AD 99-21-08

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon (Beech) Model 400A Airplanes

AD Number
99-21-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-280-AD
FR Citation
Federal Register: October 07, 1999 (Volume 64, Number 194)

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. 400A Airworthiness Directives; Raytheon (Beech) Model 400A Airplanes

Unsafe Condition

Chafing of the fuel tube assembly against the elevator control cable due to inadequate clearance between the components could result in fuel leakage from the fuel drain tube assembly and consequent risk of a fire.

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

Required Actions

Replace the existing aft fuselage fuel drain tube assembly (P/N 128-920151-1) with a new modified assembly (P/N 128-920237-1) in accordance with Raytheon Aircraft Service Bulletin SB.28-3076. Compliance is required at the next scheduled inspection but no later than 200 flight hours after the effective date of this AD. No person shall install the old part number (P/N 128-920151-1) after the effective date.

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 (November 12, 1999)

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Affected Aircraft

Raytheon (Beech) Model 400A airplanes, serial numbers RK-1 through RK-92 inclusive.

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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