EasyManuals Logo

Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
752 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #516 background imageLoading...
Page #516 background image
FLIGHT COMPARTMENT.
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 necessary to cut or grind the new windshield to acquire the proper dimensions.
2. Apply Behr-Manning vinyl foam tape number 560 or equivalent, completely around the edges of the
windshield
3. Apply Behr-Manning sealant number PRC 5000 or equivalent under the edge of the moldings and trim
strips.
4. 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 divider
post for expansion.
5. Lay sealant at the bottom and center (inboard) of the windshield in the hollow between the outside
edge and channel.
6. Lay a small amount of sealant under the center trim strip, install and secure.
7. Lay black vinyl tape on the underside of the collar molding, install and secure.
8. Seal with sealant any areas around windshield that may allow water to penetrate past the windshield .
9. Remove excess exposed sealer and tape.
CABIN.
REMOVAL OF SIDE WINDOWS.
The PA - 2 8 RT-201/201T airplanes are equipped with single pane side windows. For removal of these
windows, the following instructions may be used:
1. Remove the retainer molding from around the window by removing the attachment screws.
56-20-01
Page 56-01
Revised: July 24, 1981
2J21
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Piper Arrow IV Turbo and is the answer not in the manual?

Piper Arrow IV Turbo Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelArrow IV Turbo
Horsepower200 hp
Seating Capacity4
Landing GearRetractable tricycle
Range773 nautical miles
Service Ceiling20, 000 ft
Fuel Capacity72 gallons
Propeller2-blade constant speed
Max Takeoff Weight2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)55 knots
Rate of Climb1, 000 ft/min

Related product manuals