3.
NOSEGEARDOOR ACTUATOR, RETRACTIONROD
END AND CYLINDER ROD END MIL-L-7870 100 HRS
4.
UP LOCK HOOKAND UP LOCKROD MIL-L-7870 100 HRS
5.
DOORHINGE BOLT MIL-L-7870 100 HRS
6.
DRAGLINKASSEMBLYAND IDLER LINK MIL-G-23827,
MIL-G-7711A 100 HRS
7.
WHEELBEARINGS MIL-G-3545C,
MIL-G-7711A 100 HRS
8.
UPPER AND LOWER TORQUE LINKS MIL-G-23827,
MIL-G-7711A 100 HRS
9.
UPPERAND LOWER TORQUE LINK CONNECTING MI L-G-23827,
BOLT AND SHIMMY DAMPENER MIL-G-7711A 100 HRS
10.
GEARHOUSINGBUSHINGS MOLYKOTENO.33 100 HRS
11.
NOSEGEARSTEERING CONTROL ROD ENDS MIL-L-7870 100 HRS
12.
NOSEGEAR UP LOCK CABLE ASSEMBLY (Referto Special Instructions #7, 12-20-00, Page2) MIL-G-81322 100 HRS
13.
NOSEGEARSTEERINGGREASE FITTING MIL-G-23827 100 HRS
11 4
2 6
9
11
NoseLandingGear Figure 302
EFFECTIVITY:
040-999
Jan 10/90 12-20-00
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
B. LubricationCharts(continued)
CHART 4 LUBRICATIONCHART (CONTROL SYSTEM)(Sheet 1 of 3)
COMPONENT LUBRICAN
1.AILERONTRIM SCREW MIL-G-23827,MIL-G-7711A
2.
AILERON TRIM TAB HINGS AND CONTROL ROD ENDS MIL-L-7870
3.
RUDDER TRIM SCREW MIL-G-23827,MIL-G-7711A
4.
RUDDER AND RUDDER TRIM TAB HINGES AND CONTROL ROD ENDS MIL-L-7870
5.
ELEVATORAND ELEVATOR TRIM TAB HINGES AND CONTROL ROD ENDS MIL-L-7870
6.
AILERON HINGES, RIGHT AND LEFT MIL-L-7870
7.
FLAP TRANSMISSION PIVOT BOLTS AND SENDER ARM MIL-L-7870
8.
FLAP TRACKS, RIGHT AND LEFT ALL PURPOSE SLIP SPRAY
(DUPONT NO. 6611)
9.
FLAP TRACK ROLLERS, RIGHT AND LEFT MIL-L-7870
10.AILERON BELLCRANK CABLE ENDS, PIVOT BEARINGAND CONTROL ROD ENDS RIGHT AND LEFT MIL-L-7870
11.TRIM SCREWS MIL-G-3278 OR MIL-G-23827
12.TRANSMISSIONSCREWS, RIGHT AND LEFT MIL-G-23827
13.ELEVATORTRIM SCREW MIL-S-8660B (DOW CORNING 4 COMPOUND OR
14.ELEVATORDOWN SPRING MIL-C-16173D CorrosionRetardant (Referto 91 -00-00)
FREQUENCY 500 HRS 100 HRS 500 HRS 100 HRS 100 HRS 100 HRS 100 HRS
50 HRS
100 HRS
100 HRS
500 HRS
100 HRS
100 HRS
100 HRS
ControlSystem
Figure 303 (Sheet1 of 3)
EFFECTIVITY:
040-999
PAGE5
12-20-00Jan10/90
PIPER AIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCE MANUAL
B. LubricationCharts(continued)
CHART 4 LUBRICATIONCHART(CONTROLSYSTEM)(Sheet2 of 3)
View A View B
13 View E
14
View F
Control System Figure303 (Sheet2 of 3)
EFFECTIVITY:
040-999
PAGE
6 12-20-00
Jan 10/90 122
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
B. LubricationCharts(continued)
CHART 4
LUBRICATIONCHART(CONTROLSYSTEM) (Sheet3 of 3)
COMPONENT LUBRICANT FREQUENCY
1. AILERON BELLCRANKASSEMBLYBUSHING MIL-L-7870 100 HRS
2. CONTROL WHEELCHAIN,VERTICALANDHORIZONTAL MIL-L-7870 500 HRS
3. RUDDER PEDALS,TORQUETUBE BEARINGS AND BLOCK, CONTROL
CABLEENDS,BRAKECYLINDERENDS, AND PULLEYS MIL-L-7870 100 HRS
2
View G View H
Control System
Figure 303 (Sheet3 of 3)
EFFECTIVITY:
040-999
PAGE7
12-2 0 Jan10/90
PIPER AIRCRAFT
PA-42-720(Advanced Trainer)
MAINTENANCEMANUAL
B. Lubrication Charts (continued)
CHART 5 LUBRICATION CHART (POWERPLANT, PROPELLER & REVERSING LINKAGE)
COMPONENT
1.
ZERK FITTINGS, BLADE HUB (2 PER BLADE)
2.
FUEL CONTROL UNIT INTERCONNECT ROD ENDS
3.
CONTROL CAM AND PINS
4.
PROPELLERCONTROLROD ENDS
5.
OIL FILTER ELEMENT
6.
OIL TANK
7.
PUSH PULL CONTROL -WIRE ROPE
NOTE:
Refer to Hartzell Service LetterNo. 61A
1
LUBRICANT
MIL-G-23827 MIL-G-23827 LUBRIPLATE130A MIL-G-23827
MIL-G-21164
FREQUENCY 100 HRS 100 HRS 100 HRS 100 HRS
REFER TO SPECIAL
INSTRUCTION12-20-00Page 2
REFER TO SPECIAL
INSTRUCTION12-20-00 Page 2
100 HRS
PROPELLER
NOTE
SPECIAL INSTRUCTIONS
Clean or replace oil filter element at each oil drain period as described in 79-00-00. In aircraft with a typical utilization of 50 hours/months or less, change engine oil every 400 hours or 9 months, whichever comes first. Refer to Pratt and Whitney Service Bulletin No. 13001 for a list
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