Piper ARROW III Service Manual

6-15. NOSE GEAR ACTUATING CYLINDER.
6-16. REMOVAL OF NOSE GEAR ACTUATING CYLINDER.
a. Place the airplane on jacks. (Refer to Jacking, Section II.)
b. Disconnect the hydraulic lines from the actuating cylinder and cover the open line ends to prevent
contamination.
c. Disconnect the cylinder operating rod end from the downlock hook by removing attachment nut and
bolt.
d. Disconnect the cylinder from its attachment fitting by removing nut and bolt.
e. 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, remove the fitting from the piston rod (6) end of the
cylinder (7). Mark the position of the fitting to facilitate reinstallation.
b. On Syncro Devices nose gear actuating cylinders, remove the snap ring (1) from the annular slot in the
end of the housing. On Gar-Kenyon nose gear actuating cylinder, remove safety wire (9) and unscrew
end gland (2).
c. On Syncro Devices assemblies, pull the piston (6) with end gland (2) from the cylinder housing. On
Gar-Kenyon assemblies, remove piston (6) after unscrewing end gland (2).
6-18. CLEANING, INSPECTION, AND REPAIR OF NOSE GEAR ACTUATING CYLINDER.
a. Clean the cylinder parts with a suitable dry type solvent and dry thoroughly.
b. Inspect the cylinder assembly for the following:
1. Interior walls of the cylinder and exterior surfaces of the piston for scratches, burrs, corrosion, etc.
2. Threaded areas for damage.
3. Rod end fitting and swivel fitting of cylinder for wear, cracks and corrosion.
4. O-rings for damage.
c. Repairs to the cylinder and limited to polishing out small scratches, burrs, etc. and replacing parts.
6-19. ASSEMBLY OF NOSE GEAR ACTUATING CYLINDER. (Refer to Figure 6-7.)
a. Install O-ring (5) on the exterior of the end gland (2).
b. Install O-ring (4) line the interior of the end gland. The Syncro Devices assemblies also include a ring
back-up (3) with the O-ring (4).
c. Install O-ring (8) on the body of the piston assembly.
d. Install the spacer into the cylinder body if applicable.
e. Lubricate the areas around the O-rings with hydraulic fluid, slide the end gland on the piston rod and
the piston into the cylinder housing (7).
f. Secure the end gland in the cylinder by installing the snap ring (1) in the annular slot in the Syncro
Devices cylinder. The end gland on the Gar-Kenyon cylinder is secured by threading gland into
cylinder body (7) and securing with safety wire (9).
g. Install restrictor fitting in the piston rod end of the cylinder.
h. Check smoothness of operation of the piston.
Revised: 2/13/89
1I4
* CHEROKEE ARROW III SERVICE MANUAL
HYDRAULIC SYSTEM

Piper ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	ARROW III
Engine	Lycoming IO-360-C1C6
Horsepower	200 hp
Maximum Takeoff Weight	2, 750 lb (1, 247 kg)
Seating Capacity	4
Propeller	2-blade, constant speed
Length	24 ft 7 in (7.49 m)