AD 98-19-17

final rule
Data completeness: 70%

Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-400 Gliders

AD Number
98-19-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-CE-12-AD
FR Citation
Federal Register: September 17, 1998 (Volume 63, Number 180)

Applicability

TypeManufacturerModelDetails
aircraft DG Flugzeugbau GmbH DG-400 Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-400 Gliders

Unsafe Condition

Damage to the engine caused by vibration, which could result in loss of engine power during critical phases of flight.

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

Required Actions

Inspect the powerplant (engine) mount and propeller mount for any loose parts within 1 calendar month after the effective date. If loose parts are found, within 3 calendar months or prior to further flight, modify the starter motor, retrofit the holder for the starter motor, check and adjust the engine ignition timing, and ensure compliance with specified technical notes and maintenance manuals.

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

Compliance Time

Within 1 calendar month after the effective date of this AD for the inspection, and within 3 calendar months after the inspection or prior to further flight if loose parts are found, whichever occurs first.

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

Affected Aircraft

Glaser-Dirks Flugzeugbau GmbH Model DG-400 gliders, serial numbers 4-1 through 4-249.

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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