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Cessna Index >  

A-4 STC'd Windshield Installation Instructions

INSTRUCTIONS A-4

One Piece Windshield Installation
(STC'd Elimination of Center Strip)

PAGE INDEX:
Used on Chart
Materials Needed
Instructions
 
Other Pages
Cessna Menu
170 Index
172 Index
175 Index
180 Index
182 Index
185 Index
205 Index
206 Index
210 Index
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This File as PDF:

52 KB
 
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Cessna Model #'s
Part # W-, W/T- or W/G-
STC #
Serial #'s Weight and balance information
Weight # Moment in. #
170, A & B
2055
SA210GL
ALL + 3.8 + 65
172 & A
2055
SA211GL
28000 ~ 47746 + 3.8 + 65
172 B & C
2056
SA211GL
47747 ~ 49544 + 3.8 + 65
175, A, B, & C
2056
SA212GL
55001 ~ 57119 + 3.8 + 65
180
2072
SA471GL
30000 ~ 31261 + 3.8 + 65
180, 180A
2072
SA471GL
31261 ~ 50355 No change No change
180, 180B, 180C, 180D, 180E, 180F, 180J, 180K
2073
SA471GL
50356 & up No change No change
182, 182A,
2072
SA301GL
33000 ~ 51556 No change No change
182B, 182C, 182D
2073
SA301GL
51557 ~ 53598 No change No change
182E, 182F, 182G
2071
SA301GL
53559 ~ 55844 +4.4 + 75
185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 
2073
SA472GL
0001 & up No change No change
210-5 (205), 210-5A (205A)
2065
SA393GL
All +4.4 + 75
206, &  U206, 
2065
SA392GL
0001 ~ U0437  +4.4 + 75
P206
2065
SA392GL
P0001 ~ 0160 +4.4 + 75
210
2065
SA393GL
57841 ~ 58715 + 4.4 + 75


 

Materials:

1.    1 Windshield as noted above
2.    4 felt strips (1pc M-1001-2 46.5", 2 pcs M-1001-1 18.5", 1 pc M-1001-1 76.5")
3.    4 elastomer Bushings ( M-1001-1 )
4.    4 pcs, AN-526-632R10 screws
5.    4 pcs, AN-364-632 nuts
6.    Sealant - optional - not supplied
7.    Miscellaneous hardware ( rivets, etc. ) - not supplied  
 

Instructions (removal of Cessna Windshield Center strip)

1.    Remove center strip ( both inner and outer)

2.    Remove lower fairing and wing root fairings

3.    remove old windshield by sliding the windshield forward out of the top and side channels

4.    Clean channels and mounting surfaces that will contact the windshield. straighten and repair as required. any nicks or distorted metal that will contact the windshield.

5.    Place the new windshield in position and check the fit of the windshield - trim if required. See trimming instructions.

6.    Again Place the windshield in position and temporarily attach the lower fairing and wing fairings so that the windshield is held in the exact final position.

7.    Remove the protective paper from the double stick tape in the drill template and carefully locate the template on the top of the windshield and over the top of the upper channel, aligning the template with the marks on the windshield. Check the edge distance of the holes to the edge of the skin- it should be at least 1/4 inch. Mark the hole locations carefully. A No. 27 drill may be used to start the hole in the skin and thus leaving a mark. It is important that this step be done very carefully as the alignment of the holes depends on it.

8.    Remove the template and the windshield and finish drilling (with a No. 27 drill) the 4 holes thru the outer and inner walls of the top channel as marked. Remove any burrs and chips that the drilling created.

9     Install the 4 bushings in the holes and attach the self-adhesive felt strips in the windshield. Cut small holes thru the felt to allow the screws to go through the 4 bushings.

10   Place the windshield in position and install the 4 screws and nuts. Tighten the screws lightly, they should be only finger tight and should not distort the metal skin. Over-tightening can cause crazing and premature failure of the windshield.

11   Reinstall the lower fairing and wing root fairings. (Note: sealant may be used in addition to the felt to help prevent leakage.)

12   Fill the holes remaining from the center strip attachment points using the screws and nuts (AN-526 and AN 364) or rivets.

13   Touch up or paint as needed.

14   Relocate compass as desired. A C-2400L4P compass may be located on top of the instrument panel or a standard compass in the instrument panel.

15.   New Weight and balance information (see above)

16.   Fill out 337 form

NOTE: Some models have the outside air temperature gauge through the center strip of the windshield - this can be moved to the wing root air vent as is common in other Cessna models.  

 
This step shows the method suggested for locating the holes drilled in the windshield to be drilled in the skin of the aircraft
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This picture shows a cut-away section of a hole to show how to assemble thie windshield into the aircraft.
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.This shows a typical hole spacing
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A-4 Cessna 1 Piece Windshield Conversion