Airworthiness Bulletin AWB 67-006 Issue 5 - 28 July 2022
Robinson R44 Raven II · Service Bulletins
Overview
This Airworthiness Bulletin (AWB 67-006 Issue 5) addresses governor control anomalies in Robinson R22 and R44 helicopters equipped with Engine Monitoring Units (EMUs). It serves as an advisory document to inform owners, operators, pilots, and maintenance personnel about potential issues with the Engine RPM Governor that could lead to engine overspeed or underspeed conditions. The bulletin emphasizes the importance of monitoring governor operation and provides recommendations for maintenance actions to ensure safe flight operations. Although the bulletin outlines concerns, it does not classify the situation as an unsafe condition warranting an Airworthiness Directive. The document aims to gather data for further investigation and potential solutions.
- This bulletin applies to Robinson R22 and R44 helicopters with EMUs installed.
- Pilots should monitor the governor operation and be prepared to take manual control if necessary.
- If a governor malfunction is suspected, land as soon as practical and have it serviced by qualified personnel.
- Report all governor control problems to CASA with detailed information.
- Follow maintenance instructions strictly to prevent contamination of connectors and wiring.
Document
Source
Originally published by www.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Service Bulletins
- Year
- 2022
- Pages
- 4
- File size
- 104 KB
- Publisher
- www.casa.gov.au
Common. One of the most common aircraft types we track.
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- Pilot's Operating Handbook / AFM
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In this document
Effectivity
This bulletin applies to R22 and R44-series helicopters that have an Engine Monitoring Unit (EMU) installed. EMUs can be identified by an amber status indication light on the respective panels of the helicopters. New helicopters purchased after January 15, 2020, are equipped with EMUs.
Purpose
The purpose of this bulletin is to inform stakeholders about reports of intermittent or abnormal operation of the Engine RPM Governor, which may lead to engine overspeed or underspeed during flight. It aims to gather data to understand the causative factors and implement necessary solutions.
Recommendations
Pilots are advised to monitor governor operation closely during flight. If a malfunction is suspected, they should switch off the governor, take manual control, and land as soon as practical. Maintenance personnel should service the governor as needed. The bulletin also emphasizes the importance of adhering to maintenance instructions to prevent contamination of connectors and wiring.
Reporting
All instances of governor control problems should be reported to CASA via their DRS system. Detailed information about maintenance history, troubleshooting, and operational parameters should be included to assist in identifying potential failure causes.
Enquiries
For any inquiries regarding this Airworthiness Bulletin, contact the Civil Aviation Safety Authority (CASA) via email or in writing to their Airworthiness and Engineering Branch.
Safety notes
- The governor may not prevent overspeed or underspeed during aggressive maneuvers.
- Never use high-pressure spray to clean the helicopter.
Full document text
AWB 67-006 Issue 5 28 July 2022 Page 1 of 4 Airworthiness Bulletin AWB 67-006 Issue 5 - 28 July 2022 Robinson R22/R44 Governor Control Anomalies An Airworthiness Bulletin is an advisory document that alerts, educates, and makes recommendations about airworthiness matters. Recommendations in this bulletin are not mandatory. 1. Effectivity R22 and R44-series helicopters with an Engine Monitoring Unit (EMU) installation. (Factory new helicopters purchased after 15 January 2020 had EMUs installed). Note: EMU installations can be identified by the presence of a status indication light; For R22-series helicopters, EMU status is indicated by an amber light on the aft wall of the compartment under the pilot’s seat. For R44-series helicopters, status is indicated by the amber EMU segment on the annunciator panel. 2. Purpose To advise owners, registered operators, pilots, maintenance organisations and Licensed Aircraft Maintenance Engineers of reports of intermittent or abnormal operation of the Engine RPM Governor ¹ leading to engine overspeed or underspeed conditions during flight. To gather data to form a clear understanding of all potential causative factors so that solutions can be implemented through design, manufacturing, component, or operational changes. At this time, the airworthiness concern described in this Airworthiness Bulletin is not considered an unsafe condition that would warrant an Airworthiness Directive to be issued under Part 39 of the Civil Aviation Safety Regulations 1998. 3. Background Several cases have been reported of the governor not controlling engine RPM under normal conditions leading to either a rotor overspeed or underspeed condition requiring the pilot to override the governor by applying corrective throttle inputs to arrest the condition and complete the flight. Robinson Helicopter Company, as the Type Certificate (TC) holder for the affected aeronautical products, are investigating those reports to identify causal factors and solutions. The US Federal Aviation Administration (FAA), as the TC issuer for Robinson Helicopters, has also been notified and engaged as part of the investigation. AWB 67-006 Issue 5 28 July 2022 Page 2 of 4 ¹ Engine RPM Governor – This system senses engine RPM and makes adjustments to the throttle control to maintain a constant engine RPM, which leads to a constant rotor RPM in flight. Issue 4 was prompted by continued reporting of erratic governor controller operation, even on aircraft in a post SB-111 or SB-119 configuration. Robinson Helicopters is continuing to analyse all relevant data to determine a final solution, with oversight by the FAA. Issue 5 expands the recommended actions to include removal of the C143 engine RPM sensor for cleaning to assure signal integrity. 4. References Robinson Helicopter R22 Service Bulletin SB-119 Robinson Helicopter R22 Kit Instructions KI-288 Robinson Helicopter R44 Service Bulletin SB-111 Robinson Helicopter R44 Kit Instructions KI-287 R22-Series and R44-Series SAFETY ALERT Robinson Helicopter R22 Service Letter SL-94 Robinson Helicopter R44 Service Letter SL-83 News: RPM governor AWB (atsb.gov.au) 5. Recommendations Note that the governor is designed to assist in controlling RPM under normal conditions, it may not prevent over or under speed conditions during aggressive manoeuvres. Exercise care not to unintentionally override governor by squeezing throttle twist grip too tightly. Monitor governor operation during flight by keeping hand lightly on throttle twist grip. A properly functioning governor will provide relatively slow, small, and frequent twist grip rotation in both directions. If twist grip rotation becomes erratic or stops altogether, governor may be malfunctioning. If a governor malfunction is suspected, switch governor off, assume manual RPM control using twist grip, land as soon as practical, and have governor serviced by qualified maintenance personnel. Note that a mechanical linkage from the collective to the engine provides assistance and lessens the need for manual inputs. Regardless of the Governor & Engine RPM Sensor configuration, pilots need to remain vigilant and consciously monitor governor system operation. If an overspeed condition is encountered the Robinson rotorcraft maintenance manual must be consulted for the appropriate inspection. CASA AWB 62-007 also refers to recent main rotor spindle bearings being worn or brinelled which may be a result of an overspeed event. AWB 67-006 Issue 5 28 July 2022 Page 3 of 4 Carry out the maintenance actions within the latest revision of the following Robinson Helicopter Service Bulletins. • R44 Service Bulletin SB-111 • R22 Service Bulletin SB-119 NOTE: Assure strict adherence with Governor & Engine RPM Sensor Connector Upgrade Kit Instructions (KI-288 or KI-287 as applicable), to prevent potential contamination of connectors or wiring. Further, Steel and iron wear particles generated during engine break-in may accumulate on the C143 engine RPM sensor, causing signal interference. Carry out cleaning of the sensor assembly in accordance with the compliance procedure given in the latest revision of Robinson Helicopter Company Service Letter SL-94 or SL-83 as applicable to the aircraft series. The FAA is currently reviewing the associated actions with a view of adopting a new airworthiness directive (AD) for applicable R22 and R44 helicopters. Irrespective of the FAA review outcome, Robinson Helicopter instructions for continued airworthiness (ICA) include, but are not limited to, the helicopter Maintenance Manual (MM), Illustrated Parts Catalogue (IPC) and Service Bulletins, (for example, refer R22 Series MM, Chapter 1, Section 1.000). This is reiterated within sub-regulation 42A of the Civil Aviation Regulations (CAR 1988) where ICA’s are to be taken to form part of the manufacturer’s maintenance schedule. Strict adherence to MM instructions also needs to be assured to prevent potential
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contamination of associated system connectors and wiring, for example; MM Ch. 23 Standard Practices - Cleaning Helicopter - CAUTION- Never use high-pressure spray to clean helicopter. 6. Reporting Report all instances of governor control problems to CASA via the DRS system available on the CASA website. Details of previous maintenance history and troubleshooting for related events should be provided in addition to information concerning fault isolation and rectification. Where possible, flight operational parameters should also be reported together with any other information on possible triggers for the reported event. This information will facilitate a detailed review of potential failure causes and contributing factors. AWB 67-006 Issue 5 28 July 2022 Page 4 of 4 7. Enquiries Enquiries with regard to the content of this Airworthiness Bulletin should be made via the direct link email address: AirworthinessBulletin@casa.gov.au or in writing, to: Airworthiness and Engineering Branch National Operations and Standards Civil Aviation Safety Authority GPO Box 2005, Canberra, ACT, 2601
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