OPTIONAL SERVICE BULLETIN NO. OSB-42-050
Diamond DA42 VI · Maintenance Manual
Overview
This document is an Optional Service Bulletin for the Diamond DA42 aircraft, specifically addressing the installation of additional ECU Backup Batteries. The bulletin is intended for aircraft owners and maintenance personnel, providing critical information regarding compliance and installation procedures. The backup batteries are designed to supply electric power to the ECU during high transient events that may cause a short-term voltage drop, particularly in scenarios involving a depleted main battery. The document outlines the reasons for this service bulletin, including a previous incident of dual engine failure due to electrical power loss, and emphasizes the importance of adhering to proper procedures to prevent such occurrences.
- The ECU Backup Battery installation is optional but recommended for safety.
- The backup batteries provide at least 30 minutes of engine operation during electrical power loss.
- Compliance with the service bulletin is at the owner's discretion.
- Installation requires approximately 10 to 13 hours of labor.
- Only certified service centers should perform the installation.
Document
Source
Originally published by download.aopa.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Maintenance Manual
- Year
- 2007
- Pages
- 4
- File size
- 875 KB
- Publisher
- download.aopa.org
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Technical Details
The bulletin details that all DA42 aircraft are affected and compliance is at the owner's discretion. It discusses the installation of additional ECU Backup Batteries, which provide at least 30 minutes of engine operation during electrical power loss.
Reason for Bulletin
The bulletin was issued following an incident where a dual engine failure occurred after starting the engines with ground power due to a fully depleted main battery. Investigations revealed that inrush currents could cause voltage drops leading to a FADEC reset, resulting in loss of engine thrust.
Planning Information
The document outlines planning information including material availability, special tools required, and estimated labor effort of approximately 10 to 13 hours for installation, depending on the aircraft configuration.
Remarks
It is emphasized that due to the complexity of the installation, only certified Diamond Aircraft Service Centers should perform the measures outlined in the bulletin. Confirmation of accomplishment must be recorded in the logbook.
Safety notes
- Failure to adhere to proper procedures may lead to dual engine failure and total loss of electrical power.
Full document text
Diamond Aircraft Industries GmbH N. A. Otto-Straße 5 A-2700 Wiener Neustadt DAI OSB-42-050 Page 1 of 4 13-Aug-2007 OPTIONAL SERVICE BULLETIN NO. OSB-42-050 I TECHNICAL DETAILS I.1 Category Optional I.2 Airplanes Affected Type: DA 42 Serial Numbers: all I.3 Time of Compliance At owners discretion. I.4 Subject Installation of additional ECU Backup Batteries to supply electric power solely to the ECU in the course of high transient causing a short term voltage drop in case of insufficient main battery power. The ECU Backup Battery capacity is sufficient for at least 30 minutes engine operation. ATA-Code: 72 I.5 Reason On one occasion after starting the engines using ground power due to fully depleted main battery without following the procedures published in the AFM the airplane experienced a dual engine failure and total loss of electrical power. In the course of the investigation ground tests on production aircraft in a similar scenario were carried out without showing the same results. Testing done by the engine manufacturer and subsequent further analysis revealed a potential for experiencing the above mentioned failures under the circumstances of failed or fully depleted main battery and non adherence to the published AFM procedures. According to the Thielert Aircraft Engines Installation Instructions, the alternator of the engine is viewed as the engine s own electrical power source. The battery is the source of electric power in the electrical system of the aircraft. The alternator is certified as part of the engine. The FADEC, alternator and battery are wired in such a way that the FADEC electrical power supply is provided by the alternator in the event of a failure of the battery as required by the Thielert Aircraft Engines Installation Instructions. It has been observed, that the alternator is not able to provide adequate electric power under Diamond Aircraft Industries GmbH N. A. Otto-Straße 5 A-2700 Wiener Neustadt DAI OSB-42-050 Page 2 of 4 13-Aug-2007 such circumstances. Inrush currents of electric consumers may cause short term voltage drops (3 to 5 ms) which trigger a FADEC reset. During such a reset which lasts about 1.28 seconds the FADEC gives no commands to the fuel injectors or the propeller control system. This leads to a sudden engine RPM drop due to no combustion and a propeller auto feather command with subsequent insufficient electrical power generation if the engine RPM are below a certain limit. This results in a total loss of engine thrust and electric power. I.6 Concurrent Documents none I.7 Approval The technical information or instructions contained in this document relate to the Design Change Advisory No. OÄM 42-129, which has been approved under the authority of EASA Design Organization Approval No. EASA.21J.052. The technical content of this document has been approved und the authority of DOA No. EASA.21J.052. I.8 Accomplishment/Instructions Comply with WI-OSB-42-050, latest effective issue. Incorporate TR-OÄM-42-129 Incorporate AMM-TR-OÄM 42-129 I.9 Mass (Weight) and CG Update the Weight and Balance report of the aircraft in accordance with AMM Airplane Maintenance Manual, Doc. No. 7.02.01, latest effective issue. II PLANNING INFORMATION II.1 Material & Availability See WI-OSB-42-050, latest effective issue. II.2 Special Tools See WI-OSB-42-050, latest effective issue. II.3 Labor Effort Approx. 10 to 13 hours, depending on airplane configuration Diamond Aircraft Industries GmbH N. A. Otto-Straße 5 A-2700 Wiener Neustadt DAI OSB-42-050 Page 3 of 4 13-Aug-2007 II.4 Credit For credit contact Diamond Aircraft. II.5 Reference Documents Diamond Aircraft DA 42 Airplane Maintenance Manual, Doc. No. 7.02.01, latest effective issue. WI-OSB-42-050, latest effective issue. AMM-TR-OÄM 42-129 TR-OÄM-42-129 III REMARKS 1. Due to the complexity of the installation all measures may only be carried out by certified Diamond Aircraft Service Centers. 2. Accomplishment of the measures must be confirmed in the log book. 3. In case of any doubt, contact Diamond Aircraft Industries. Diamond Aircraft Industries GmbH N. A. Otto-Straße 5 A-2700 Wiener Neustadt DAI OSB-42-050 Page 4 of 4 13-Aug-2007 EXECUTION REPORT for OSB 42-050 AIRPLANE DATA Airplane Serial Number: _________________ Airplane Registration: _________________ Airplane Operator: _________________ Hours of operation of airplane: _________________ No. of landings: _________________ Hours of operation-engine LH: _________________ RH: _________________ Typical operation of airplane: private, club, training, other ______________ __________________________________ Date, Name, Sign Please fax the completed form to Fax No. **43-2622-26700-369 or e-mail to airworthiness@diamond-air.at
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