Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 1254 / 1956

PAGE 8
Feb 28/07
6J22
56-10-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
FILL GAP BETWEEN WINDOW
AND HINGE HALF WITH
DEXTER HY S OL 9446 ADHE S IVE
THI S S URFACE OF
HINGE HALF
MU S T BE BONDED FLU S H
AGAIN S T WINDOW
S ILICONE
RUBBER
TUBE
APPLY PR1422-B4
S EALANT HERE
S TORM WINDOW A SS Y.
- BOND HINGE TO WINDOW PRIOR
TO BONDING LATCH PIN A
SS Y.
- MAINTAIN .0 3 0 INCH MINIMUM GAP
BETWEEN S TORM WINDOW RETAINER
AND PILOT' S S IDE WINDOW.
- CENTER HINGE HALF IN THE CUTOUT
AREA
S O THAT IT DOE S NOT
RIDE INTO CORNER RADII.
A
A
B
B
S ECTION
B-B
VIEW OUT
FWD
NOTE S : 1. BOND WITH DEXTER HY S OL 9446.
2. BOND WITH PR-1422.
3 . IF S TORM WINDOW FAIL S “WATER LEAK CHECK, ” ADD UP TO 0.15 RTV-7 3 2 (P/N 279-195) BETWEEN
S EAL AND WINDOW RETAINER AND PERFORM “ WATER LEAK CHECK ” AGAIN.
S ECTION
A-A
NOTE 1
NOTE 1
(BEFORE BONDING, REMOVE KNOB FROM
S TORM WINDOW
A SS Y. AND CENTER LATCH PIN TO THE .5 IN. DIAMETER HOLE
IN THE S TEEL RETAINER. PIN MU S T BE CENTERED WITHIN
.015 INCH. AFTER BONDING, WINDOW MU S T OPERATE
S MOOTHLY WITHOUT DRAG OR BINDING.)
WA S HER( S )
(TWO MAX.)
LATCH PIN
A
SS Y.
NOTE 2
NOTE 2
NOTE 2
100 8 77 J
100 8 79 H
IN S TALL M S 20470AD 3 - 3 RIVET
IN EACH END OF HINGE WITH
LOCTITE 420 TO RETAIN HINGE PIN
.06/.12 INCH FILLET S EAL WITH PR-1422
Storm Window
Figure 5
Effectivity
4636077 and up