Search FAA Documents

21 results found (1153ms)

Sort by: Date AD Number

Amdt-39-17690 Recurring

final rule

Airworthiness Directives; Maule Aerospace Technology, Inc. Airplanes

Unsafe Condition: Internal corrosion in wing lift struts, part numbers 2079E and/or 2080E, could lead to structural failure of the wing lift struts.

Effective: Jan 21, 2014 Category: aircraft Compliance: Within 50 flight hours after the effective date of this AD.

Why matched: Airworthiness Directives; Maule Aerospace Technology, Inc. Airplanes

98-15-18 R1

final rule

Airworthiness Directives; Maule Aerospace Technology, Inc. Airplanes

Unsafe Condition: Internal corrosion of wing lift struts, part numbers 2079E and/or 2080E, could result in reduced structural integrity.

Effective: Jan 21, 2014 Category: aircraft Compliance: Effective January 21, 2014

Why matched: Airworthiness Directives; Maule Aerospace Technology, Inc. Airplanes

2008-24-02

final rule

Airworthiness Directives; Maule Aerospace Technology, Inc. M-4, M-5, M-6, and M-7 Series and Model M-8-235 Airplanes

Unsafe Condition: Reversed elevator control rigging could result in elevator movement in the opposite direction from control input, leading to loss of control.

Effective: Dec 30, 2008 Category: aircraft Compliance: Within 12 months of the effective date (December 30, 2008).

Why matched: Airworthiness Directives; Maule Aerospace Technology, Inc. M-4, M-5, M-6, and M-7 Series and Model M-8-235 Airplanes

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

2000-09-06

final rule

Airworthiness Directives; Maule Aerospace Technology, Inc. M-4, M-5, M-6, M-7, MX-7, and MXT-7 Series Airplanes and Models MT-7-235 and M-8-235 Airplanes

Unsafe Condition: Improper crimping of the Nicopress™ sleeve terminal ends could cause a control cable to slip from the sleeve, potentially leading to loss of rudder, elevator, aileron, or flap control.

Effective: May 30, 2000 Category: aircraft Compliance: Within 50 flight hours after the effective date of the AD.

Why matched: Airworthiness Directives; Maule Aerospace Technology, Inc. M-4, M-5, M-6, M-7, MX-7, and MXT-7 Series Airplanes and Models MT-7-235 and M-8-235 Airplanes

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

97-26-14

final rule

Airworthiness Directives; MAULE Models MX-7-420 and MXT-7-420 Airplanes and Models M-7-235 and M-7-235A Airplanes Modified in Accordance With Maule Supplemental Type Certificate (STC) SA2661SO

Unsafe Condition: Loss of airplane control 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: Jan 28, 1998 Category: aircraft Compliance: within the next 30 days after the effective date of this AD

Why matched: Airworthiness Directives; MAULE Models MX-7-420 and MXT-7-420 Airplanes and Models M-7-235 and M-7-235A Airplanes Modified in Accordance With Maule Supplemental Type Certificate (STC) SA2661SO

96-10-05

final rule

Airworthiness Directives; Maule Aerospace Technologies, Inc. Models M-4-210 and M-4-210C Airplanes

Unsafe Condition: The close proximity of the flammable fuel to the exhaust system presents an unsafe condition and violates current regulations.

Effective: Jun 21, 1996 Category: aircraft Compliance: within the next 50 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Maule Aerospace Technologies, Inc. Models M-4-210 and M-4-210C Airplanes

86-17-11

final rule

Airworthiness Directives; Maule Model M-5-180C, M-5-210C, M-5-220C and M-5-235C Series Airplanes

Unsafe Condition: Restricted fuel flow in the fuel crossover supply line due to line collapse or improper installation forward of the front fuselage seat support frame.

Effective: Sep 3, 1986 Category: aircraft Compliance: within the next 25 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; Maule Model M-5-180C, M-5-210C, M-5-220C and M-5-235C Series Airplanes

84-09-07

final rule

Airworthiness Directives; Maule Model M-4 and M-5 Series Airplanes

Unsafe Condition: Plug type drain fittings in the main and auxiliary fuel tanks may fail to provide a convenient means to drain fuel system water contamination.

Effective: May 12, 1984 Category: aircraft Compliance: within the next 50 hours time-in-service

Why matched: Airworthiness Directives; Maule Model M-4 and M-5 Series Airplanes

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

82-03-05

final rule

Airworthiness Directives; Maule Model M-5-235C and M-6-235 Series Airplanes

Unsafe Condition: Engine stoppage prevention due to potential blockage in the engine alternate air hose.

Effective: Feb 11, 1982 Category: aircraft Compliance: within the next 25 hours time in service after the effective date of this AD unless already accom...

Why matched: Airworthiness Directives; Maule Model M-5-235C and M-6-235 Series Airplanes

81-25-01

final rule

Airworthiness Directives; WOODWARD GOVERNOR COMPANY Model F210681 Serial Numbers 1446751 through 1446783, 1446785 through 1446806, 1446808, 1446809, 1446811, 1446812, 1446814 through 1446817, 1567547 through 1567562, 1567564 through 1567594, and 1567596 through 1567612

Unsafe Condition: Failure of the flyweights

Effective: Dec 7, 1981 Category: appliance Compliance: Within the next 50 hours time in service from the effective date of this AD

Why matched: Airworthiness Directives; WOODWARD GOVERNOR COMPANY Model F210681 Serial Numbers 1446751 through 1446783, 1446785 through 1446806, 1446808, 1446809, 1446811, 1446812, 1446814 through 1446817, 1567547 through 1567562, 1567564 through 1567594, and 1567596 through 1567612

81-14-02

final rule

Airworthiness Directives; Maule Model M-4, M-4-210C, M-4-220S, M-4-220C, M-4-180C, M-5-220C, M-5-210C, M-5-235C, M-5-180C and M-5-210TC Series Airplanes

Unsafe Condition: Failure of the rudder pedal V-bar and associated structure of the rudder bar.

Effective: Jul 1, 1981 Category: aircraft Compliance: within 25 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Maule Model M-4, M-4-210C, M-4-220S, M-4-220C, M-4-180C, M-5-220C, M-5-210C, M-5-235C, M-5-180C and M-5-210TC Series Airplanes

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

79-12-01

final rule

Airworthiness Directives; Maule M-4-210C, M-4-220S, M-4-220C, M-4-180C, M-5-210C, M-5-220C, M-5-235C, M-5-180C, and M-5-210TC Airplanes

Unsafe Condition: Failure of the horizontal tail-to-fuselage front attach tube.

Effective: Jun 7, 1979 Category: aircraft Compliance: within 25 hours' time in service after the effective date of this AD, or 60 days after the effect...

Why matched: Airworthiness Directives; Maule M-4-210C, M-4-220S, M-4-220C, M-4-180C, M-5-210C, M-5-220C, M-5-235C, M-5-180C, and M-5-210TC Airplanes

78-13-08

final rule

Airworthiness Directives; Maule Models M-5-210C and M-5-235C

Unsafe Condition: Deformed fuel line tubes and hexagonal head clamps could reduce fuel feed or supply to the engine.

Effective: Jul 5, 1978 Category: aircraft Compliance: within the next 25 hours' time in service

Why matched: Airworthiness Directives; Maule Models M-5-210C and M-5-235C

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

75-11-02

final rule

Airworthiness Directives; Maule Models M-4-210, M-4-210C, and M-5-210C

Unsafe Condition: Fuel leakage in the cabin area and reduced fuel line flexibility due to cracking around flares on the short line and inadequate design of the long line.

Effective: May 19, 1975 Category: aircraft Compliance: within the next 30 hours' time in service after the effective date of this AD unless already acco...

Why matched: Airworthiness Directives; Maule Models M-4-210, M-4-210C, and M-5-210C

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

73-11-06

final rule

Airworthiness Directives; Maule Models M-4-180 and M-4-220

Unsafe Condition: Engine overheat during climb and incorrect cylinder head temperature reading

Effective: May 29, 1973 Category: aircraft Compliance: within the next 50 hours' time in service after the effective date of this airworthiness directive

Why matched: Airworthiness Directives; Maule Models M-4-180 and M-4-220

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

71-17-01

final rule

Airworthiness Directives; Maule Model M-4-180 and M-4-220

Unsafe Condition: Fuel line blockage due to low spots and inadequate firewall fire protection from an aluminum fuel feed line firewall bulkhead fitting.

Effective: Aug 16, 1971 Category: aircraft Compliance: within the next 50 hours' time in service after the effective date of this airworthiness directive

Why matched: Airworthiness Directives; Maule Model M-4-180 and M-4-220

71-06-06

final rule

Airworthiness Directives; Maule M-4-180C and M-4-220C

Unsafe Condition: Seat track and seat track guide spacing could allow the seat to become free from the guides.

Effective: Mar 16, 1971 Category: aircraft Compliance: within the next 10 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Maule M-4-180C and M-4-220C

69-20-02

final rule

Airworthiness Directives; Maule M-4, M-4T, M-4C, M-4S, M-4-210, M-4-210C, and M-4-220C

Unsafe Condition: The most forward aileron control system pulley, mounted on the lower portion of the control column, may separate from its bearing.

Effective: Sep 30, 1969 Category: aircraft Compliance: within the next 25 hours' time in service after the effective date of this airworthiness directiv...

Why matched: Airworthiness Directives; Maule M-4, M-4T, M-4C, M-4S, M-4-210, M-4-210C, and M-4-220C

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

68-07-08

final rule

Airworthiness Directives; Maule Models M-4, M- 4C, M-4S, M-4T, M-4-210, M-4-210C, and M-4-220S Series Aircraft

Unsafe Condition: Loss of rudder trim tab control and resultant interference with aileron operation.

Effective: Apr 11, 1968 Category: aircraft Compliance: Within the next 50 hours' time in service after the effective date of the airworthiness directive

Why matched: Airworthiness Directives; Maule Models M-4, M- 4C, M-4S, M-4T, M-4-210, M-4-210C, and M-4-220S Series Aircraft

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

65-28-04

final rule

Airworthiness Directives; Maule Model M-4-210 Airplanes

Unsafe Condition: Loss of engine power due to fuel starvation

Effective: Jan 13, 1966 Category: aircraft Compliance: within the next 100 hours' time in service after the effective date of this AD unless already acc...

Why matched: Airworthiness Directives; Maule Model M-4-210 Airplanes

65-18-01

final rule

Airworthiness Directives; MAULE Models Be Dee M-4, M-4 and M-4-210 Airplanes

Unsafe Condition: Failure of the attachment of the fuselage fabric to the windshield channel

Effective: Aug 17, 1965 Category: aircraft Compliance: within the next 50 hours' time in service after the effective date of this AD unless already acco...

Why matched: Airworthiness Directives; MAULE Models Be Dee M-4, M-4 and M-4-210 Airplanes