12-20-00 Page 12-27 Revised: February 28, 2002
COMPONENT LUBRICANT FREQUENCY
1. RUDDER & STABILATOR HINGE PINS, RUDDER TAB & STABILATOR TAB ROD END BEARINGS, STABILATOR TRIM TAB LINKS, STABILATOR CONTROL & RUDDER CONTROL CABLE PULLEYS, FLAP TORQUE TUBE BEARING BLOCK. FLAP HANDLE PIVOT POINT, FLAP LOCK MECHANISM & TURN BUCKLE END & TEE BAR PIVOT POINTS, CONTROL COLUMN FLEX JOINT, SPROCKET & “O” RING, AILERON & STABILATOR CONTROL PULLEYS. STABILATOR CONTROL ROD & IDLER PULLEY — SEE SPECIAL INSTRUCTIONS 2 AND 6 AND CAUTIONS MIL-L-7870 100 HRS
1A. AILERON, STABILATOR, AND RUDDER CONTROL CABLES (at each pulley and fairlead, see #1, above) — SEE SPECIAL INSTRUCTION 6 AND CAUTIONS 2 AND 4. AEROSHELL 33 MIL-G-23827 100 HRS
2. AILERON HINGE BEARINGS, FLAP HINGE BEARINGS AND FLAP CONTROL ROD END BEARINGS — SEE SPECIAL INSTRUCTIONS 2 AND 6 MIL-L-7870 100 HRS
3. FLAP RETURN & TENSION CHAINS, AND AILERON & STABILATOR CONTROL CHAIN — SEE SPECIAL INSTRUCTIONS 2 AND 6 MIL-L-7870 500 HRS
4. RUDDER & STABILATOR TRIM SCREW - SEE SPECIAL INSTRUCTIONS 2 AND 6 MIL-S-8660B DOW #4 COMPOUND 500 HRS
SPECIAL INSTRUCTIONS
2. Bearings and Bushings - Clean exterior with a dry type solvent before lubricating.
6. Lubrication Points - Wipe all lubrication points clean of old grease, oil, dirt, etc. before lubricating.
CAUTIONS
2. Do not over-lubricate cockpit controls.
4.
Do not oil control cables.
5.
Do not lubricate control wheel shaft or bushing. Clean only with alcohol or other suitable solvent.
Figure 12-4. Lubrication Chart (Control System, Part 1) (Sheet 1 of 2)
12-20-00 Page 12-28 Revised: February 28, 2002
1G4
12-20-00 Page 12-29 Revised: February 28, 2002
COMPONENT LUBRICANT FREQUENCY
l. RUDDER HINGE BEARINGS, RUDDER TAB STABILATOR TAB HINGE PINS - SEE SPECIAL INSTRUCTIONS 2 AND 6. MIL-L-7870 100 HRS
2. AILERON CONTROL ROD END BEARINGS, AILERON BELLCRANK PIVOT POINTS, AILERON BELLCRANK CABLE ENDS, AILERON CONTROL CABLE PULLEYS, RUDDER CONTROL CABLE PULLEYS, TRIM CONTROL WHEELS (RUDDER & STABILATOR), TOE BRAKE ATTACHMENT, RUDDER TUBE CONNECTIONS, RUDDER TUBE CABLE ENDS, NOSE GEAR STEERING ROD ENDS, BRAKE ROD ENDS, STABILATOR BELLCRANK PIVOT POINT & CABLE ENDS - SEE SPECIAL INSTRUCTION 6 AND CAUTIONS 2 AND 4. MIL-L-7870 100 HRS
2A. AILERON, STABILATOR, AND RUDDER CONTROL CABLES (at each pulley and fairlead, see #2, above) — SEE SPECIAL INSTRUCTION 6 AND CAUTIONS 2 AND 4. AEROSHELL 33 MIL-G-23827 100 HRS
3. TOE BRAKE BRACE — SEE SPECIAL INSTRUCTION 6 MIL-G-7711 100 HRS
SPECIAL INSTRUCTIONS
2. Bearings and Bushings - Clean exterior with a dry type solvent before lubricating.
6. Lubrication Points - Wipe all lubrication points clean of old grease, oil, dirt, etc., before lubricating.
CAUTIONS
2. Do not use excessive lubrication on cockpit controls.
4. Do not oil control cables.
Figure 12-5. Lubrication Chart (Control System, Part 2) (Sheet 1 of 2)
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COMPONENT LUBRICANT FREQUENCY
1. COWL FLAP HINGE, GOVERNOR CONTROL, CONTROL QUADRANT CONTROLS, CABIN HEAT & DEFROST MECHANISMS, SELECTOR VALVE CONTROL - SEE SPECIAL INSTRUCTION 6 AND CAUTION 2. MIL-L-7870 100 HRS
2. AIR FILTER - SEE SPECIAL INSTRUCTION 1 CLEAN AS OFTEN AS NECESSARY 50 HRS
3. CARTRIDGE TYPE OIL FILTER CHANGE 50 HRS
4. ENGINE SUMP: 8 QTS CAPACITY. - SEE NOTE 7. MIL-L6082B OR MIL-L-22851 50 HRS
5. PROPELLER ASSEMBLY - SEE SPECIAL INSTRUCTION 5 MIL-G-23827 100 HRS
6. COWL FLAP ACTUATING MECHANISM - SEE LUBRIPLATE #907, SPECIAL INSTRUCTION 8 (PURCH) FISKE BROS. REFINING 500 HRS
7. BATTERY - SEE NOTE 6 25 HRS
8. FUEL SYSTEM - SEE NOTE 5 AS REQUIRED
9. CARBURETOR AIR BOX FLAPPER VALVE LUBRIPLATE #907 (PURCH). FISKE BROS. REFINING CO. 100 HRS
1. 5. 6. 8. 2. 5. 6. 7. SPECIAL INSTRUCTIONS Air Filter - To clean filter, tap gently to remove dirt particles. Do not blow out with compressed air or use oil. Replace filter if punctured.or damaged. Propeller - Remove one of the two grease fittings for each blade, apply grease thru fitting until fresh grease appears at hole of removed fitting. Lubrication Points - Wipe all lubrication points clean of old grease, oil, dirt, etc., before lubricating. Outer surface of inner spacer. CAUTIONS Do not over-lubricate cockpit controls. NOTES Fuel System - Service Regularly - Fuel Pump Strainer Injector Screen - Filter Bowl - Quick Drain Unit. Battery - Check fluid level & condition every 25 hours. Use straight mineral oil during the first 50 hours of operation, or until oil consumption has stailized. For additional servicing information, refer to the latest revision of Textron Lycoming Service Bulletin No. 446 and Service Instruction No. 1014. 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：西門諾爾飛機(jī)維護(hù)手冊 simenole PA-44-180 AMM 1(34)
