AD 97-21-01 R1

final rule
Data completeness: 70%

MT-PROPELLER ENTWICKLUNG GMBH Model MTV-3-B-C/L250-21 Propellers

AD Number
97-21-01 R1
Status
final_rule
Effective Date
Product Category
propeller
Docket
97-ANE-36-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft MT-Propeller Entwicklung GmbH MTV-3 MT-PROPELLER ENTWICKLUNG GMBH Model MTV-3-B-C/L250-21 Propellers

Unsafe Condition

Propeller hub cracks could result in propeller blade separation and possible loss of control of the airplane.

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

Required Actions

Perform an initial dye penetrant or eddy current inspection of the propeller hub within 50 hours time-in-service after the effective date. If cracks are found, replace the hub before further flight. Subsequent inspections must be done at intervals not exceeding 50 hours or 6 months for P/N B-050 hubs, and 200 hours or 12 months for P/N A-909-A hubs. Rework B-050 hubs by chamfering the bore and marking with SB12C stamp.

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

Compliance Time

Within 50 hours time-in-service after the effective date

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

Affected Aircraft

MT-Propeller Entwicklung GmbH Model MTV-3-B-C/L250-21 propellers installed on Sukhoi 29 aircraft.

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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