SERVICE BULLETIN NUMBER: SB 500-34-019, REV C

Heater Verification Test Procedure P1149, Rev E, Section 3, Line 12 (T1 test). (a) On MFD, scroll to ICE synoptic page by using the lower left/right knob. Press the PITOT/ STATIC softkey to select ON. (b) Using left/right lower knob on MFD, scroll to the ECB synoptic page. Press ECB BY SYSTEM softkey and using outer knob scroll to ICE PROT. Press inner knob to select. Using outer knob, scroll to ECB - L PITOT HEAT (BATTERY) and press the RESET softkey followed by the CONFIRM RESET softkey. (c) Perform Harco Labs, Inc, Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E starting at Section 3, Line 12. Issued: 20 Aug 2008— Rev C SB 500-34-019 3 of 6 ALERT SERVICE BULLETIN (d) After test is complete, collar ECB by using left/right lower knob on MFD, scroll to the ECB synoptic page. Press ECB BY SYSTEM softkey and using outer knob scroll to ICE PROT. Press inner knob to select. Using outer knob, scroll to ECB - L PITOT HEAT (BATTERY) and press the COLLAR softkey followed by the CONFIRM COLLAR softkey. NOTE: If T4 test is required, perform steps (1)(a) and (1)(b) to power on the pitot/AOA heater, then proceed to Harco Labs, Inc, Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E, Section 3, Line 21. After T4 test is complete, perform step (d) for turning off power to pitot/AOA heater. (2) Right Pitot/AOA Probe Test Supplements Harco Labs, Inc, Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E, Section 3, Line 12 (T1 test). (a) On MFD, scroll to ICE synoptic page by using the lower left/right knob. Press the PITOT/ STATIC softkey to select ON. (b) Using left/right lower knob on MFD, scroll to the ECB synoptic page. Press ECB BY SYSTEM softkey and using outer knob scroll to ICE PROT. Press inner knob to select. Using outer knob, scroll to ECB - R PITOT HEAT (R FWD Bus) and press the RESET softkey followed by the CONFIRM RESET softkey. (c) Perform Harco Labs, Inc, Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E starting at Section 3, Line 12 (T1 test). (d) After test is complete, collar ECB by using left/right lower knob on MFD, scroll to the ECB synoptic page. Press ECB BY SYSTEM softkey and using outer knob scroll to ICE PROT. Press inner knob to select. Using outer knob scroll to ECB - R PITOT HEAT (R FWD Bus) and press the COLLAR softkey followed by the CONFIRM COLLAR softkey. NOTE: If T4 test is required, perform steps (2)(a) and (2)(b) to power on the pitot/AOA heater, then proceed to Harco Labs, Inc, Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E, Section 3, Line 21. After T4 test is complete, perform step (d) for turning off power to pitot/AOA heater. C. Job Close-Up (1) On MFD scroll to ICE synoptic page by using the lower left/right knob, press the PITOT/ STATIC softkey to select AUTO. (2) Using left/right lower knob on MFD, scroll to the ECB synoptic page. Press ECB BY SYSTEM softkey and using outer knob scroll to AVIONICS. Press inner knob to select. Using outer knob, scroll to select ECB and press the RESET softkey followed by the CONFIRM RESET softkey for the following ECBs. • ECB - DEICE MANIFOLD HTR (R AFT Bus) • ECB - L PITOT HEAT (BATTERY) • ECB - R PITOT HEAT (R FWD Bus) • ECB - L STATIC HEAT (BATT Bus) • ECB - L STATIC HEAT (R FWD Bus) • ECB - R STATIC HEAT (L FWD Bus) • ECB - R STATIC HEAT (R FWD Bus) • ECB - STBY PITOT HEAT (L FWD) • ECB - L WINDSHIELD HEAT (L AFT Bus) • ECB - R WINDSHIELD HEAT (R AFT Bus) Issued: 20 Aug 2008— Rev C SB 500-34-019 4 of 6 ALERT SERVICE BULLETIN (3) Power down the aircraft by setting the SYS BATT and START BATT switches to OFF and the BUS TIE to OPEN. (4) Remove external electrical power. Refer to AMM-24-40-00. (5) Replace probes that fail to meet the pass criteria in Harco Labs, Inc, Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E. Refer to EA500 Illustrated Parts Catalog (IPC) for part numbers and AMM 34-10-10 for removal and Installation procedures. NOTE: Replacement of the failed probes can be delayed for 50 hours or 90 days, which ever comes first from the issue date of this SB for aircraft with Standby Pitot/Static Probes P/N 100564-18. (6) Remove all tools, equipment and unwanted material from the work area. (7) If all other maintenance is complete, return the aircraft to service. Refer to AMM-20-00-02. D. Limitations and Procedures None E. Parts Disposition Return defective probes to Eclipse Aviation. F. Cost Parts and Labor will be supplied by Eclipse Aviation Corporation at no charge to the aircraft owner. This Service Bulletin must be accomplished at an Eclipse Aviation Service Center or Eclipse Aviation Designated Service Center. 4. RECORD OF COMPLIANCE Upon completion of this Service Bulletin, make an appropriate maintenance-record entry specifying the Eclipse Service Bulletin number, Harco Labs, Inc, SB-34-10-10-001, Rev F – Pitot/AOA Probe 100435-X-() and Harco Labs, Inc Pitot AOA Probe Internal Tubing Heater Verification Test Procedure P1149, Rev E. 5. NOTIFYING ECLIPSE AVIATION On completing this service bulletin, the operator/maintainer shall complete the attached Compliance Record and send it and a copy of the completed Harco Test Procedure P1149 Data Sheet # A-1 or B-1 (which ever is applicable to the aircraft) to Eclipse Aviation via regular mail, fax, or e-mail. MAILING ADDRESS Eclipse Aviation Corporation ATTN: Customer Care 2503 Clark Carr Loop SE Albuquerque, NM 87106 Fax 1-505-241-8802 E-mail customercare@EclipseAviation.com Issued: 20 Aug 2008— Rev C SB 500-34-019 5 of 6 SERVICE BULLETIN COMPLIANCE RECORD SB 500-34-019, Rev C: Pitot/AOA Probe Inspection/Test MODEL _________ AIRPLANE S/N ________ REG. NO. _________ TOTAL TIME ______ (HOURS) OWNER NAME: ______________________________________________________________________ ADDRESS: ______________________________________________________________________ ______________________________________________________________________ TELEPHONE NO. (___) __________________________ FAX NO. (___) ______________________ COMPLIANCE WITH SB 500-34-019, Rev C Description of Work Performed (Inspection | Modification | Repair | Option Installation | Defect or Damage Found, if applicable) Left Pitot/AOA Probe S/N:___________________________________________________________ Right Pitot/AOA Probe S/N:__________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ DATE _______________ WORK PERFORMED BY ____________________________________________________________ (PRINTED) __________________________________________________________ (SIGNATURE) COMPANY __________________________________________________________ ADDRESS __________________________________________________________ __________________________________________________________ TELEPHONE ________________________________ FAX__________ ____________________