AD 2001-05-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Rolls-Royce | GmbH Models BR700-710A1-10 and BR700-710A2-20 | Airworthiness Directives; BMW Rolls-Royce GmbH Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines |
Unsafe Condition
Cracks in the dovetail area of fan disks, which could result in an uncontained engine failure and damage to the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually or ultrasonically inspect fan disks within 25 flight cycles after the effective date of the AD. If cracks are found, remove the disk and replace it with a serviceable one. Conduct repetitive inspections as specified in Rolls-Royce Deutschland Service Bulletin No. SB-BR700-72-900229, Revision 2.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 flight cycles after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BMW Rolls-Royce GmbH models BR700-710A1-10 with fan disks part numbers BRR18803, BRR19248, or BRR20791, and BR700-710A2-20 turbofan engines with fan disks part numbers BRR19248 or BRR20791 installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.