AD 90-23-16

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
90-23-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-202-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-100B Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200B Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200C Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200F Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-300 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400D Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400F Series Airworthiness Directives; BOEING Model 747 Series Airplanes

Unsafe Condition

Failure of the gear selector valve installation could result in partial gear-up or all gear-up landings.

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

Required Actions

Inspect the nose and body gear selector valve installation and the wing gear selector valve installation in accordance with Boeing Service Bulletins. Correct discrepancies prior to further flight. Retorque the self-locking nut to 50 to 80 inch-pound where discrepancies were corrected. Submit a report of any improper configuration to the FAA within 10 days of inspection completion.

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

Compliance Time

Within 30 days of October 30, 1990 (the effective date of AD 90-19-10, Amendment 39-6743) for line positions 002 through 803; within 30 days after the effective date of this AD for line position 806. Special flight permits may be issued under FAR 21.197 and 21.199.

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

Affected Aircraft

Boeing Model 747 series airplanes, line position 002 through 803, and 806 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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