Piper SARATOGA PA-32-301 Maintenance Manual page 444

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
FLIGHT COMPARTMENT.
WINDSHIELD.
REMOVAL OF WINDSHIELD.
1. Remove the collar molding from around the bottom of the windshield and the trim strip from
between the windshield halves by removing the attaching screws.
2. Remove the windshield by raising the lower portion of the windshield and carefully pulling it out and
downward to release the top and side edges.
- NOTE -
A damaged windshield should be saved since it can be used as a
pattern for drilling required holes in the new windshield.
3. Clean the old tape and sealer from the windshield channels, strips and divider post.
INSTALLATION OF WINDSHIELD. (Refer to Figure 56-1.)
1. Be certain that the new windshield outside contours are the same as that of the old windshield. It may
be found that it is necessary to cut or grind the new windshield to acquire the proper dimensions.
2. Apply black vinyl plastic tape around the outer edges of the entire windshield.
3. Apply PMS-K0003 Type I vinyl foam tape or equivalent overthe plastic tape. completely around the
edges of the windshield.
4. Apply PMS-C1012 sealant or equivalent under the edge of the moldings and trim strips.
5. Place the windshield in position for installation and slide the windshield aft and up into place, using
caution not to dislocate the tape around the edges. Allow clearance between the two windshields at the di\ ider
post for expansion.
6. Lay sealant at the bottom and center (inboard) of the windshield in the hollow between the outside
edge and channel.
7. Lay a small amount of sealant under the center trim strip, install and secure.
8. Lay black vinyl tape on the underside of the collar molding, install and secure.
9. Seal with sealant any areas around windshield that may allowwaterto penetrate past the windshield.
10. Remove excess exposed sealer and tape.
CABIN.
SIDE WINDOWS.
The PA-32-301 301T airplane is equipped with single pane side windows. For removal and installation of
the windows. refer to the following instructions.
56-20-01
Page 56-01
2H7
Revised: August 9. 1984