(c)
Lube scavenge tube
(d)
Tube for anti-siphon oil return
(e)
Scupper drain tube.
S 034-006-C00
(6)
Remove and keep the gaskets for the vent, lube supply and lube scavenge tube.
S 034-009-C00
(7)
Remove the oil quantity transmitter (AMM 79-31-01/401).
S 034-010-C00
(8)
Remove the nut from the forward mount pin.
(a) Remove the ground strap.
1) ENGINES WITH CFMI SB 72-444; Remove the ground strap with the bolt cup attached.
S 034-011-C00
(9) Disconnect the retainers for the forward and aft mount bushings:
(a)
Remove the two bolts from each retainer.
(b)
Disconnect the retainers.
S 034-012-C00
(10)
Remove the cotter pin, nut and bolt that attach the tank to the upper mount link.
(11)
Remove the tank.
(12)
Install caps in the open ends of the tubes and tank openings.
S 024-013-C00
S 494-014-C00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-11-01
ALL ú ú C02 Page 405 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-015-C00
(13)
Remove the nut from the aft mount pin.
S 034-016-C00
(14)
Remove the forward and aft retainers and bushings.
S 034-017-C00
(15)
If you replace the tank, do the steps that follow:
(a)
Remove the four bolts at the forward and aft mount pins.
(b)
Remove and keep the pins.
(c)
Discard the o-rings.
TASK 79-11-01-404-019-C00
3. Oil Tank Installation
_____________________
A. Consumable Materials
(1)
DOO599, 0il, (CP2442) engine - CFMI SB 79-001
(2)
D00601, Grease, (CP2101) graphite - GP460, Aeroshell 8
(3)
D00625, Grease, (CP2338) conductive - Brisal OX
B. References
(1)
AMM 12-13-11/301, Engine Oil
(2)
AMM 70-30-01/201, Seals (Preformed Packing and O-rings)
(3)
AMM 71-00-00/501, Power Plant
(4)
AMM 71-11-02/201, Fan Cowl Panels
(5)
AMM 79-31-01/401, Oil Quantity Transmitter
C. Access
(1)
Location Zones 506 Engine No. 1 - Right side on the fan case 606 Engine No. 2 - Right side on the fan case
(2)
Access Panels 5737L Right Fan Cowl Panel - Engine No. 1 5837R Right Fan Cowl Panel - Engine No. 2
D. Procedure (Fig. 401)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
79-11-01
ALL ú ú C03 Page 406 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 864-065-C00
WARNING:_______DO NOT LET ENGINE OIL STAY ON YOUR SKIN. USE ENGINE OIL IN AREA WITH GOOD VENTILATION. ENGINE OIL IS POISONOUS AND CAN BE ABSORBED THROUGH YOUR SKIN. ENGINE OIL FUMES CAN IRRITATE YOUR RESPIRATORY TRACT.
CAUTION: DO NOT LET ALKALINE CLEANING FLUID GET INTO THE ENGINE OIL.
_______ VERY SMALL QUANTITIES OF THIS FLUID CAN CHANGE THE ENGINE OIL. DAMAGE TO EQUIPMENT CAN OCCUR.
CAUTION: DO NOT LET HOT OIL GET ON THE ENGINE OR OTHER COMPONENTS.
_______ IMMEDIATELY CLEAN THE COMPONENT IF OIL FALLS ON IT. OIL CAN CAUSE DAMAGE TO PAINT AND RUBBER.
(1)
Obey the above Warning and Cautions through all this procedure.
S 214-020-C00
(2)
Examine the gaskets you kept (AMM 70-30-01/201).
(a) Use the gaskets if they are in a good condition.
S 434-021-C00
(3) If you replaced the tank, do the steps that follow:
(a) Install the forward and aft mount pins on the replacement tank. 1) Lubricate a new o-ring with engine oil. 2) Install the o-ring in the groove on the mount pin. 3) Install the mount pin in the tank. 4) Install four bolts, lightly lubricated with grease. 5) Tighten the bolts to 100-110 pound-inches
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 滑油 OIL(12)
