AD 2015-13-08

final rule
Data completeness: 80%

Airworthiness Directives; Dassault Aviation Airplanes

AD Number
2015-13-08
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2015-1988
FR Citation
80 FR 37150

Applicability

TypeManufacturerModelDetails
aircraft Dassault Aviation Airworthiness Directives; Dassault Aviation Airplanes
aircraft Aviat Various Airworthiness Directives; Dassault Aviation Airplanes

Unsafe Condition

Manufacturing deficiency of some engine air inlet anti-ice piccolo tubes leading to reduced performance of the engine anti-ice protection system, resulting in ice accretion and ingestion into the engines, which could cause dual engine power loss and reduced controllability.

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

Required Actions

Revise the airplane flight manual to include a procedure for addressing minimum fan speed rotation (N1) values during stand-alone engine anti-ice system operation for engines equipped with certain air inlets. This revision must be completed within 10 flight cycles after the effective date of the AD.

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

Compliance Time

Within 10 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

All Dassault Aviation Model FALCON 2000EX airplanes, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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