SB 500-25-009, REV B

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MANDATORY www.eclipseaerospace.net SERVICE BULLETIN NUMBER: SB 500-25-009, REV B MODEL: ECLIPSE EA500 SUBJECT: FORWARD CENTER FLOOR PANEL MODIFICATION 1. PLANNING INFORMATION A. Effectivity Aircraft Serial Numbers 000105 through 000112, 000116 through 000119, 000121 through 000122, 000125 through 000300. Aircraft Serial Numbers 000001 through 000104, 000113 through 000115, 000120, 000123 through 000124 modified by SB 500-99-002. B. Reason To improve clearances between the Center Forward Floor Panel and the Left Main Cabin Wiring Harness Revision B changes: Extended effectivity to 000300 C. Description This Service Bulletin provides the procedure to rework the Forward Center Floor Panel to provide more clearance for the Left Main Cabin Wiring Harness. D. Relevant Publications None E. Compliance Eclipse Aerospace Inc. considers this to be a mandatory modification that must be accomplished at the next 300 hour / 24 Month Inspection. Compliance with revision A of this Service Bulletin constitutes compliance with revision B. F. Approval This Service Bulletin is based on engineering data that is FAA-approved, and the modification herein complies with the applicable regulations. G. Labor Requirements The following information is for planning purposes only. (1) Estimated labor hours to perform: Suggested number of personnel: 1 Job Setup: 8 Hours Center Forward Floor Panel Modification: 2 Hours Job Close up: 14 Hours Total labor hours: 24 The above is an estimate based on properly equipped and experienced personnel complying with this Service Bulletin. Actual labor hours may vary depending on workforce experience, concurrent maintenance, discovery of other discrepancies, etc. Issued: 9 Nov 2011 – Rev B COPYRIGHT © 2011 ECLIPSE AEROSPACE INC. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form or by means, electronic, mechanical, photocopy, recording or otherwise without prior written permission by Eclipse Aerospace Inc.. SB 500-25-009 1 of 8 MANDATORY SERVICE BULLETIN (2) Qualification of personnel: • A person properly authorized to perform aircraft maintenance under 14 CFR 43 or equivalent approved by the Civil Aviation Authority having jurisdiction. H. Weight and Balance Change None I. Electrical Load Data Change None J. Software Accomplishment Summary Not applicable K. References Aircraft Maintenance Manual (AMM) P/N 06-117751, latest revision Wiring Repair Manual (WRM) P/N 06-120792 L. Publications Affected None 2. MATERIAL INFORMATION A. Materials There are no parts required for this Service Bulletin. B. Consumables The following consumables are required for this Service Bulletin. Material Specification Use Epxoy 3M Scotch-Weld 2216 B/A Epoxy Adhesive or Hysol EA 934NA Epoxy Paste Adhesive Floorboard Edge Fill Aerodynamic Smoothing Sealant PRC Desoto PR-2050 or equivalent Nose Access Panel Installation Conformable Teflon Tape 76025A691 or equivalent Nose Access Panel Installation Carpet Tape Scotch 3M CT 1020 or equivalent Carpet Installation Strap, Tiedown MS3367-2-0 or equivalent Duct Installation Strap, Tiedown MS3367-1-9 or equivalent Forward Evaporator Drain Tube Installation Threadlocker Loctite 242 or equivalent Parking Brake Valve Control Cable Installation Oil General Purpose Light Parking Brake Valve Control Cable Installation Issued: 9 Nov 2011– Rev B COPYRIGHT © 2011 ECLIPSE AEROSPACE INC. All rights reserved SB 500-25-009 2 of 8 MANDATORY SERVICE BULLETIN C. Tooling The following special tooling/support equipment is required to accomplish this Service Bulletin. Nomenclature Specification Use Seat Foot Release Cable Tool EAI, 9000-2521275 Seat Removal and Installation R134 Service Cart RHS 780 or equivalent Air Conditioning Servicing Electronic Refrigerant Leak Detector Snap-on ACT730 or equivalent Air Conditioning Servicing D. Interchangeability/Intermixability of Parts None E. Part Re-identification Remark part per Accomplishment Instructions 3. ACCOMPLISHMENT INSTRUCTIONS A. Job Set-up (1) Make the aircraft safe for maintenance. Refer to AMM 20-00-01 MAKE SAFE FOR MAINTENANCE. (2) Remove the Floor Panel, Forward Center Cockpit - 122 BZ as follows: (a) Remove the pilot and copilot seats as necessary to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 25-11-10 - COCKPIT SEAT - REMOVAL. (b) Remove the carpet as necessary to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 25-21-40 - CARPET ASSEMBLY - REMOVAL. (c) Remove the transition strip as necessary to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 25-21-25 - TRANSITION STRIPS - REMOVAL. (d) Remove the Throttle Quadrant to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 25-10-01 - THROTTLE QUADRANT - REMOVAL. (e) Remove the Center Console Assembly including left and right Console Kick Panels, Fire Extinguisher and Parking Brake Cable, to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 25-11-20 - COCKPIT PANELS - REMOVAL. (f) Remove the forward evaporator module to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 21-50-20 - FORWARD EVAPORATOR MODULE - REMOVAL. (g) Remove the Floor Panel, Aft Center Cockpit - 121 CZ to gain access to the Floor Panel, Forward Center Cockpit - 122 BZ. Refer to AMM - 25-11-30 - COCKPIT FLOOR PANELS - REMOVAL. (h) Remove and retain the screws (3, Figure 1) that attach the Floor Panel, Forward Center Cockpit - 122 BZ (2, Figure 1) to the structure (1, Figure 1). (i) Remove the Floor Panel, Forward Center Cockpit - 122 BZ (2, Figure 1) from the aircraft. Issued: 9 Nov 2011– Rev B COPYRIGHT © 2011 ECLIPSE AEROSPACE INC. All rights reserved SB 500-25-009 3 of 8 MANDATORY SERVICE BULLETIN 1 2 (4X) 3 50101362A A A Cockpit Floor Panels Figure 1 Issued: 9 Nov 2011– Rev B COPYRIGHT © 2011 ECLIPSE AEROSPACE INC. All rights reserved SB 500-25-009