R  CAUTION : DO NOT USE SHARP AND/OR METALLIC TOOLS OR OBJECTS TO_______ 
R  REMOVE/INSTALL THE WINDSHIELD. DO NOT USE A LEVER AGAINST THE 
R  EDGE OF THE WINDSHIELD BECAUSE IF YOU DO, YOU WILL CAUSE DAMAGE 
R  TO THE WINDSHIELD. 
R  (1) Use vacuum handles (55) to put the windshield panel (14) in position 
R  in its housing. 
R  NOTE : Two persons are necessary to install the windshield panel:____ 
R  - One person out of the aircraft to hold the windshield panel, 
R  - A second person in the aircraft with one arm through the 
R  sliding window and one hand on the inner face of the 
R  windshield panel to put it in the lateral frame. 
R  (2) Install the adjustment tools (50) and (54) on the upper part of the 
R  windshield with the pins (52). 
R  (3) Operate the suction cups of the adjustment tools (50) and (54) to 
R  hold the windshield panel with the tool. 
R  (4) Put the windshield panel in position with the knurled screws (51) and 
R  the knurled nut (53). 
R  (5) When the windshield panel is correctly adjusted, remove the R/I FRONT 
R  WINDOW TOOL (98F56103000000). 
R  Subtask 56-11-11-914-054 
R  B. Sealant Application 
R  (Ref. Fig. 405/TASK 56-11-11-991-015) 
R  (1) Apply a bead of SEALANTS (Material No. 09-016) or SEALANTS (Material 
R  No. 09-053) at the intersection area between: 
R  - the frame structure and the lower retainer, 
R  - the frame structure and the upper retainer, 
R  - the front retainer and the upper and lower retainers. 
R  NOTE : If you use PR1436GB-ND1/2 at 23deg.C, the application time is____ 
R  1/2 hour and the cure time is 24 hours. If you use 
R  PR1436GB2-NA at 23deg.C, the application time is 2 hours and 
R  the cure time is 30 hours. If you use PR1436GB4-NA at 23deg.C, 
R  the application time is 4 hours and the cure time is 40 hours. 
R  If you use DAPCO 72 at 23deg.C, the application time is 1/4 
R  hour and the cure time is 2 1/2 hours.

R  (2) If the sealant cure time is not sufficient before aircraft take-off, 
R  do the procedure below: 
R  CAUTION : BEFORE YOU APPLY THE TAPE, MAKE SURE THAT THE SEALANT IS_______ 
R  NOT TACKY. IF IT IS TACKY, THE TAPE CAN CAUSE DAMAGE TO THE 
R  SEALANT. 
R  CAUTION : WHEN YOU APPLY THE TAPE, MAKE SURE THAT THERE ARE NO_______ 
R  BUBBLES. THIS WILL HELP TO PREVENT THE REMOVAL OF THE TAPE 
R  DURING FLIGHT. 
R  (a) Put a strip of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-
R  052) on the intersection areas. 
R  NOTE : If you use PR1436GB-ND1/2 at 23deg.C, the sealant is not____ 
R  tacky after 10 hours. If you use PR1436GB2-NA at 23deg.C, 
R  the sealant is not tacky after 16 hours. If you use 
R  PR1436GB4-NA at 23deg.C, the sealant is not tacky after 28 
R  hours. If you use DAPCO 72 at 23deg.C, the sealant is not 
R  tacky after 40 minutes. 
R  (b) Do a visual check of the intersection areas between each flight. 
R  (c) Remove BONDING AND ADHESIVE COMPOUNDS (Material No. 08-052) after 
R  the sealant cure time. 
R  NOTE : During the flight, temperatures are under 10deg.C and the____ 
R  sealants do not dry. The sealant cure times given above do 
R  not include the flight hours. 
R  Subtask 56-11-11-420-058 
R  C. Installation of the Lower Retainer 
R  (Ref. Fig. 402/TASK 56-11-11-991-002, 406/TASK 56-11-11-991-016) 
R  (1) Put the lower retainer (12) in position and install two wooden shims 
R  between the lower retainer (12) and the windshield (14). 
R  (2) With a non metallic lever, lift the lower retainer (12) and install 
R  two wooden shims between the lower retainer (12) and the aircraft 
R  structure. 
R  (3) Apply SPECIAL MATERIALS (Material No. 05-002) below the head of the 
R  five hex head bolts (13). 
R  (4) Install the five washers (28), the five hex head bolts (13) and 
R  lightly tighten them.