AD 2001-24-08

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model EC 120 Helicopters

AD Number
2001-24-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-SW-23-AD
FR Citation
66 FR 60143

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model EC 120 Airworthiness Directives; Eurocopter France Model EC 120 Helicopters

Unsafe Condition

In-flight loss of a cabin sliding door, which had been locked in the open position, leading to potential impact with the horizontal stabilizer or fenestron tail rotor, and subsequent loss of control of the helicopter.

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

Required Actions

Add a stop to the front rail and modify the rear stop of the middle rail in accordance with Eurocopter France Alert Service Bulletin No. 52A004, Revision 1, dated April 19, 2001.

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

Compliance Time

Within 90 days or before the next flight with the door open, whichever occurs first.

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

Affected Aircraft

Eurocopter France Model EC120B helicopters, serial number 1169 and below, with a cabin sliding door rail, part number C533C8102201, C533C8102202, C533C8103201, or C533C8103202, installed, 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

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