AD 98-24-06

final rule
Data completeness: 70%

Airworthiness Directives; Dornier-Werke G.m.b.H. Model Do 27 Q-6 Airplanes

AD Number
98-24-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-CE-137-AD
FR Citation
Federal Register: November 23, 1998 (Volume 63, Number 225)

Applicability

TypeManufacturerModelDetails
aircraft Dornier-Werke GmbH Do 27 Q-6 Airworthiness Directives; Dornier-Werke G.m.b.H. Model Do 27 Q-6 Airplanes

Unsafe Condition

Loose rivets attaching the forward stabilizer attach fitting to the airplane fuselage could result in reduced or loss of control of the airplane due to stabilizer detachment at the forward stabilizer attach flanges.

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

Required Actions

Within 3 calendar months after the effective date, inspect the rivets for looseness in accordance with Dornier SB No. 1140-0000. Thereafter, inspect at intervals not exceeding 100 hours time-in-service. Replace any loose rivets prior to further flight as specified in the same service bulletin.

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

Compliance Time

Within the next 3 calendar months after the effective date, and thereafter at intervals not to exceed 100 hours time-in-service.

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

Affected Aircraft

Dornier-Werke GmbH Model Do 27 Q-6 airplanes, all serial numbers.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.