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19 results found (2212ms)

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2023-11-07

final rule

Airworthiness Directives; Various Helicopters

Unsafe Condition: unsafe condition on these products.

Effective: Jun 22, 2023 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Helicopters

2022-05-10 Recurring

final rule

Airworthiness Directives; Goodrich Externally-Mounted Hoist Assemblies

Unsafe Condition: The overload clutch in the Goodrich externally-mounted hoist assemblies can fail, leading to in-flight loss of the hoist load, possibly resulting in injury to persons on the ground or in a hoisting...

Effective: Apr 20, 2022 Category: aircraft Compliance: Within 12 months of effective date

Why matched: Airworthiness Directives; Goodrich Externally-Mounted Hoist Assemblies

2021-22-11 Recurring

final rule

Airworthiness Directives; MD Helicopters Inc. (MDHI) Helicopters

Unsafe Condition: A report of a spiral crack in the pilot-to-copilot tail rotor torque tube (torque tube) that appears to have originated from a hole where the tail rotor torque tube control fitting attaches to the ...

Effective: Jan 10, 2022 Category: aircraft Compliance: Within 100 hours TIS after the effective date of this AD, or within 5 hours TIS or 30 days after ...

Why matched: Airworthiness Directives; MD Helicopters Inc. (MDHI) Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2020-18-20

final rule

Airworthiness Directives; MD Helicopters Inc. (MDHI), Helicopters

Unsafe Condition: Reports of leading edge abrasion strips manufactured by HTC departing the MR blades during flight. An investigation determined that the abrasion strips were manufactured from electroformed nickel, ...

Effective: Oct 28, 2020 Category: aircraft Compliance: Within 10 hours TIS and thereafter before the first flight of each day until the abrasion strip h...

Why matched: Airworthiness Directives; MD Helicopters Inc. (MDHI), Helicopters

2020-06-11

final rule

Airworthiness Directives; MD Helicopters Inc. Helicopters

Unsafe Condition: a link assembly remaining in service beyond its fatigue life, which could result in failure of the link assembly, failure of M/R blade pitch control, and subsequent loss of helicopter control.

Effective: Apr 28, 2020 Category: aircraft Compliance: Within 100 hours time-in-service (TIS)

Why matched: Airworthiness Directives; MD Helicopters Inc. Helicopters

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2016-04-15

final rule

Airworthiness Directives; MD Helicopters Inc., Helicopters

Unsafe Condition: A pin remaining in service beyond its fatigue life, which could result in failure of a pin, loss of a main rotor blade, and subsequent loss of control of the helicopter.

Effective: Mar 31, 2016 Category: aircraft Compliance: Within 100 hours time-in-service (TIS) or during the next annual inspection, whichever occurs first.

Why matched: Airworthiness Directives; MD Helicopters Inc., Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2016-01-19

final rule

Airworthiness Directives; MD Helicopters Inc.

Unsafe Condition: Rotating cone assembly remaining in service beyond its fatigue life, which could result in failure of the rotating cone assembly and loss of control of the helicopter.

Effective: Feb 25, 2016 Category: aircraft Compliance: Within 1 year or at the next annual inspection, whichever comes later.

Why matched: Airworthiness Directives; MD Helicopters Inc.

2007-05-51

final rule

Airworthiness Directives; MD Helicopters Inc. (MDHI) Model MD600N Helicopters

Unsafe Condition: Cracks in the lateral mixer output link assembly (mixer link), specifically in the bearing end area, emanating from staking marks, could result in failure of the mixer link and subsequent loss of c...

Effective: May 7, 2007 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; MD Helicopters Inc. (MDHI) Model MD600N Helicopters

2004-16-08

final rule

Airworthiness Directives; MD Helicopters Inc. Model MD900 Helicopters

Unsafe Condition: Fatigue failure of the piston rod in the spring capsule of the control rod assembly, which could result in failure of the piston rod and subsequent loss of control of the helicopter.

Effective: Aug 25, 2004 Category: aircraft Compliance: Before September 17, 2004, or based on specified hours time-in-service (TIS) of the control rod a...

Why matched: Airworthiness Directives; MD Helicopters Inc. Model MD900 Helicopters

2002-10-05

final rule

Airworthiness Directives; MD Helicopters Inc. Model MD-900 Helicopters

Unsafe Condition: Cracks starting at the drive plate attachment holes in the main rotor upper hub assembly drive plate attachment flange have been reported, which could lead to failure of the hub assembly, loss of d...

Effective: Jun 19, 2002 Category: aircraft Compliance: Before further flight if a crack is found.

Why matched: Airworthiness Directives; MD Helicopters Inc. Model MD-900 Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2001-07-09

final rule

Airworthiness Directives; MD Helicopters Inc. Model MD-900 Helicopters

Unsafe Condition: Failure of the hub assembly, loss of drive to the main rotor, and subsequent loss of control of the helicopter due to cracked main rotor upper hub assembly drive plate attachment flange.

Effective: May 1, 2001 Category: aircraft Compliance: Within 6 hours TIS for initial inspection and crack determination; within 25 hours TIS for subseq...

Why matched: Airworthiness Directives; MD Helicopters Inc. Model MD-900 Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2000-10-06

final rule

Airworthiness Directives; MD Helicopters Inc. Model MD900 Helicopters

Unsafe Condition: Drive shafts with no assembly part number marked could remain in service past their life limit, leading to fatigue failure and total loss of drive to the main rotor hub, resulting in loss of contro...

Effective: Jun 1, 2000 Category: aircraft Compliance: Before accumulating 1,450 hours time-in-service (TIS) or before further flight if TIS equals or e...

Why matched: Airworthiness Directives; MD Helicopters Inc. Model MD900 Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2000-08-22 Recurring

final rule

Airworthiness Directives; MD Helicopters Inc. Model 369D, 369E, 500N, and 600N Helicopters

Unsafe Condition: Erroneous turbine outlet temperature (TOT) readings and incorrect wiring harness terminal lugs on the thermocouple wiring, which could lead to an erroneous TOT indication, damage to critical engine...

Effective: May 22, 2000 Category: engine Compliance: Within the next 50 hours time-in-service or on or before June 15, 2000, whichever occurs earlier.

Why matched: Airworthiness Directives; MD Helicopters Inc. Model 369D, 369E, 500N, and 600N Helicopters

2000-04-21

final rule

Airworthiness Directives; MD Helicopters Inc. Model MD600N Helicopters

Unsafe Condition: Fuel hose connections between the fuel cells and the engine can be incorrectly installed, leading to fuel starvation of the engine while the fuel gage indicates fuel remaining in the tank, engine f...

Effective: Apr 5, 2000 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; MD Helicopters Inc. Model MD600N Helicopters

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

Amdt-39-11564

final rule

Airworthiness Directives; MD Helicopters Inc. Model 500N and 600N Helicopters

Unsafe Condition: Stress corrosion cracks in the thruster control cable conduit cap may lead to failure of the cap, causing a fixed thruster condition and subsequent loss of normal anti-torque directional control.

Effective: Mar 1, 2000 Category: aircraft Compliance: Within 5 hours TIS or before further flight after December 31, 1999, for the initial inspection; ...

Why matched: Airworthiness Directives; MD Helicopters Inc. Model 500N and 600N Helicopters

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

99-25-08

final rule

Airworthiness Directives; MD Helicopters Inc. Model 500N and 600N Helicopters

Unsafe Condition: Stress corrosion cracks in the thruster control cable conduit cap at the telescopic swivel end and relieved area could cause failure of the cap, leading to a fixed thruster condition and subsequent...

Effective: Mar 1, 2000 Category: aircraft Compliance: Within 5 hours time-in-service or before further flight after December 31, 1999 (first inspection...

Why matched: Airworthiness Directives; MD Helicopters Inc. Model 500N and 600N Helicopters

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

99-20-12

final rule

Airworthiness Directives; MD Helicopters Inc. Model 369D, 369E, 369FF, 500N, and 600N Helicopters

Unsafe Condition: Failure of the oil cooler blower bracket (P/N 369F5190-1) could result in loss of cooling of engine oil and transmission oil, leading to a subsequent forced landing.

Effective: Nov 4, 1999 Category: aircraft Compliance: Within 100 hours time-in-service

Why matched: Airworthiness Directives; MD Helicopters Inc. Model 369D, 369E, 369FF, 500N, and 600N Helicopters

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Amdt-39-11342

final rule

Airworthiness Directives; MD Helicopters Inc. Model 369D, D369E, 369FF, 500N, and 600N Helicopters

Unsafe Condition: Cracked oil cooler blower bracket may lead to failure of the bracket, loss of cooling for engine oil and transmission oil, and subsequent forced landing.

Effective: Nov 4, 1999 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; MD Helicopters Inc. Model 369D, D369E, 369FF, 500N, and 600N Helicopters

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

98-14-03

final rule

Airworthiness Directives; AlliedSignal Inc. KT 76A Air Traffic Control (ATC) Transponders.

Unsafe Condition: The inability of AlliedSignal Inc. KT 76A ATC transponders to coordinate with ground-based ATC radar sites and nearby TCAS-equipped aircraft, caused by silver migration in resistor network modules ...

Effective: Aug 16, 1998 Category: appliance Compliance: within 12 calendar months

Why matched: Airworthiness Directives; AlliedSignal Inc. KT 76A Air Traffic Control (ATC) Transponders.