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时间:2011-04-23 09:57来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

4. Start fuel .ow from fuel dispenser and refuel helicopter.

If fuel is observed .owing from vent, dis-continue refueling and make an entry on DA Form 2408-13-1.
Change 4 2-75

12
3
76 54

C
APU OIL FILLER CAP
A2
AND DIPSTICK
A1

FILL TO
SPILL PLUG
FULL
ADD
FULL
1
OIL LEVEL
ADD
 INDICATOR
A1
B

OIL LEVEL INDICATOR
ADD
NO. 1 NO. 2 AND BACKUP

FRONT
HYDRAULIC PUMP MODULES LEVEL INDICATOR

HYDRAULIC FLUID COLOR
SPEC MIL.H
FULL LEVEL CAPACITY 65 CU. IN. @ 70
REFILL LEVEL CAPACITY 35 CU. IN. @ 70 F
6
7 RED GREEN BLUE (REFILL) (FULL) (EXPANSION)

NOTE SOME HELICOPTERS MAY HAVE COLORS AS RED
ENGINE OIL
LEVEL INDICATOR
(SAME FOR NO. 1
AND NO. 2 ENGINES)

1. & 2. AUXILIARY POWER UNIT
 3. INTERMEDIATE GEAR BOX OIL
2

LEVEL INDICATOR
 4.
CLOSED CIRCUIT AND PRESSURE REFUELING PORTS, NO. 1 (LEFT)FUEL TANK GRAVITY REFUEL PORT

5.  
NO. 1 AND NO. 2 ENGINE
OIL LEVEL INDICATOR


6.
NO. 1 HYDRAULIC PUMP MODULE

 7.
BACKUP HYDRAULIC PUMP
MODULE

 

T.62T.40.1 APU
OIL FILL CAP
A2 GTC.P36.150 APU

FOR REFILL, GREEN FOR FULL, AND BLACK FOR EXPANSION AS VIEWED FROM HELICOPTER RIGHT
4

SIDE PRESSURE
NO. 1 ENGINE OIL LEVEL INDICATOR  NO. 1 (LEFT) FUEL TANK GRAVITY REFUEL PORT 

5 CLOSED CIRCUIT REFUEL PORT CAP 

B
REFUEL PORT CAP
INTERMEDIATE GEAR BOXNO. 1 ENGINE LEFT SIDE

(SAME FOR NO. 1 AND NO. 2 ENGINES)  SA AA0324_1B 
Figure 2-24. Servicing Diagram (Sheet 1 of 3) 
2-76  Change 3 

9 10
8

12  11 

TRANSMISSION OIL LEVEL DIPSTICK  ENGINE OIL FILLER CAP 
OR  FAR SIDE VIEW D  D  OIL FILLER CAP  9

NO. 2 ENGINE RIGHT SIDE (SAME FOR NO. 1 AND NO. 2 ENGINES)
RESERVOIR INDICATOR

NO. 2 HYDRAULIC QUANTITY HANDLE
PUMP MODULE
LOW SWITCH FLUID LEVEL INDICATOR HANDPUMP (SAME FOR ALL SELECTOR
11

PUMP MODULES) VALVE
INDICATOR
(SERVICEABLE IF
GOLD BAND EXPOSED)
10
MAIN ROTOR DAMPER

HYDRAULIC PUMP MODULE REFILL OIL LEVEL
REFILL WITH ONE QUART WHEN FLUID INDICATOR

HANDPUMP
REACHES THIS LEVEL
E E

 8. MAIN TRANSMISSION OIL FILLER PORT   11. MAIN ROTOR DAMPER CHARGE 
AND DIP STICK INDICATOR
 9. NO. 2 ENGINE OIL FILLER PORT AND   12. NO. 2 (RIGHT) FUEL TANK GRAVITY 
SIGHT GAGE REFUEL PORT
 10. NO. 2 HYDRAULIC PUMP MODULE AND   13. TAIL ROTOR GEAR BOX LEVEL SIGHT 
PUMP MODULE REFILL HANDPUMP GAGE  AA0324_2 
SA 

Figure 2-24. Servicing Diagram (Sheet 2 of 3)

5. Once fuel has reached the desired level, remove the fuel dispenser nozzle from the refueling adapter and cap pressure fueling adapter.
2.78.5 Fuel Sampling System. Fuel sampling is done with a thumb-operated handpump (Figure 2-24) containing 5 feet of plastic tubing. The tubing is placed in a guide tube inside the fuel tank and is directed to the bottom of the tank. The handpump is stroked and fuel is drawn from the tank, with contaminants at the bottom. When sampling is completed, the tubing is emptied, rolled, and stowed with the pump on the gravity refueling door.

Fuel sam-pling of the external extended range fuel system is done by taking the sample with a fuel sampler tube from the sump drain located at the bottom aft of each tank.
2.79 EXTERNAL AIR SOURCE/ELECTRICAL REQUIREMENTS.
Refer to Chapter 5 for limitations.
 
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