ALERT SERVICE BULLETIN 427-21-44
BELL 427 · Service Bulletins
Overview
This Alert Service Bulletin (ASB) 427-21-44 provides instructions for the inspection and replacement of the transmission oil check valve on Bell 427 helicopters. It addresses potential issues with check valves manufactured by Circor Aerospace that may be susceptible to cracking and outlines compliance timelines for inspections and replacements.
- Affected helicopters: Serial numbers 56001-56084, 58001, 58002.
- Inspection required within 25 flight hours or 30 days.
- Check valves without 'TQL' marking may crack over time.
- Part III replacement required no later than 600 flight hours or 12 months.
- No warranty credit for parts or labor associated with this bulletin.
- No special tools required for inspection or replacement.
- Weight and balance not affected by this bulletin.
- Contact Bell Product Support for questions.
Document
Source
Originally published by bellcustomer.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Service Bulletins
- Year ·
- 2021
- File size ·
- 482 KB
- Publisher ·
- bellcustomer.com
- Language ·
- en
What is the ALERT SERVICE BULLETIN 427-21-44?
The ALERT SERVICE BULLETIN 427-21-44 is a service bulletins for the BELL 427, dated 2021.
Where does the ALERT SERVICE BULLETIN 427-21-44 come from?
This copy of the ALERT SERVICE BULLETIN 427-21-44 was originally published by bellcustomer.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the ALERT SERVICE BULLETIN 427-21-44 published?
The ALERT SERVICE BULLETIN 427-21-44 — the BELL 427 service bulletins on file — is dated 2021.
Most owners only have the POH. Here's the essential set for the BELL 427.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More BELL 427manuals & documents
Related documents
In this document
Compliance
Part I: Inspection within 25 flight hours or 30 days. Part II: Recurring inspection every 25 flight hours or 30 days. Part III: Replacement no later than 600 flight hours or 12 months.
Description
The bulletin addresses cracked transmission oil check valves manufactured by Circor Aerospace and mandates inspections and potential replacements.
Accomplishment Instructions
Instructions for inspecting the check valve, including measuring housing dimensions and determining serviceability.
Material
Required material includes oil check valve part number 209-062-520-001 and packing M25988/1-910.
Manpower
Approximately 1 man-hour for Part I, 0.5 man-hour for Part II, and 1 man-hour for Part III.
Approval
The engineering design aspects of this bulletin are approved by Transport Canada Civil Aviation.
Safety notes
- Check valves with 'TQL' marking are not affected by this bulletin.
- If a crack is found, Part III must be performed prior to the next flight.
- If the valve is not replaced immediately, Part II inspections must continue every 25 flight hours or 30 days.
Full document text
ASB 427-21-44-RA Page 1 of 7 Approved for public release. ALERT SERVICE BULLETIN 427-21-44 15 February 2021 Revision A, 6 April 2021 MODEL AFFECTED: 427 SUBJECT: TRANSMISSION OIL CHECK VALVE 209-062-520- 001, INSPECTION AND REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers 56001 through 56084, 58001, and 58002. COMPLIANCE: Part I: Within the next 25 flight hours or 30 days, whichever comes first after the release date of this bulletin. Part II: Within the next 25 flight hours or 30 days, whichever comes first after accomplishment of Part I and every 25 flight hours or 30 days thereafter until Part III is accomplished. Part III: No later than 600 flight hours or 12 months, whichever comes first after accomplishment of Part I. DESCRIPTION: Bell recently received a report of a cracked transmission oil check valve manufactured by Circor Aerospace (Circle Seal). This check valve was manufactured in 2009 which is outside of the manufacturing date range (October 2011 to March 2015) addressed in Alert Service Bulletin (ASB) 427-15-37. Corrective actions implemented in 2015 by Circor Aerospace to prevent cracking of the check valve housings are indicated by the “TQL” marking. A recent check valve cracking report indicates that additional oil check valves 209-062- 520-001 manufactured by Circor Aerospace (Circle Seal) not having the “TQL” marking may be susceptible to cracking with time in service. ASB 427-21-44-RA Page 2 of 7 Approved for public release. This Alert Service Bulletin (ASB) mandates a one-time inspection of the suspected oil check valve for housing dimension measurement. Oil check valves that do not meet the inspection requirements outlined in the Part I of the Accomplishment Instructions of this bulletin will require replacement. Check valves found serviceable after accomplishment of Part I of this bulletin will not require further inspection or replacement. Alert Service Bulletin 427-15-37 mandated a one-time inspection of transmission oil check valves manufactured between October 2011 and March 2015 without the “TQL” marking. Following the release of ASB 427-15-37, Bell received reports from operators indicating that some transmission oil check valves did not have a manufacturing date stamped on the housing. Based on additional information provided by Circor Aerospace, this bulletin mandates the inspection of all transmission oil check valves manufactured by Circor Aerospace at the Corona facility in California, not having the “TQL” marking. Transmission oil check valves manufactured at the Corona facility have the “CORONA CA” marking. Regardless of the manufacturing date, transmission oil check valves with the “TQL” marking are not affected by this bulletin. Bell has been informed by Circor Aerospace that the “TQL” marking on some oil check valves manufactured after March 2015 may have been omitted. Revision A of this bulletin informs operators that the omission of the “TQL” marking does not impact the serviceability of those affected check valves and they can be used as is. The housing dimension measurement on these check valves is not required. Revision A does not change the compliance of this bulletin. Applicability of this bulletin to any spare part shall be determined prior to its installation on an affected helicopter. APPROVAL: The engineering design aspects of this bulletin are Transport Canada Civil Aviation (TCCA) approved. CONTACT INFO: For any questions regarding this bulletin, please contact: Bell Product Support Engineering Tel: 1-450-437-2862 / 1-800-363-8023 / productsupport@bellflight.com MANPOWER: Approximately 1 man-hour is required to accomplish Part I of this bulletin and 0.5 man- hour to accomplish Part II. Approximately 1 man-hour is required to accomplish Part III of this bulletin. This estimate is based on hands-on time and may vary with personnel and facilities available. ASB 427-21-44-RA Page 3 of 7 Approved for public release. WARRANTY: There is no warranty credit applicable for parts or labor associated with this bulletin. MATERIAL: Required Material: The following material is required for the accomplishment of this bulletin and may be obtained through your Bell Supply Center. Part Number Nomenclature Qty (Note) 209-062-520-001 Oil check valve A/R (1) M25988/1-910 Packing A/R (1) NOTE 1: Replacement will be required only if the check valve does not meet the inspection requirements of Part I of this bulletin. SPECIAL TOOLS: None required. WEIGHT AND BALANCE: Not affected. ELECTRICAL LOAD DATA: Not affected. REFERENCES: BHT-427-MM, Maintenance Manual, Chapter 79. PUBLICATIONS AFFECTED: None affected. ACCOMPLISHMENT INSTRUCTIONS: Part I. Oil check valve inspection. 1. Prepare the helicopter for maintenance and gain access to the transmission oil check valve. The transmission oil check valve is located on the transmission oil cooler (Figure 1, Details A). ASB 427-21-44-RA Page 4 of 7 Approved for public release. -NOTE- It is not necessary to remove the transmission oil check valve for inspection; however, some clamping may require removal for better access. Regardless of the manufacturing date, any transmission oil check valves with the “TQL” marking are not affected by this bulletin. Oil check valves manufactured by other suppliers are also not affected by this bulletin. Transmission oil check valves with the “CORONA CA” marking and without the “TQL” marking are affected by this bulletin. (Figure 1, Detail B). 2. Verify if the installed check valve is affected by this bulletin. 3. If the check valve is not affected, go to step 5. 4. If the check valve is affected, proceed as follows: a. Using a caliper or equivalent, measure the check valve housing at the center and record the dimension (Figure 2). b. Measure the housing at the inlet end where the threaded fitting is installed and record the dimension. c. If the dimension measured at the inlet end is no more than 0.003 inch (0.0762
Show full textShow less
mm) greater than the measurement at the center, the valve is serviceable and does not require accomplishment of Part II or Part III of this bulletin. Go to step 5. -NOTE- Due to possible delay in getting replacement check valves, Bell recommends that owner/operators place their order as soon as Part I is accomplished if the check valve is found cracked or not meeting dimensional criteria and would require replacement in accordance with Part III of this bulletin. d. If the dimension measured at the inlet end is greater than 0.003 inch (0.0762 mm) when compared to the measurement at the center, the valve will require replacement. Part III can be accomplished immediately, or Part II can be accomplished until the affected check valve can be replaced in accordance with Part III. e. If the defective check valve is not replaced immediately, Part II must be accomplished every 25 flight hours or 30 days, whichever comes first, until Part III is accomplished. ASB 427-21-44-RA Page 5 of 7 Approved for public release. 5. Make an entry in the helicopter logbook and historical service records indicating the findings and compliance with Part I of this Alert Service Bulletin. Part II. Recurring 25 flight hour or 30-day inspection. 1. Prepare the helicopter for maintenance and gain access to the transmission oil check valve (Figure 1, Details A). 2. Using a strong light source, visually inspect the transmission oil check valve for general condition and oil leaks. Inspect for cracks at the inlet end where the threaded fitting is installed (Figure 2). 3. If a crack is found, perform, Part III of this bulletin prior to next flight. Figure 3 shows an example of a cracked check valve. 4. If no cracks or any other defects that would cause the check valve to be unserviceable are found, go to step 5. 5. Make an entry in the helicopter logbook and historical service records indicating the findings and compliance with Part II of this Alert Service Bulletin. 6. For affected transmission oil check valves, Part II of this bulletin shall be performed every 25 flight hours or 30 days, whichever comes first, until Part III of this bulletin is accomplished. Part III. Transmission oil check valve replacement. -NOTE- The accomplishment of Part III of this bulletin constitutes the terminating action of this ASB. 1. Prepare the helicopter for maintenance and gain access to the transmission oil check valve (Figure 1, Detail A). 2. Replace the affected transmission oil check valve (BHT-427-MM, Chapter 79). 3. Make an entry in the helicopter logbook and historical service records indicating compliance with Part III of this Alert Service Bulletin. ASB 427-21-44-RA Page 6 of 7 Approved for public release. Transmission oil check valve and location Detail A Circor Aerospace Oil Check Valve Marked “TQL” Detail B Figure 1. Transmission Oil Check Valve Inspection ASB 427-21-44-RA Page 7 of 7 Approved for public release. Figure 2. Transmission Oil Check Valve Outside Diameter Measurement Figure 3. Cracked Oil Check Valve