AD 98-16-21

final rule
Data completeness: 70%

Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes

AD Number
98-16-21
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-146-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft ATR - GIE Avions de Transport Régional ATR42-200 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR42-300 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR42-320 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR42-500 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR72-101 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR72-102 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR72-201 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR72-202 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR72-211 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes
aircraft ATR - GIE Avions de Transport Régional ATR72-212 Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 Series Airplanes

Unsafe Condition

Wear (scratches or grooving) of the aft upper fittings of the rear engine mount and incorrect shape of the stiffeners for the upper engine cowl, leading to reduced structural integrity of the engine mounts.

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

Required Actions

Perform one-time inspections of the stiffeners for the upper engine cowls to verify correct lower edge profile and inspect for wear of the aft upper fittings of the rear engine mounts. Modify or replace stiffeners not meeting specifications and repair worn fittings as specified in service bulletins, prior to further flight if non-compliant.

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

Compliance Time

Within 10 months after the effective date of this AD

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

Affected Aircraft

Aerospatiale Model ATR42 and ATR72 series airplanes listed in Service Bulletins ATR42-54-0019 and ATR72-54-1011, dated March 9, 1998, certificated in any category.

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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