AD 78-05-02

final rule
Data completeness: 70%

AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines

AD Number
78-05-02
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. TPE331-1 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-1U AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-1UA AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-2 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-2U AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-2UA AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-3 AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-3U AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-3UW AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines
engine Honeywell International Inc. TPE331-3W AIRESEARCH MANUFACTURING COMPANY OF ARIZONA Model TPE331-1, -2, -3, -5, and -6 Series Engines

Unsafe Condition

Failure of the propeller pitch control cam follower pin

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Required Actions

Remove propeller pitch control sleeve assembly Part Number 869647-1, -2, or -3 and replace it with a serviceable propeller pitch control sleeve assembly Part Number 869647-4 or later FAA approved sleeve assembly per AiResearch Service Bulletin TPE331-72-0115, or equivalent method approved by the FAA.

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Compliance Time

Within the next 500 hours time in service after April 1, 1978 or prior to September 30, 1979, or at next engine overhaul, whichever comes first

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

Affected Aircraft

AiResearch Model TPE331-1, -2, -3, -5, and -6 Series engines

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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