AD/CF34/13 Uncontained Fan Disk Failure (Cth)
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
General Electric Turbine Engines - CF34 Series
| AD/CF34/13 | Uncontained Fan Disk Failure | 4/2007 TX |
Applicability: | General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1 turbofan engines that have fan disks with serial numbers (SNs) listed in Table 1 of this AD. Affected regional jet fan disk part numbers (P/Ns) are 5922T01G04, 5922T01G05, 6078T57G01, 6078T57G02, 6078T57G03, 6078T57G04, 6078T57G05, and 6078T57G06. Affected business jet fan disk P/Ns are 5921T18G01, 5921T18G09, 5921T18G10, 5921T54G01, 5922T01G02, 5922T01G04, 5922T01G05, 6020T62G04, 6020T62G05, 6078T00G01, 6078T57G01, 6078T57G02, 6078T57G03, 6078T57G04, 6078T57G05, and 6078T57G06. Note 1: These engines are installed on, but not limited to, Bombardier, Inc. Table 1 - Fan Disk SNs and Last Known
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Requirement: | Perform a onetime visual and tactile inspection of the bore area on the 31 fan disks listed in Table 1 of this AD, that have not had a shop-level inspection. - For regional jet engine models CF34-3A1/-3B1, use paragraphs 3.A through 3.B.(2)(g) of the Accomplishment Instructions of GE Alert Service Bulletin No. CF34-AL S/B 72-A0232, dated 15 February 2007, to do the inspections. - For business jet engine models CF34-3A1/-3B, use paragraphs 3.A through 3.B.(2)(g) of the Accomplishment Instructions of GE Alert Service Bulletin No. CF34-BJ S/B 72-A0213, dated 15 February 2007, to do the inspections. |
| Note 2: FAA Emergency AD 2007-04-51 dated16 February 2007 refers. | |
Compliance: | Within 20 engine flight hours after the effective date of this AD, unless the actions have already been done. |
| This Airworthiness Directive becomes effective on 2 March 2007. | |
Background: | This AD results from a report that a GE CF34-3B1 turbofan engine experienced an uncontained fan disk failure during flight operation. The issuing of this AD to detect electrical arc-out defects on fan disks, which could result in uncontained fan disk failure and aeroplane damage. |
David Punshon
Delegate of the Civil Aviation Safety Authority
27 February 2007
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