CHAPTER 79 ENGINE OIL SYSTEM. Section Title Page

Transcription

1 CHAPTER 79 ENGINE OIL SYSTEM Section Title Page Description Scroll and Fanwheel Assemblies Fanwheel-to-Inlet Gaps Oil Tank Assembly Oil Temperature Sender Sight Gage Engine Oil Cooler Engine Oil Line Assemblies and Fittings SEP 2012 R66 Maintenance Manual Chapter 79 Engine Oil System Page 79.i

2 Intentionally Blank Page 79.ii Chapter 79 Engine Oil System R66 Maintenance Manual SEP 2012

3 CHAPTER 79 ENGINE OIL SYSTEM Description The R66 helicopter has a dry-sump engine oil system. Oil is stored in a remote tank located in the main rotor gearbox compartment. Refer to Section for oil servicing instructions. A Rolls-Royce-supplied oil temperature sender is mounted on the inboard side of the oil tank. Oil circulates through the engine oil system via three oil delivery lines. Refer to Figure Cool oil exits the oil tank and enters the engine, hot oil exits the engine and enters the engine oil cooler, and cooled oil exits the oil cooler and returns to the oil tank. An oil tank vent line is plumbed to the engine accessory gearbox, which is vented to the exhaust pipe. The engine oil cooler has an internal thermostat and pressure relief valve. The thermostat maintains normal system operating pressure by allowing cool oil to bypass the heat exchanger and return to the oil tank. Higher than normal system pressure will open a pressure relief valve. When draining the oil system, residual oil is trapped in the bottom corner of the oil cooler due to the oil cooler installation angle in the R66. An oil cooler drain plug allows the technician to drain trapped oil during servicing. The engine oil system includes an oil pump, oil filter and regulating valve, an oil sump tank, a check valve, and two magnetic plug inserts. Refer to RR300 OMM for a complete description of the engine oil system. FIGURE 79-1 ENGINE OIL SYSTEM SCHEMATIC SEP 2012 R66 Maintenance Manual Chapter 79 Engine Oil System Page 79.1

4 FIGURE 79-2 SCROLL AND FANWHEEL ASSEMBLIES Page 79.2 Chapter 79 Engine Oil System R66 Maintenance Manual SEP 2012

5 79-10 Scroll and Fanwheel Assemblies Refer to R66 Illustrated Parts Catalog (IPC) Figure Remove F196-1 fan shaft per Section Refer to Figure Remove perimeter screws securing F236-1 scroll assembly to F306-1 box assembly. 3. Remove aluminum tape sealing gaps & joints, or gently pull scroll away from box assembly and, using a scribe or similar sharp instrument, tear aluminum tape sealing gaps & joints. Remove scroll, with G174-1 fanwheel assembly inside, up through frame. 4. Remove hardware securing forward or aft F305-5 inlet to scroll; remove inlet & fanwheel. Remove damaged aluminum tape from scroll and box assembly. 1. Refer to Figure Observing AFT orientation marking on fanwheel plate, place G174-1 fanwheel assembly inside F236-1 scroll assembly accordingly. Position F305-5 inlets on scroll and install hardware. Verify security. 2. Lower scroll, with fanwheel inside, through frame and install hardware securing scroll to F306-1 box assembly. Verify security. Seal gaps & joints using A701-1 aluminum tape. 3. Install F196-1 fan shaft per Section Fanwheel-to-Inlet Gaps A. Measuring Gap 1. Remove tailcone cowling assembly per Section Refer to Figure Verify 0.10 inch minimum gap between G174-1 fanwheel assembly and forward and aft F305-5 inlets. Check gap all the way around; rotate fanwheel and check gap again (several positions). If gap is within limits at forward and aft inlets, no further action is required. 3. Verify proper tail rotor driveline shimming per Section Trim inlets as required per Part B. 5. Install tailcone cowling assembly per Section SEP 2012 R66 Maintenance Manual Chapter 79 Engine Oil System Page 79.3

6 FIGURE 79-3 ENGINE OIL SYSTEM Page 79.4 Chapter 79 Engine Oil System R66 Maintenance Manual SEP 2012

7 79-11 Fanwheel-to-Inlet Gaps (continued) B. Trimming Inlets 1. Refer to Figure Remove hardware securing F305-5 inlets to F236-1 scroll assembly. 2. If inlets are slotted, carefully twist inlets over F196-1 fan shaft and remove inlets. If inlets are not slotted, remove hardware securing fan shaft to C947-3 plate assemblies, noting hardware removed, and remove inlets. 3. Refer to Figure 79-2, Detail A. Trim inlets as required to meet minimum fanwheelto-inlet gap. Do not exceed minimum inlet dimensions. 4. Refer to Section Smooth inlet edges and coat bare metal with primer. Touchup primed area using dark gray Dupont Imron polyurethane enamel in accordance with paint manufacturer s recommendations. 5. If inlets are slotted, carefully twist inlets over fan shaft and install hardware securing inlets to scroll assembly (slot orientation is optional). Verify security. 6. If inlets are not slotted, install inlets around fan shaft and install hardware securing inlets to scroll assembly. Verify security. Install hardware securing fan shaft to plate assemblies, standard torque nuts and palnuts per Section 20-32, and torque stripe per Figure Measure fanwheel-to-inlet gaps per Part A. Repeat procedure as required for minimum 0.10 inch gap at forward and aft inlets Oil Tank Assembly Refer to R66 Illustrated Parts Catalog (IPC) Figure Drain engine oil per Section Remove tailcone cowling assembly per Section Open main rotor gearbox compartment access door. 3. Refer to Figure Cut and discard safety wire securing tube to G689-1 oil tank assembly scupper drain. Pull tube off of drain. 4. Disconnect harness assembly plug from MS oil temperature sender (located on inboard side of tank). 5. Remove hardware securing line assembly clamps. 6. Loosen F723-1, F723-3, and F723-4 line assembly B-nuts from engine, F649-1 oil cooler, and tank fittings; disconnect lines from tank fittings and plug lines. 7. Remove nuts securing tank fittings to firewall. 8. Remove hardware securing tank tabs to F384-3 angles. Remove tank through access door and cap fittings. SEP 2012 R66 Maintenance Manual Chapter 79 Engine Oil System Page 79.5

8 79-20 Oil Tank Assembly (continued) 1. Refer to Figure Remove caps from G689-1 oil tank assembly fittings. 2. Torque check union at oil cooler, and torque check engine (oil line) unions and check valve per Section Insert tank through main rotor gearbox compartment access door. Install hardware securing tank tabs to F384-3 angles. 4. Install nuts securing tank fittings to firewall and special torque nuts per Section Remove plugs and connect F723-1, F723-3, and F723-4 line assembly B-nuts to tank fittings. Special torque B-nuts at tank, F649-1 oil cooler, and engine per Section and torque stripe fittings. 6. Install hardware securing line assembly clamps. 7. Connect harness assembly plug to oil temperature sender (located on inboard side of tank). 8. Fit tube onto tank scupper drain. Wrap tube with two turns inch diameter lockwire and safety tube to drain. 9. Service engine oil per Section Install tailcone cowling assembly per Section Oil Temperature Sender Refer to R66 Illustrated Parts Catalog (IPC) Figure Drain engine oil per Section Remove tailcone cowling assembly per Section Refer to Figure Disconnect harness assembly plug from MS oil temperature sender (located on inboard side of G689-1 oil tank assembly). 4. Remove sender and gasket from tank, and discard gasket. 5. Tape sender opening to protect tank from contaminants. 1. Refer to Figure Remove tape from G689-1 oil tank assembly sender opening and verify tank interior is free of contaminants. 2. Install new gasket on MS oil temperature sender, and install sender in inboard side of tank. Special torque sender per Section Connect harness assembly plug to sender. 4. Service engine oil per Section Install tailcone cowling assembly per Section Page 79.6 Chapter 79 Engine Oil System R66 Maintenance Manual SEP 2012

9 79-22 Sight Gage Refer to R66 Illustrated Parts Catalog (IPC) Figure Drain engine oil per Section Refer to Figure Remove B563-2 sight gage and o-ring from G689-1 oil tank assembly. Discard o-ring. 3. Tape gage opening to protect tank from contaminants. 1. Refer to Figure Remove tape from G689-1 oil tank assembly gage opening and verify tank interior is free of contaminants. 2. Lubricate new o-ring using approved turbine engine oil per R66 Pilot s Operating Handbook (POH) Section 8. Install o-ring on B563-2 sight gage, and install gage in tank. Special torque gage per Section Service engine oil per Section Engine Oil Cooler Refer to R66 Illustrated Parts Catalog (IPC) Figure Drain engine oil per Section Refer to Figure Remove fasteners securing F649-1 oil cooler to F309-1 box assembly. 3. Remove hardware securing line assembly clamps. 4. Support oil cooler without damaging oil cooler fins. Loosen F723-2 and F723-4 line assembly B-nuts at engine, oil cooler, and G689-1 oil tank assembly fitting; disconnect lines at oil cooler unions. Cap unions and plug lines. 1. Refer to Figure Remove F649-1 oil cooler union caps. Torque check oil cooler unions and engine (oil line) union or check valve (early R66s) per Section Remove plugs and connect F723-2 and F723-4 line assembly B-nuts to oil cooler fittings. Special torque B-nuts at tank, oil cooler, and engine per Section and torque stripe fittings. 3. Install hardware securing line assembly clamps. 4. Install hardware securing F649-1 oil cooler to F309-1 box assembly. 5. Service engine oil per Section SEP 2012 R66 Maintenance Manual Chapter 79 Engine Oil System Page 79.7

10 79-40 Engine Oil Line Assemblies and Fittings Refer to R66 Illustrated Parts Catalog (IPC) Figure Drain engine oil per Section Refer to Figure Remove hardware securing line assembly clamps. 3. Disconnect F723 line assembly B-nuts from engine, F649-1 oil cooler, and/or G689-1 oil tank assembly fittings, as required. Cap fittings and plug lines. 4. Carefully remove line assembly from engine compartment. 1. Refer to Figure Remove caps from unions. Torque check F649-1 oil cooler unions and/or G689-1 oil tank assembly nuts per Section 20-33; torque check engine (oil line) unions and/or check valve (early R66s) per Section 20-33, as required. 2. Remove plugs and connect F723 line assembly B-nuts to engine, oil cooler, and/or tank, as required. Verify 0.2 inch minimum clearance between shaft weldment and firewall grommet; verify equal gap concentrically between shaft and box assembly hole edges. Adjust F174-1 support weldment rod ends per Section as required. Special torque B-nuts per Section and torque stripe fittings. 3. Install hardware securing line assembly clamps. 4. Service engine oil per Section Page 79.8 Chapter 79 Engine Oil System R66 Maintenance Manual SEP 2012