AD 2000-25-04

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon (Beech) Model MU-300, MU-300-10, 400, 400A, and 400T Series Airplanes

AD Number
2000-25-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-60-AD
FR Citation
65 FR 77782

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Various Airworthiness Directives; Raytheon (Beech) Model MU-300, MU-300-10, 400, 400A, and 400T Series Airplanes

Unsafe Condition

Hydraulic fluid leakage from the B-nut area, which attaches a hydraulic tube to the anti-skid valve assembly, could lead to sudden loss of normal braking to the left wheel, causing an asymmetric braking condition and longer stopping distance, potentially resulting in the airplane overrunning the runway surface.

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

Required Actions

Perform a one-time general visual inspection to detect hydraulic fluid leakage from the B-nut area. If no leakage is found, install an additional support (new nutplate, clamp, and screw) for the hydraulic tube. If leakage is found, replace the hydraulic tube with a new or serviceable one and install the additional support.

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

Compliance Time

Within 200 flight hours after the effective date of this AD.

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Affected Aircraft

Raytheon (Beech) Model MU-300, MU-300-10, 400, 400A, and 400T series airplanes, as listed in Raytheon Aircraft Service Bulletin SB 32-3300, dated December 1999, 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 6, 2026

Rights: U.S. Government Public Domain

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