AD 97-15-10

final rule
Data completeness: 70%

Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines

AD Number
97-15-10
Status
final_rule
Effective Date
Product Category
engine
Docket
96-ANE-13
FR Citation
Federal Register: July 23, 1997 (Volume 62, Number 141)

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. TPE331-10 Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10A Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10AV Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10B Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10G Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10GP Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10GR Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10GT Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10J Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines
engine Honeywell International Inc. TPE331-10N Airworthiness Directives; AlliedSignal Inc. TPE331 Series Turboprop Engines

Unsafe Condition

Icing of the inlet Pt2 sensor can produce an erroneous high pressure signal to the fuel control, causing little or no response to power lever movement.

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

Required Actions

Revise the Emergency Procedures or Abnormal Procedures Section of the FAA-approved AFM or POH to include a paragraph about a non-responsive power lever. Replace or rework orifice fittings and restrictors as terminating actions to the AFM revision requirement.

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

Compliance Time

Within 30 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

AlliedSignal Inc. TPE331-3, -5, -6, -10, -11, -12 series turboprop engines equipped with Woodward fuel controls, installed on specified aircraft models including Ayres S2R-G5, S2R-G6, S2R-G10, Beech Model B100, CASA C-212, Dornier 228, Fairchild SA226/SA227, Jetstream 3101/3201, Mitsubishi MU-2B, Short SC-7 Skyvan Series 3, Twin Commander 680/690/695.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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