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AD/BR700/3 Amdt 1 - LP Compressor Fan Disc Cracks
Rolls Royce Germany Turbine Engines - BRRolls Royce Germany Turbine Engines - BR700 Series
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Rolls Royce Germany Turbine Engines - BR700 Series
| AD/BR700/3 Amdt 1 | LP Compressor Fan Disc Cracks | 6/2005 |
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| Applicability: | Rolls Royce BR700-710A1-10 and BR700-710A2-20 engines. |
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| Requirement: | 1. Inspect the fan disc using the visual and/or ultrasonic methods in accordance with Rolls Royce Service Bulletin (S/B) SB-BR700-72-900229 Revision 6.2. Inspect the fan disc using both the ultrasonic and visual method in accordance with Rolls Royce S/B SB-BR700-72-900229 Revision 6.Terminating ActionInstallation of a changed design fan disc in accordance with S/B-BR700-72-900229 Rev 6 constitutes terminating action to this Directive.Note: LBA AD 2000-348R6, approved by EASA Approval No 2005-2313 dated 11 March 2005 refers. |
| Compliance: | For Requirement 1:For Fan Discs Part Number (P/N) BRR18803 and P/N BRR19248:For engines with discs that have already shown compliance with Revision 3 or later of the reference document that used the visual technique; within 25 flight cycles from the effective date of this Directive and thereafter at intervals of 25 flight cycles from the previous inspection until an ultrasonic inspection is carried out, at which time the interval can increase to 75 flight cycles after the first repeat inspection.For engines with discs that have already shown compliance with Revision 3 or later of the reference document that used the ultrasonic technique; within 75 flight cycles from the effective date of this Directive and thereafter at intervals of 75 flight cycles.For Fan Discs P/N BRR20791 installed in Engine Serial Numbers (S/N) prior to 11453(GV) and 12353(GX):For engines with discs that have already shown compliance with Revision 3 or later of the reference document that used the visual technique; within 25 flight cycles from the effective date of this Directive and thereafter at intervals of 25 flight cycles from the previous inspection until an ultrasonic inspection is carried out, at which time the interval can increase to 150 flight cycles after the first repeat inspection. |
| For engines with discs that have already shown compliance with Revision 3 or later of the reference document that used the ultrasonic technique; within 150 flight cycles from the effective date of this Directive and thereafter at intervals of 150 flight cycles.For Fan Discs P/N BRR20791 installed in Engine S/N 11453(GV), S/N 12353(GX) and all subsequent engines, and P/N BRR20791 fan discs held as spares with a JAA form certificate dated on or after 1 January 2002:Initial inspection within 150 flight cycles since new.For Fan Discs P/N BRR20791 held as spares with a JAA Form One certificate date on or after 1 January 2002:Initial inspection within 150 flight cycles since new.For Requirement 2:For all Fan Discs:At each “A” check. |