TM 55-1520-228-10
Change 11 8-3
8-8. BEFORE EXTERIOR CHECKS.
1. Deleted.
2. Publications – Check DA Forms 2408-12
,
-13
,
-14
,
and -18
;
DD Form 1896 if required; DD
Form 365-4
;
Compass Cards; locally required
forms, records and publications; and availabil-
ity of operator’s manual (-10) and checklist
(-CL).
* 3. Covers, locking devices, tiedowns (except
main rotor), and grounding cables – Removed
and secured.
* 4. Ignition switch – On.
5. Cockpit – Check as follows:
a.
FUEL BOOST switch – OFF.
b.
BAT switch – BAT (check fuel quantity).
c.
NON-ESS BUS switch – MAN.
d.
Lights – Check and set if use is anticipated
(LDG, ANTI-COLLISION, POS, CONSOLE,
INST, and NVG lights).
e.
WARNING and CAUTION lights – Check for
illumination of the ROTOR RPM, MASTER
CAUTION, ENGINE OUT, and XMSN OIL
PRESS lights. Press the WARNING LTS
TEST switch to check XMSN OIL HOT light.
Test caution lights and reset. DC GENERA-
TOR, HYD PRESS, and INST INVERTER
caution lights should remain illuminated. Do
not fly if any of these lights fail to illuminate.
f.
BAT switch – OFF.
g.
Pilot seat, seat belt, shoulder harness, and
armor side panels – Check condition.
O
h.
Crew Door – Check condition.
8-9. EXTERIOR CHECK.
8-10. AREA 1 (figure 8-1) – FUSELAGE –
CABIN RIGHT SIDE.
1. Cabin interior – Check as follows:
O
* a.
Cargo/loose equipment – Check for proper
loading and tiedown.
O
* b.
Auxiliary fuel cell – Check condition, fuel
level, and cap secure.
* c.
Passenger seats and belts – Check as fol-
lows:
(1) Check seat and back cushions for con-
dition and security. Ensure seat belts
are through loops on seat and back
cushions and secured with nylon safe-
ty cord.
(2) Check tabs on top of seat back for con-
dition and security.
(3) Check seat belts and shoulder har-
nesses for condition and security. En-
sure shoulder harnesses and belts are
properly fastened together and tight-
ened when not in use.
(4) If seat belts are not installed, seat and
back cushions must be removed prior
to flight with doors off.
d.
First aid kit – Check.
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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 ...
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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 ...
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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 ...
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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 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 ...
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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 ...