2-48. INDUCTION AIR FILTER.
2-49. REMOVAL OF AIR FILTER. The location of the PA-28R-201 filter is on the left side and just in front of
the firewall. The PA-28R-201T filter is located just in front of the firewall above the turbocharger. Remove
filter by following procedure:
a.
Remove upper engine cowl.
b. Loosen studs and carefully move the cover assembly aside.
c.
The filter is now free for removal. Clean or replace the filter as given in Paragraph 2-50.
2-50. SERVICE INSTRUCTION. (CLEANING AND INSPECTION.)
a.
The filter should be cleaned daily when operating in dusty conditions and if any holes or tears are
noticed, the filter should be replaced immediately. For replacement filter, refer to Parts Catalog.
b. Remove the filter element and shake off loose dirt by tapping on a hard surface, being careful not to
damage or crease the sealing ends.
CAUTION
Never wash the filter element in any liquid or soak in oil. Never attempt to
blow off dirt with compressed air.
c.
The filter housing can be cleaned by wiping with a clean cloth soaked in suitable quick drying type
solvent. When the housing is dry, reinstall in accordance with Paragraph 2-51.
2-51. INSTALLATION OF AIR FILTER. After cleaning and inspection, install the filter element and cover in
reverse order of removal instructions.
2-52. PROPELLER.
2-53. SERVICING PROPELLER. The spinner, back plate and propeller surfaces should be cleaned and
inspected frequently for nicks, scratches, corrosion and cracks. Minor nicks and scratches may be removed as
found in Section VIII or VIIIA. The face of each blade should be painted when necessary with a flat paint to
retard glare. To prevent corrosion, wipe surfaces with a light oil or wax.
In addition, propellers should be inspected for grease or oil leakage and freedom of rotation on the hub
pilot tube. To check freedom of rotation, rock and blade back and forth through the slight freedom allowed by
the pitch change mechanism. Lubricate the propeller at 100-hour intervals in accordance with the Lubrication
Chart.
Additional service information for the propeller may be found in Section VIII or VIIIA.
2-54. FUEL SYSTEM.
2-55. SERVICING FUEL SYSTEM. At intervals of 50-hours or 90 days, whichever comes first, clean the fuel
strainer screen, located in the fuel bowl mounted on the lower left side of the firewall, and on PA-28R-201
only, clean the screen in the inlet side of the injector. Remove and clean the fuel strainer screen in accordance
with the instructions outlined in Section IX. Additional fuel system service information may also be found in
Section IX. Inspection intervals of the various fuel system components may be found in Section III.
Revised 12/ 11/78
1B19
*CHEROKEE ARROW III SERVICE MANUAL
HANDLING AND SERVICING
Summary of Contents for ARROW III
Page 4: ...THIS PAGE INTENTIONALLY LEFT BLANK 1A4...
Page 12: ...THIS PAGE INTENTIONALLY LEFT BLANK 1A12...
Page 94: ...Figure 4 2 Wing Installation Revised 2 13 89 1D22 CHEROKEE ARROW III SERVICE MANUAL STRUCTURES...
Page 171: ...lH3 INTENTIONALLY LEFT BLANK...
Page 172: ...lH4 INTENTIONALLY LEFT BLANK...
Page 286: ...THIS PAGE INTENTIONALLY LEFT BLANK Revised 2 13 89 2A8...
Page 528: ...INTENTIONALLY LEFT BLANK 2K10 THRU 2L24 2K10...
