Boeing 737-600 - Page 1942

E
3
C
C
4
E
FWD
C-C
3
4
NOSE
RADOME
GAP
LOCATION B1
NOSE RADOME
INNER SURFACE
GAP AT LOCATION B1 IS 0.046 TO 0.216 INCH (1.70 TO 5.49 mm)
ONLY MEASURE THE GAP WHEN NOSE RADOME IS FULLY CLOSED.
NOSE RADOME INNER SURFACE
FUSELAGE
L35246 S0006581058_V3
Nose Radome Installation
Figure 401/53-52-00-990-802 (Sheet 3 of 3)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-52-00
Page 409
D633A101-ILF Oct 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
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