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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.
GROUND HANDLING AND SERVICING HANDBOOK A ZONE 711 02 01 A ZONES 721 731 CUT ACROSS TREAD RIBS 1/8 OF THE CIRCUNFERENCE 02 1 in SIDEWALL BEAD TREAD WORN TO ANY GROOVE BASE 01 CHINE TOP FABRIC APPLICABLE ONLY TO THE NLG TIRE. TREAD TREAD GROOVE CASING PLIES (FABRIC) A TYPICAL TREAD RIB RIB UNDERCUTTING 1/8 OF THE CIRCUNFERENCE = 8.2 in (210 mm) FOR MAIN LANDING GEAR OR 5.9 in (150 mm) FOR NOSE LANDING GEAR TREAD OR SIDEWALL BULGE EM500ENGHSH320020B.DGN 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. EFFECTIVITY: ALL Nose and Main Wheel Tires - Inspection Figure 601, Sheet 1 Copyright © by EMBRAER S.A. - All rights reserved - See title page for details. 32-45-00-210-801-A/600 Page 603 Rev.10 - AUG 27/10
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