AD 98-24-07

final rule
Data completeness: 70%

Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

AD Number
98-24-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-CE-53-AD
FR Citation
Federal Register: November 23, 1998 (Volume 63, Number 225)

Applicability

TypeManufacturerModelDetails
aircraft Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300 Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes
aircraft Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300L Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes
aircraft Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300S Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

Unsafe Condition

Failure of the rudder pedal footrest caused by overloading the rudder pedal safety control stop, which could result in loss of directional control of the airplane.

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

Required Actions

Inspect the rudder pedal alignment, safety control stop for wear and clearance, rudder cables for elongation, and footrest flange for cracks. Correct or replace discrepant parts as applicable, including re-rigging or replacing cables, replacing the safety control stop, and replacing the rudder pedal if cracks are found. Inspections must be repeated every 50 hours time-in-service.

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

Compliance Time

Within the next 50 hours time-in-service after the effective date of this AD (December 28, 1998), unless already accomplished, and thereafter at intervals not to exceed 50 hours TIS. Replacements or corrective actions are required prior to further flight after discrepancies are found.

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

Affected Aircraft

EXTRA Flugzeugbau GmbH Models EA-300 (all serial numbers with electric actuated rudder pedal adjustment produced before November 1995), EA-300S (serial numbers 001 through 028), and EA-300L (serial numbers 001 through 015).

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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