AD Amdt-39-10866

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC 135 Helicopters

AD Number
Amdt-39-10866
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-SW-35-AD
FR Citation
63 FR 59206

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter Deutschland GmbH Model EC 135 Airworthiness Directives; Eurocopter Deutschland GmbH Model EC 135 Helicopters

Unsafe Condition

could result in loose bearing attachment bolts, or cracked bearing supports, which could result in loss of drive to the tail rotor and subsequent loss of control of the helicopter.

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.

View Official Source ↗ Find More ADs for Eurocopter Deutschland GmbH Model EC 135

Related Airworthiness Directives

2000-13-08 Recurring

final rule

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC 135 Helicopters

Unsafe Condition: This amendment supersedes an existing airworthiness directive (AD) that applies to Eurocopter Deutschland GmbH (ECD) Model EC 135 helicopters. That AD requires conducting a tail rotor drive shaft v...

Effective: Aug 9, 2000 Category: aircraft

2000-01-19

final rule

Airworthiness Directives; Eurocopter Deutschland GMBH Model EC 135 P1 and EC 135 T1 Helicopters

Unsafe Condition: could result in severe vibration during flight and subsequent loss of control of the helicopter.

Effective: Feb 4, 2000 Category: aircraft

Amdt-39-10632

final rule

Airworthiness Directives; Eurocopter Deutschland GmbH Model EC 135 Helicopters

Unsafe Condition: could result in loss of drive to the tail rotor and subsequent loss of control of the helicopter.

Effective: Jul 13, 1998 Category: aircraft

View all Eurocopter ADs →