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ECLIPSE Service Bulletin

ECLIPSE 550 · Service Bulletins

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Overview

This document is a Service Bulletin for the Eclipse 550 aircraft, specifically addressing the inspection of the Wheel Speed Transducer (WST) connector pins. It outlines mandatory compliance requirements, inspection procedures, and repair instructions if necessary.

  • Mandatory inspection for specific aircraft serial numbers.
  • Inspection of WST connector pins is required at the next 300 Hour/24 month Inspection.
  • Revision B updates wire crimping specifications.
  • Estimated labor time for inspection is 1 hour, with potential additional time for repairs.
  • No modifications to the approved configuration are included.
  • Compliance record must be submitted to Eclipse Aerospace after completion.

Document

Source

Originally published by eclipse.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Service Bulletins
Year
·
2015
File size
·
827 KB
Publisher
·
eclipse.aero
Language
·
en
About this document
What is the ECLIPSE Service Bulletin?

The ECLIPSE Service Bulletin is a service bulletins for the ECLIPSE 550, dated 2015.

Where does the ECLIPSE Service Bulletin come from?

This copy of the ECLIPSE Service Bulletin was originally published by eclipse.aero and is hosted on Sprinkle as a free, searchable reference copy.

What year was the ECLIPSE Service Bulletin published?

The ECLIPSE Service Bulletin — the ECLIPSE 550 service bulletins on file — is dated 2015.

Documentation completeness
1/7

Most owners only have the POH. Here's the essential set for the ECLIPSE 550.

  • Pilot's Operating Handbook / AFM
  • Checklist
  • Maintenance Manual
  • Parts Catalog (IPC)
  • Systems & Wiring
  • Service Bulletins on file
  • Type Certificate (TCDS)

More ECLIPSE 550manuals & documents

In this document

Planning Information

Details the effectivity, reason for the bulletin, and compliance requirements for the inspection of WST connector pins.

Accomplishment Instructions

Provides step-by-step procedures for inspecting and repairing the WST connector pins.

Material Information

Lists materials, consumables, and tooling required for the inspection and repair process.

Labor Requirements

Estimates labor hours needed for inspection and potential repairs, along with personnel qualifications.

Record of Compliance

Instructions for documenting the completion of the service bulletin and notifying Eclipse Aerospace.

Export Control

Notes on the export regulations applicable to the commodities and technology involved.

Full document text

ECLIPSE Service Bulletin Issued: 19 March 2015 - Rev B SB 550-32-001 © 2015 ECLIPSE AEROSPACE, INC Page 1 of 6 NUMBER: SB 550-32-001, Rev B Mandatory MODEL: ECLIPSE 550® www.ECLIPSE.aero SUBJECT: Wheel Speed Transducer (WST) Connector Inspection 1. PLANNING INFORMATION A. Effectivity Aircraft Serial Numbers: 550-0263 to 550-0265, 550-0268 to 550-0280, and 550-0282 to 550-0284. B. Reason This Service Bulletin inspects the Wheel Speed Transducer (WST) connector pins. Revision B updates Figure 2 to reflect wire crimping specs. C. Description This Service Bulletin provides instructions on inspecting the Wheel Speed Transducer (WST) connector pins and repairs them if needed. D. Relevant Publications 06-123838 – Eclipse 550 AMM, current revision E. Compliance Eclipse Aerospace Inc. considers this to be a mandatory inspection that should be accomplished at the next 300 Hour/24 month Inspection. F. Approval This Service Bulletin contains no modification information that revises the approved configuration and therefore does not require governmental or other regulatory agency approval. G. Labor Requirements The following information is for planning purposes only. (1) Estimated labor hours to perform: Suggested number of personnel: 1 Inspection: 1.0 Hour Part Replacement, if needed: 2.0 hours Total labor hours: 3.0 Hours 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. (2) Qualification of personnel: • A person properly authorized under 14 CFR 43 to perform aircraft maintenance. ECLIPSE Service Bulletin Issued: 19 March 2015 - Rev B SB 550-32-001 © 2015 ECLIPSE AEROSPACE, INC Page 2 of 6 H. Weight and Balance Change N/A I. Electrical Load Data Change N/A J. Software Accomplishment Summary N/A K. References 06-123838 – Eclipse 550 AMM, current revision Document: IPC/WHMA-A-620, Requirements and Acceptance for Cable and Wire Harness Assemblies, (Document location: http://www.ipc.org) L. Publications Affected None M. Export Control These commodities, technology or software were exported from the United States in accordance with the Export Administration Regulations. These commodities, technology or software are intended for use only in the End User’s country. An export license from the U.S. Department of Commerce may be required before these products can be re-exported, transferred, transshipped on a non-continuous voyage, or otherwise disposed of in any other country, either in their original form or after being incorporated into an end item. Diversion of this end-item or its use contrary to any applicable U.S. government license or to U.S. law is prohibited. 2. MATERIAL INFORMATION A. Materials [1] Document is provided with this service bulletin. B. Consumables Per Q300-059 and Q300-060. C. Tooling Per Q300-059 and Q300-060. D. Interchangeability/Intermixability of Parts N/A E. Part Re-identification N/A F. Cost Contact Eclipse Aerospace Customer Care for cost information and availability. Part Number Description Qty Unit of Issue Q300-059 [1] Field Connector Inspection 1 EA. Q300-060 [1] Field Repair Instructions 1 EA. ECLIPSE Service Bulletin Issued: 19 March 2015 - Rev B SB 550-32-001 © 2015 ECLIPSE AEROSPACE, INC Page 3 of 6 3. ACCOMPLISHMENT INSTRUCTIONS A. Procedure (1) Make aircraft safe for maintenance. Refer to AMM 20-00-01- MAKE SAFE FOR MAINTENANCE. (2) Perform inspection of 32A33P01 and 32A34P01 WST connector pins per Q300-059. (3) If required, perform repair of the WST connector pins per Q300-060, Figure 1. WST Connector Pinout Figure 2. WST Crimp Examples ECLIPSE Service Bulletin Issued: 19 March 2015 - Rev B SB 550-32-001 © 2015 ECLIPSE AEROSPACE, INC Page 4 of 6 B. Close Up (4) If all other maintenance is complete, return aircraft to service. Refer to AMM 20-00-02-051-801 RETURN TO SERVICE (AFTER MAINTENANCE). C. Limitations and Procedures N/A D. Parts Disposition N/A 4. PART MARKING None. 5. RECORD OF COMPLIANCE Upon completion of this Service Bulletin, make an appropriate maintenance-record entry specifying the Service Bulletin number. 6. NOTIFYING ECLIPSE AEROSPACE On completing this service bulletin, the operator/maintainer shall complete the attached Compliance Record and send it to Eclipse Aerospace via regular mail, fax, or e-mail. Mailing Address Eclipse Aerospace Incorporated ATTN: Service Engineering 2503 Clark Carr Loop SE Albuquerque, NM 87106 Fax 1-505-241-8802 E-mail sbcompliance@eclipse.aero ECLIPSE Service Bulletin Issued: 19 March 2015 - Rev B SB 550-32-001 © 2015 ECLIPSE AEROSPACE, INC Page 5 of 6 [Intentionally Blank Page] ECLIPSE Service Bulletin Issued: 19 March 2015 - Rev B SB 550-32-001 © 2015 ECLIPSE AEROSPACE, INC Page 6 of 6 SERVICE BULLETIN COMPLIANCE RECORD MODEL __________ AIRPLANE S/N ____________ REG. NO. __________ TOTAL TIME ______ (HOURS) OWNER NAME: _____________________________________________________________________ ADDRESS: _________________________________________________________________________ _________________________________________________________________________ TELEPHONE NO. (___) ________________________ FAX NO. (___) ________________________ COMPLIANCE WITH SB 550-32-001, Rev B Description of Work Performed (Inspection | Modification | Repair | Option Installation | Defect or Damage Found, if applicable) ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________

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___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ ___________________________________________________________________________________________ DATE ______________ WORK PERFORMED BY _________________________________________ (PRINTED) _________________________________________ (SIGNATURE) COMPANY _________________________________________________________________________________ ADDRESS _________________________________________________________________________________ __________________________________________________________________________________ TELEPHONE ________________________ FAX ________________________ Field Connector Inspection Work Instructions for D202106 Work Order No.: _________ Finished S/N: ____________ FORM: Q300-059 REV. A APPROVED 02/03/2015 Page 1 Work Instructions Step No. Directions Tech QA 1 Gain access to connector at the end of the Wheel Speed Transducer (D201106) wire harness. N/A 2 Disconnect connector. Remove screws from Circular Strain Relief (M85049- 38S9N), Unscrew from mating connector (D38999-26FA98PN), and slide down Braided Shielding (100-001A171) to expose individual conductors. N/A Tools List Item No. Description MFG. Part No. QTY Suggested MFG. 1 Installation/Removal Tool M81969/14-10 or ZZ001208 1 QPL Document List Item No. Description Revision Qty. 1 Q300-060 latest 1 2 D202106 B 1 3 WHMA-A-620 any 1 Material List Item No. Description Part No. Qty. 1 Contact Pins, Connector, Size 20 M39029/58- 363 3 Field Connector Inspection Work Instructions for D202106 REV. B FORM: Q300-059 REV. A APPROVED 02/03/2015 Page 2 3 Using Installation/Removal Tool, remove Contact Pins (M39029/58-363) from Connector (D38999-26FA98PN) N/A 4 Inspect Crimp on Contact Pins (M39029/58-363) to requirements of IPC- WHMA-A-620 Class 2, specifically looking at location of crimp relative to Contact Pin. Field Connector Inspection Work Instructions for D202106 Work Order No.: _________ Finished S/N: ____________ FORM: Q300-059 REV. A APPROVED 02/03/2015 Page 3 5 If crimp is deemed acceptable, note below, re-install pins using Installation/Removal Tool per wiring diagram on drawing D202106 Rev. B, re- assemble Circular Strain Relief (M85049-38S9N), attach to Connector (D38999-26FA98PN) and re-connect connector. If deemed unacceptable, note below and execute Q300-060 for Field Repair Instructions. CRIMP DEEMED Acceptable: __________________ Unacceptable: ______________ COMPLETED: Signature: __________________ Date Completed: ______________ Field Repair Instructions Work Instructions for D202106 Work Order No.: _________ Finished S/N: ____________ FORM: Q300-060 REV. A APPROVED 02/03/2015 Page 1 Instruction to be used in conjunction with Q300-059, Field Connector Inspection Work Instructions for D202106. Work Instructions Step No. Directions Tech QA 1 Cut existing Contact Pins (M39029/58-363) off of conductors as near the Contact Pin as possible. N/A Tools List Item No. Description MFG. Part No. QTY Suggested MFG. 1 Crimp Tool M22520/1-01 or M22520/7-01 1 QPL 2 Turret M22520/1-04 or M22520/7-08 1 QPL 3 Installation/Removal Tool M81969/14-10 or ZZ001208 1 QPL Document List Item No. Description Revision Qty. 1 Q300-059 latest 1 2 D202106 B 1 3 WHMA-A-620 any 1 Material List Item No. Description Part No. Qty. 1 Contact Pins, Connector, Size 20 M39029/58- 363 3 Field Repair Instructions Work Instructions for D202106 FORM: Q300-060 REV. A APPROVED 02/03/2015 Page 2 2 Strip the individual conductors as required by IPC WHMA-A-620 N/A 3 Crimp new Contact Pins (M39029/58-363) onto conductors using Crimp Tool and Turret. Inspect to the requirements of IPC WHMA-A-620. Field Repair Instructions Work Instructions for D202106 Work Order No.: _________ Finished S/N: ____________ FORM: Q300-060 REV. A APPROVED 02/03/2015 Page 3 4 Insert Contact Pins (M39029/58-363) into Connector (D38999-26FA98PN) according to wiring diagram on drawing D202106 Rev. B. using Installation/Removal Tool. (Note: Installing all 3 pins loosely in connector before using installation tool will aid in this process) 5 Install Circular Strain Relief (M85049-38S9N) on connector (D38999- 26FA98PN) and reattach strain relief, attaching solder sleeve terminal to one side, using screws. Return to Q300-059 to complete. Field Repair Instructions Work Instructions for D202106 FORM: Q300-060 REV. A APPROVED 02/03/2015 Page 4 COMPLETED: Signature: __________________ Date Completed: ______________