Emergency Exit Installation Diagram - Piper PA-44-180 SEMINOLE Maintenance Manual

6
6
4,5
3,5
3,4,5
A - A
2313
B
5
1
NOTES:
1. FILL ALL GAPS AND HOLES BETWEEN THE SILLS AND LONGERON WITH PMS-C1012 SEALANT COMPOUND
2. NEOPRENE SEAL BONDED TO DOOR SILLS WITH NEOPRENE RUBBER ADHESIVE (PMS-C1002). SEE CHART 9105.
3. COVER CONTACTING SURFACE WITH VINYL CHLORIDE COPOLYNER FILM (SARAN-48 GAUGE TYPE B) MIL-P-6264B.
4. WHEN THE ADJUSTMENT OF DOOR IS COMPLETED TRIM THE EXCESS POLYMER FILM FROM THE INSIDE AND OUTSIDE OF THE
INSTALLATION.
5. FILL EXTERIOR GAPS BETWEEN THE DOOR AND FUSELAGE WITH PMS-C1012 SEALANTS COMPOUND.
6. FOR WINDOW SEALING AND INSTALLATION INFORMATION, REFER TO CHAPTER 56.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3,4,5
2
3,5
6
6
B - B
B
Figure 52-3. Emergency ExitInstallation
3B2
6
C - C
5
A
A
1
2
6
3,4,5
D - D
C
5
C
D D
TINNED COPPER WIRE
AWG 26, .0159 DIA.
5 2 - 2 1 - 0 1
Page 52-07
Revised: May 15, 1989