Disassembly Of Nose Gear Actuating Cylinder - Piper Lance II Service Manual

1
2 4
5
6
7
1. SAFETY WIRE
2. END GLAND
3. "O" RING
4. "O" RING
5. PISTON
6. BODY, CYLINDER
7. "O" RING
Figure 6-7. Nose Gear Actuating Cylinder
CAUTION
Whenever aircraft is placed on jacks for the purpose of
manually retracting the nose gear assembly, insure the
nose gear downlock is fully disengaged before releasing
the nose gear drag links. Damage could occur to the
downlock if not disengaged fully.
d. Disconnect the aft end of cylinder from its attachment fitting and remove the
cylinder from the wheel well.
6-17. DISASSEMBLY OF NOSE GEAR ACTUATING CYLINDER (Refer to Figure 6-7.)
a. With the cylinder removed from the airplane, mark the position of the end gland (2)
to facilitate reinstallation.
b. Remove safety wire (1) and unscrew end gland (2).
c. Additional disassembly of piston (5) and "O" rings (3), (4) and (7) may now be
accomplished.
Issued: 1/3/78
HYDRAULIC SYSTEM
LANCE II SERVICE MANUAL