damage the skin by flipping
the strap weights around the
tailboom.
NOTE
Ensure that strap side of main rotor tie-
down boot is on top side of blade and
drain hole is positioned at bottom of
blade.
a.
To tie-down the aft blade, securely tie the straps
of the boot to the 1/2 inch polyester rope near the boot.
Ensure the ropes are long enough to cross and tie in
position.
b.
The forward blade shall also be tied down using
the same boot strap/rope arrangement device. The
ropes shall be routed between the base and side sup-
port struts of the forward lower cutter and tied at the rear
of the base. In the final tie-position the blades must be
in a level position.
c.
Install covers on pitot tube, engine exhaust, and
engine inlets.
d.
An alternate method of installing pitot and en-
gine inlet covers will aid in preventing marring and
scratching of windshields and is accomplished as fol-
lows:
(1)
Route strap from pitot tube through lower
front edge of pilot door near lower hinge, and then out
the top edge of door to engine air inlets.
(2)
Cut strap connecting pitot cover to engine
shields strap at both ends. Pitot tube cover may be held
in place with the nylon cord and/or a scrapped packing
of proper diameter. If a packing is used, it may be perma-
nently attached to pitot tube cover to prevent its loss
when the cover is removed. The strap connecting the
engine shields should also be shortened.
e.
Position collective control full down, and tighten
friction.
f.
Center cyclic control and tighten friction.
g.
Close all windows, doors, and access panels.
h.
Fill fuel tank to capacity with prescribed fuel.
i.
Secure all ground handling equipment.
2-87.
MOORING - FLOAT EQUIPPED HELICOP-
TER.
Float equipped helicopters may be moored using same
procedures as are used for skid gear equipped helicop-
ters. Surface of mooring area must be smooth and free
of any objects which may damage or penetrate floats.
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 133: ...TM 55 1520 228 10 Change 11 3 13 FIGURE 3 7 HAS BEEN DELETED ...
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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 ...
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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 ...
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 ...
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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 ...