Embraer EMB-505 Phenom Service Manual page 184

(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) If balance is affected because of wet braking flat spot or dry braking
flat spot.
NOTE: Uneven wear - if you find irregular wear, the tire can be dis-
D. Job Close-Up
(1) Put the aircraft back to its initial condition.
EFFECTIVITY: ALL
Copyright © by EMBRAER S.A - All rights reserved - See title page for details.
assembled and turned in the opposite direction if there is
no fabric that can be seen.
GROUND HANDLING AND
SERVICING HANDBOOK
32-45-00-210-801-A/600
Rev.03- FEB 24/11
Page 602