AD 2011-22-01

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (RRD) BR700-710 Series Turbofan Engines

AD Number
2011-22-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0684
FR Citation
76 FR 64791

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (RRD) BR700-710 Series Turbofan Engines

Unsafe Condition

Analysis of service data has shown that the effect of touch-and-go and overshoot on life cycle counting is higher than anticipated. Therefore, the life cycle counting method for touch-and-go and overshoot as defined by the Time Limits Manual needs to be changed to reflect this higher effect on life.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Revise the airworthiness limitations section (ALS) of the operators' approved maintenance program to remove the requirement to record each touch-and-go or overshoot as 1/5 of a flight cycle on engines installed on airplanes used for Pilot Training. Revise the ALS to add a requirement to record each touch-and-go or overshoot as 1 flight cycle to the life of all critical parts and the fan blades. Within 120 days, determine the number of touch-and-go's and overshoots experienced by each individual critical part since entry into service for Pilot Training and recalculate the accumulated flight cycles if the number of touch-and-go's and overshoots is one percent or more of the total flight cycles on the critical part.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 30 days and within 120 days after the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

All Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20 turbofan engines, all BR700-710C4-11 model engines with hardware configuration standard 710C4-11 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard not incorporated), and all BR700-710C4-11 model engines with hardware configuration standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated). These engines are installed on, but not limited to, Bombardier BD-700-1A10 and BD-700-1A11 airplanes and Gulfstream GV (G500) and GV-SP (G550) airplanes.

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

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