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2020-26-14 Recurring

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

Unsafe Condition: The propeller pitch control (PPC) lever linkages may disconnect at the engine.

Effective: Feb 2, 2021 Category: propeller Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

2016-08-19

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

Unsafe Condition: Reports of cracks found in the attach fittings of the main landing gear oleo strut, resulting from improper lubrication and/or hard landings.

Effective: Jun 6, 2016 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2015-01-02

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

Unsafe Condition: Stress corrosion cracking in the flanges of the airframe at stations 4610 and 5605.

Effective: Feb 26, 2015 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

2011-12-01

final rule

Airworthiness Directives; Koito Industries, Ltd., Seats and Seating Systems Approved Under Technical Standard Order (TSO) TSO-C39b, TSO-C39c, or TSO-C127a

Unsafe Condition: Seats and seating systems may not meet certain flammability, static strength, and dynamic strength criteria. Failure to meet static and dynamic strength criteria could result in injuries during eme...

Effective: Aug 1, 2011 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Koito Industries, Ltd., Seats and Seating Systems Approved Under Technical Standard Order (TSO) TSO-C39b, TSO-C39c, or TSO-C127a

2010-10-17

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Models MU-2B Airplanes

Unsafe Condition: The FAA is correcting an airworthiness directive (AD) that has published in the Federal Register. That AD applies to the products listed above. The reissue date of September 24, 1986, of the MU-2B-...

Effective: Nov 23, 2010 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Models MU-2B Airplanes

2007-17-09

final rule

Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

Unsafe Condition: Pilots attempting to force additional nose-down trim manually jammed the trim system, preventing subsequent electric trim changes until manually freed.

Effective: Sep 25, 2007 Category: aircraft Compliance: Within 100 flight hours from April 11, 1994, the effective date of AD 94-04-16.

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

2006-17-05

final rule

Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

Unsafe Condition: Improper adjustment of the flight idle fuel flow setting, which could result in degraded performance and poor handling qualities with consequent loss of control of the airplane in certain situations.

Effective: Sep 22, 2006 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

2006-15-07

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition: Improper rigging and/or adjustment of the propeller feathering linkage, which could result in the inability of the linkage to pull the feather valve to function as designed, leading to asymmetric d...

Effective: Aug 24, 2006 Category: propeller Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2006-14-08

final rule

Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

Unsafe Condition: Incorrect flight idle blade angle settings could lead to an asymmetric thrust situation in certain flight conditions, which could result in airplane controllability problems.

Effective: Aug 21, 2006 Category: aircraft Compliance: Within the next 100 flight hours

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

2006-13-15

final rule

Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

Unsafe Condition: Failure of wing attach barrel nuts and/or associated wing attachment hardware due to cracks, corrosion, fractures, and incorrect torque values.

Effective: Aug 11, 2006 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries MU-2B Series Airplanes

2005-22-11 Recurring

final rule

Airworthiness Directives; Mitsubishi Model YS-11 Airplanes, and Model YS-11A-200, YS-11A-300, YS-11A-500, and YS-11A-600 Series Airplanes

Unsafe Condition: Fatigue cracking of the propeller hub, which could cause the loss of the propeller.

Effective: Dec 6, 2005 Category: propeller Compliance: Before further flight.

Why matched: Airworthiness Directives; Mitsubishi Model YS-11 Airplanes, and Model YS-11A-200, YS-11A-300, YS-11A-500, and YS-11A-600 Series Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-22-07 R1

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU- 2B Series Airplanes

Unsafe Condition: The unsafe condition is the potential for icing-related incidents or accidents due to pilot error when pilots-in-command (PIC) of MU-2B series airplanes lack proficiency in recognizing adverse oper...

Effective: Apr 16, 2004 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU- 2B Series Airplanes

Amdt-39-13504

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

Unsafe Condition: Pilot error in icing conditions could lead to unsafe operation of Mitsubishi MU-2B series airplanes.

Effective: Apr 16, 2004 Category: aircraft Compliance: Within 30 days of the effective date of this AD revision.

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

2003-22-07

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

Unsafe Condition: Pilot error in recognizing severe icing conditions that may overpower the propeller ice protection system and result in rapid airspeed loss without significant airframe ice accretion.

Effective: Dec 15, 2003 Category: aircraft Compliance: Within the next 10 days after the effective date of this AD.

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

2003-17-04 Recurring

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition: Cockpit windshield or cabin window separation during flight, caused by repeated cabin pressurization cycles, leading to shattering glass.

Effective: Oct 3, 2003 Category: engine Compliance: Before further flight.

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

2000-09-15

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition: Several icing-related incidents and accidents of Mitsubishi MU-2B series airplanes, indicating potential for departure from controlled flight while operating in icing conditions.

Effective: Jul 24, 2000 Category: aircraft Compliance: Within 12 months of the effective date (July 24, 2000).

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Amdt-39-11819

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

Unsafe Condition: Departure from controlled flight while operating in icing conditions.

Effective: Jul 24, 2000 Category: aircraft Compliance: Within 12 calendar months after July 24, 2000

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

2000-09-15 R1

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

Unsafe Condition: Icing Conditions

Effective: Jul 24, 2000 Category: aircraft

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd., MU-2B Series Airplanes

2000-02-25

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Model MU-2B Series Airplanes

Unsafe Condition: Reports of in-flight incidents and an accident in icing conditions where the airframe pneumatic deicing boots were not activated, leading to reduced controllability due to ice accumulation.

Effective: Mar 24, 2000 Category: aircraft Compliance: Not specified.

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Model MU-2B Series Airplanes

99-19-06

final rule

Airworthiness Directives; Mitsubishi Model YS-11 and YS-11A Series Airplanes

Unsafe Condition: Failure to activate airframe pneumatic deicing boots at the first signs of ice accumulation leading to reduced controllability due to adverse aerodynamic effects of ice adhering to the airplane pri...

Effective: Dec 27, 1999 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Model YS-11 and YS-11A Series Airplanes

99-10-16

final rule

Airworthiness Directives; Mitsubishi Model YS-11 Series Airplanes

Unsafe Condition: Fatigue cracking in the manhole doublers of the lower wing panels could result in failure of the wing structure.

Effective: Jun 22, 1999 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Mitsubishi Model YS-11 Series Airplanes

Amdt-39-10807

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition: could result in loss of control of the airplane.

Effective: Nov 20, 1998 Category: aircraft

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

98-20-39

final rule

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition: The wing tip tank may separate from the airplane because of an incorrect bolt corroding, which could result in loss of control of the airplane.

Effective: Nov 20, 1998 Category: aircraft

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

98-13-13

final rule

Airworthiness Directives; Mitsubishi Heavy Industries Ltd. Model YS-11 and YS-11A Series Airplanes

Unsafe Condition: Loss of airplane controllability or engine overspeed with consequent loss of engine power caused by the power levers being positioned below the flight idle stop while the airplane is in flight.

Effective: Jul 23, 1998 Category: aircraft Compliance: Within 30 days after the effective date of this AD (July 23, 1998).

Why matched: Airworthiness Directives; Mitsubishi Heavy Industries Ltd. Model YS-11 and YS-11A Series Airplanes

98-04-34

final rule

Airworthiness Directives; Mitsubishi Model YS-11 and YS-11A Series Airplanes

Unsafe Condition: Operating the airplane in severe icing conditions outside the certification envelope may lead to potential hazards due to insufficient flight crew information on recognizing and exiting such condit...

Effective: Mar 25, 1998 Category: aircraft Compliance: Effective date as specified in the AD, requiring compliance within a set timeframe after publicat...

Why matched: Airworthiness Directives; Mitsubishi Model YS-11 and YS-11A Series Airplanes