# Cameron Balloons Service Bulletin 28: Revision 3

- Rights: © Cameron Balloons. Filed by the FAA in regulations.gov docket FAA-2022-0469; AD 2022-15-02 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Cameron Balloons Service Bulletin 28](https://openairdocs.org/service-documents/cameron-balloons/sb-28.md)
- Title as filed: Cameron Balloons SB28 Rev3
- Pages: 4
- PDF: https://openairdocs.org/files/sha256/f5/39/f5397e93aa3105bc724a82e21b70ad65e637d5d65fc7b8fafd7a058371a62fdf
- Page: https://openairdocs.org/service-documents/cameron-balloons/sb-28/file/f5397e93aa31

## Text

Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

Service Bulletin 28
Cameron Balloons Ltd., St Johns S
treet 
Bedminster, Bristol BS3 4NH, United Kingdom  
Page 1 of 4 Template Ref: CBL/TN/FJD/2368 
Issue: D Date: 30/12/2018
1. General
(a) Service Bulletin
No: 28  
(b) Revision / Date 3 / 03-February-2021 
(c) Title: Stratus Dou ble Burner, Burner Hanger Inspection 
(d) Description: Inspection /  Replacement of Stratus Double Burner Hanger. 
(e) Applicability:
Manuf
acturers: Altisph’air, Ballons Libert sprl, 
Ballonservice & Technik, Balóny Kubíček spol. s.r.o., 
Ballons Chaize, Cameron Balloons Ltd., Lindstrand Hot Air 
Balloons  Ltd., Lindstrand Technologies, Llopis Balloons, 
Notheisz HAB,  Nouvelle Manufacture d’Aerostats,  
Schroeder Fire Balloons GmbH, Sup‐Air, Ultramagic S.A. 
TCDS Numbers: Austria BA 009‐ACG, EASA.BA.003,  
EASA.BA.010, EASA.BA.012, EASA.BA.013, EASA.BA.014, 
EASA.BA.015, EASA.BA.016, EASA.BA.019,  EASA.BA.021, 
EASA.BA.022, EASA.BA.025, EASA.BA.026, EASA.BA.030, 
EASA.BA.119, EASA.BA.517, EAS.IM.BA.110 and France 
No.186. 
Burner Assembly Part Numbers: CB8720 & CB8721. 
(f) Effectivity: All CN where Stratus Double Burners are used; burner serial number up to & including 320. 
Note:  Applicability= All types and variants to which the change can be applied. 
 Effectivity = Actual CN or group of CN’s to which the bulletin has 
been/will be applied. 
2. Background:
A Stratus burner hanger, CB8504, has failed in service after landing. The burner
hanger faile
d, leaving one burner unit detached from the load frame. Examination
of our recor
ds shows a small number of similar failures.
The failures appear to be caused by progressive fatigue cracking of the welded 
joint between the central tube and the end plate of the hanger assembly 
An improved version of the hanger was introduced with CB8504 Issue D in 2009 
which is stronger and more easily inspected.   
3. Compliance (Category) and times:    Required within 30 days or 10 flights.
4. Consequences of Non-Compliance (Possible):  F ailure of the burner hanger
may re
sult in one or both cans detaching from the frame, resulting in an unsafe
condition
.

### Page 2

Service Bulletin 28 
 
  
Cameron Balloons Ltd., St Johns Street 
Bedminster, Bristol BS3 4NH, United Kingdom  
Page 2 of 4               Template Ref: CBL/TN/FJD/2368 
Issue: D Date: 30/12/2018 
5. Required Action (s)): 
 
1/ Identify the build standard of the burner hanger – see accomplishment 
instructions section 2; CBL/TN/DCB/3191 Issue B or later issue. 
 
2/ If the burner hanger is identified to be issue C or earlier inspect the hanger 
for cracks in the weld – see accomplishment instructions Section 3:  
CBL/TN/DCB/3191 Issue A or later issue. 
 
3/ Should any visible cracks be found further flight with the affected burner is 
not permitted.  Report any observed defects to 
technical@cameronballoons.co.uk attaching photographs if available. Cracked 
hangers must not be re-welded. Repair affected burners by replacing the 
cracked hanger with a new issue D or later burner hanger. 
 
4/ Record the inspection in the aircraft log-book. 
 
5/ For burners with hanger CB8504 issue C or earlier the inspection must be 
repeated at each annual inspection. 
 
6/ A number of burners were produced in 1995 / 1996 using a doubler plate to 
reinforce the central part of the hanger bracket (Fig 2).  The welded joint is 
hidden by the doubler plate and therefore impossible to inspect. Hangers of this 
design must be replaced by a new hanger CB8504-0000 Issue D or later. 
        
 
Fig 1.  Hanger with Weld Crack.                    Fig 2. Hanger with doubler plate. 
6. Materials – See CBL/TN/DCB/3191 Issue A or later

### Page 3

Service Bulletin 28 
 
  
Cameron Balloons Ltd., St Johns Street 
Bedminster, Bristol BS3 4NH, United Kingdom  
Page 3 of 4               Template Ref: CBL/TN/FJD/2368 
Issue: D Date: 30/12/2018 
7. Other Publications Affected  None 
8. Mass (Weight)/Balance: Not affected 
9. Maintenance and Operating Instructions Not affected 
10. Additional Information 
An improved burner hanger, CB8504-0000 Issue D or later is available for retrofit 
from Cameron Balloons Ltd.  
 
Fitting of the CB8504-0000 Issue D or later constitutes terminating action for the 
repetitive inspections required by Section 5 paragraph 5 above. 
 
The contents of this bulletin will be added to the Cameron Balloons Inspection 
Schedule at its next revision (Maintenance manual Section 6). 
 
This Service Bulletin (from revision 2) is linked to EASA Airworthiness 
Directive 2021-0042 
 
Notes: 
Date: 03-02-21 Name: D J Cameron 
11. Design Organisation Approval 
 
Date: 03-02-21 Name: D Boxall

### Page 4

Service Bulletin 28
Cameron Balloons Ltd., St Johns S
treet 
Bedminster, Bristol BS3 4NH, United Kingdom  
Page 4 of 4 Template Ref: CBL/TN/FJD/2368 
Issue: D Date: 30/12/2018
Date: 03-02-21 Name: D Boxall 
Note: If this 
Service Bulletin is or will become the subject of an Airworthiness 
Directive, a statement to that effect must be entered in Section 10 of this form.

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