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AD/B737/313 - Circumferential Butt Splices and Bonded Doublers
Boeing 737 Series AeroplanesBoeing 737 Series Aeroplanes
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Boeing 737 Series Aeroplanes
| AD/B737/313 | Circumferential Butt Splicesand Bonded Doublers | 2/2008 |
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| Applicability: | Model 737 series airplanes listed in Boeing Service Bulletin 737-53-1076, Revision 4, dated 26 September 1991; certificated in any category. |
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| Requirement: | Carry out inspections and, if required, repairs contained in the technical requirements of FAA AD 92-25-09.Note: FAA AD 92-25-09 refers. |
| Compliance: | Carry out inspection and, if required, repairs at intervals specified in the technical requirements of FAA AD 92-25-09 except with a revised effective date of14 February 2008. Where FAA AD 92-25-09 specifies a compliance time relative to 28 May 1991, revise this date to the effective date of this AD. |
| This Airworthiness Directive becomes effective on 14 February 2008. | |
| Background: | Operators have reported occurrences of delamination or corrosion of bonded skin panels. This AD requires inspections and repairs to prevent cabin pressurisation difficulties or possible rapid decompression. |
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David Punshon
Delegate of the Civil Aviation Safety Authority
4 January 2008