AD 2014-15-15

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Beechcraft Corporation Airplanes

AD Number
2014-15-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0187
FR Citation
79 FR 44677

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Aircraft Company Airworthiness Directives; Beechcraft Corporation Airplanes
aircraft Beechcraft Corporation Airworthiness Directives; Beechcraft Corporation Airplanes
aircraft Mitsubishi Heavy Industries Airworthiness Directives; Beechcraft Corporation Airplanes

Unsafe Condition

Fatigue cracking in the horizontal stabilizer ribs, which could result in the failure of the horizontal stabilizer and loss of pitch control of the airplane.

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

Required Actions

Perform a radiographic (x-ray) or borescope inspection for cracking of the horizontal stabilizer rib assemblies, in accordance with an approved method. Repeat the inspection at intervals not to exceed 2,400 flight hours.

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

Compliance Time

Before the accumulation of 7,400 total flight hours or within 6 months after the effective date of this AD, whichever occurs later.

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

Affected Aircraft

Beechcraft Corporation Model MU-300 airplanes, serial numbers A003SA through A093SA; Model 400 airplanes, serial numbers RJ-1 through RJ-65; Model 400A airplanes, serial numbers RK-1 through RK-604; Model 400T (T-1A) airplanes, serial numbers TT-1 through TT-180; and Model 400T (TX), serial numbers TX-1 through TX-13.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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