AD 2004-01-09

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS355E, F, F1, F2, and N Helicopters

AD Number
2004-01-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-SW-24-AD
FR Citation
69 FR 1519

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Model AS355E, F, F1, F2, and N Airworthiness Directives; Eurocopter France Model AS355E, F, F1, F2, and N Helicopters

Unsafe Condition

Complete loss of electrical power generating systems, except for direct battery power, due to a combination of high outside temperature and long flight duration with the landing light on, causing nontemperature compensated trip switches to prematurely trip.

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

Required Actions

Revise the Limitations section of the Rotorcraft Flight Manual (RFM) to prohibit using the landing light except for landing and takeoff. Replace the 40 amp 10P1 and 10P2 contactors with 50 amp circuit breakers. Upgrade the electrical master boxes.

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

Compliance Time

Before further flight

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

Affected Aircraft

Eurocopter France Model AS355E, F, F1, F2, and N helicopters.

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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