AD 2007-10-06

final rule
Data completeness: 70%

Airworthiness Directives; Turbomeca Arriel 2B1 Turboshaft Engines

AD Number
2007-10-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-28009
FR Citation
72 FR 26714

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Turbomeca Arriel 2B1 Turboshaft Engines
engine Turbomeca Arriel 2B1 Airworthiness Directives; Turbomeca Arriel 2B1 Turboshaft Engines

Unsafe Condition

Two cases of flameout have been reported on Arriel 2B1 engines: One when lowering collective pitch on ground at landing and one when switching from Flight Position to idle Position on ground. Both flameout events are explained as occurring when the stepper motor loses steps to a value below the 'level 1 failure' detection threshold, reducing the fuel flow of the anti-flameout limit sufficiently to cause an engine flameout when decreasing rapidly the demand for power.

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

Required Actions

Download and install DECU software version 5.02 as soon as practicable, but no later than August 31, 2007.

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

Compliance Time

Within 3 months of the effective date (August 31, 2007)

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Affected Aircraft

Turbomeca Arriel 2B1 Turboshaft Engines

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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