EMB-500 - Embraer

GROUND HANDLING AND
SERVICING HANDBOOK
HARD COPY IS UNCONTROLLED. ONCE PRINTED, THIS PAGE MUST NOT BE RETAINED FOR FUTURE REFERENCE.
BEFORE USING, MAKE SURE THIS HARD COPY IS THE LATEST ISSUE.
(j) Heat damage in bead.
(k) Impact break.
(l) One or more of the conditions that follow with exposed fabric:
1. Groove cracking.
2. Dry braking flat spot.
3. Tread chunking.
4. Chevron cutting.
5. Sidewall crack.
6. Sidewall cut or snag.
7. Radial or circumferential crack.
(m) Balance affected because of wet braking flat spot or dry braking flat spot.
NOTE: Uneven wear - if you find irregular wear, the tire can be
disassembled and turned in the opposite direction if there
is no fabric that can be seen.
D. Job Close-Up
(1) Put the aircraft back to its initial condition.
EFFECTIVITY: ALL
32-45-00-210-801-A/600
Page 602
Rev.10 - AUG 27/10
Copyright © by EMBRAER S.A. - All rights reserved - See title page for details.