Textron Aviation 208 - Page 7

Figure 202 : Sheet 1 :
NOTE 3:
THE LIFT TRANSDUCER MOUNTING FACE MUST BE EVEN WITH OR INSET
NO MORE THAN 0.010 INCH FROM THE POROUS PANEL OUTER FACE.
APPLY A FILLET SEAL AROUND THE MOUNTING PLATE WITH U060031 SEALANT.
NOTE 2:
INSTALL THE NAS1149FN832P WASHER UNDER THE NUT.NOTE 1:
2610T7004
AA2601T535
A73401
A
A
VIEWA−A
MS21044N08
NUT
NAS1149FN832P
WASHER
(4 EACH REQUIRED)
(NOTE 1)
MS24694−S6
SCREW
B
WING LEADING EDGE
B
LEFT MID−WING
POROUS PANEL
A
NAS1149FN816P
WASHER
NAS1149FN832P
WASHER
VANE
MS24694−S5
SCREW
LIFT
TRANSDUCER
Model 208/208B Maintenance Manual (Rev 33)
27-31-00-2 (Rev 28)
Copyright © Textron Aviation Inc. Page 7 of 8
Retain printed data for historical reference only. For future maintenance, use only current data.
Print Date: Mon May 08 12:14:36 CDT 2023