AD 93-15-06

final rule
Data completeness: 70%

Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes

AD Number
93-15-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
93-NM-118-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2-1A Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B2-1C Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B2-203 Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B2K-3C Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B4-103 Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B4-203 Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B4-2C Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B4-601 Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B4-603 Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
aircraft Airbus A300 B4-605R Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes

Unsafe Condition

Jamming of the free fall mechanical control mechanism could result in failure of the nose landing gear (NLG) to extend during a gravity free fall.

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

Required Actions

Perform a detailed visual inspection of the bolts attaching the NLG door uplock assemblies and the free fall rod connection within 30 landings after the effective date. If bolts are incorrectly installed, correct them prior to further flight and perform a functional test of the landing gear systems. Submit a report of findings within 7 days.

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

Compliance Time

within 30 landings after the effective date of this AD

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

Affected Aircraft

All Airbus Industrie Model A300, A310, and A300-600 series airplanes 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.