AD 2012-21-08

final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2012-21-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-0856
FR Citation
77 FR 64711

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Erroneous output from a single radio altimeter channel, which resulted in premature autothrottle retard during approach, could lead to premature autothrottle landing flare retard and the loss of automatic speed control, and consequent loss of control of the airplane.

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

Required Actions

Inspect the part numbers of the operational program software (OPS) of the flight control computers (FCCs). Perform corrective actions if necessary, including installing FCC software part number 2274-COL-AC1-07 or later versions approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) after May 18, 2012.

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

Compliance Time

Within 3 months after the effective date of this AD (November 27, 2012).

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

Affected Aircraft

The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes.

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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