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2007-05-05

final rule

Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models M.S. 760, M.S. 760 A, and M.S. 760 B Airplanes

Unsafe Condition: unsafe condition on an aviation product.

Effective: Apr 9, 2007 Category: aircraft

Why matched: Airworthiness Directives; SOCATA--Groupe AEROSPATIALE Models M.S. 760, M.S. 760 A, and M.S. 760 B Airplanes

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

2001-06-05

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Unsafe Condition: Oil contamination in the gaseous oxygen system service compartment due to oil seeping out of the engine oil pump breather could result in a fire or explosion.

Effective: May 11, 2001 Category: aircraft Compliance: Within the next 100 hours time-in-service (TIS) after May 11, 2001 (the effective date of this AD).

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

98-24-04

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Unsafe Condition: Cracks in the web of the left and right flap carriages could result in loss of flap function with consequent reduced and/or loss of airplane control.

Effective: Dec 28, 1998 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD, and thereafter at ...

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

98-21-15

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Unsafe Condition: Failure of the oxygen generators caused by misalignment of the firing pin, which could result in crew incapacitation and loss of the airplane.

Effective: Nov 20, 1998 Category: aircraft Compliance: within 45 days after the effective date of this AD

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

98-18-13

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB20 and TB21 Airplanes

Unsafe Condition: Cracks in the main landing gear (MLG) attachment bearing could result in collapse of the main landing gear during taxi and landing operations.

Effective: Oct 24, 1998 Category: aircraft Compliance: Within the next 100 hours time-in-service after the effective date of this AD, or upon accumulati...

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB20 and TB21 Airplanes

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

98-08-21

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB10 and TB200 Airplanes

Unsafe Condition: Cracks in the wing rear attachment fittings could result in the wing separating from the airplane if operated with cracked fittings over an extended period of time.

Effective: Jun 3, 1998 Category: aircraft Compliance: prior to further flight after the inspection required by paragraph (a) of this AD

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB10 and TB200 Airplanes

98-08-27

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes.

Unsafe Condition: Interference between the side trim of the left-hand front side lower panel and the roll control compass on the left-hand wheel assembly could result in loss of directional control of the airplane.

Effective: May 31, 1998 Category: aircraft Compliance: within the next 100 hours time-in-service (TIS) after the effective date of this AD, unless alrea...

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes.

98-04-47

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB9, TB10, and TB200 Airplanes

Unsafe Condition: Cracks in the main landing gear (MLG) support ribs could cause MLG failure, resulting in loss of control during landing operations.

Effective: Apr 3, 1998 Category: aircraft Compliance: Upon accumulating 1,500/3,000/6,000 landings on MLG support ribs or within the next 75/100 landin...

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB9, TB10, and TB200 Airplanes

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

98-04-04

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Unsafe Condition: Failure of the starter generator mounting adapter could result in loss of electrical power.

Effective: Mar 24, 1998 Category: aircraft Compliance: within the next 25 hours time-in-service (TIS) after the effective date of this AD

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

98-04-03

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB9, TB10, TB20, TB21, and TB200 Airplanes

Unsafe Condition: Failure of the upper seat belt attachment caused by excessive loads on the upper attachment of the belt, which could result in bodily injury to the occupants during landing.

Effective: Mar 24, 1998 Category: aircraft Compliance: Within the next 50 hours time-in-service (TIS) after the effective date of this AD

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB9, TB10, TB20, TB21, and TB200 Airplanes

98-04-22

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE, Model TBM 700 Airplanes

Unsafe Condition: Flight in freezing rain, freezing drizzle, or mixed icing conditions may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in ice for...

Effective: Mar 13, 1998 Category: aircraft Compliance: Within 30 days after the effective date of this AD

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE, Model TBM 700 Airplanes

97-20-11

final rule

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

Unsafe Condition: Corrosion of the main landing gear (MLG) inboard door locking hooks (hinges) could cause the doors to jam and prevent the MLG from extending, leading to potential loss of control during landing ope...

Effective: Nov 13, 1997 Category: aircraft Compliance: within the next 100 hours time-in-service after the effective date of this AD or within 12 calend...

Why matched: Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Model TBM 700 Airplanes

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

92-06-08

final rule

Airworthiness Directives; GULFSTREAM AMERICAN Model GA-7 Airplanes

Unsafe Condition: Elevator binding and loss of pitch control, which could result in loss of control of the airplane.

Effective: Apr 17, 1992 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; GULFSTREAM AMERICAN Model GA-7 Airplanes

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

89-18-08

final rule

Airworthiness Directives; GULFSTREAM AEROSPACE CORPORATION Models AA-5, AA-5A, AA-5B, and GA-7 Airplanes

Unsafe Condition: Fuel tank/fuel system contamination caused by deterioration of fuel tank access cover sealant.

Effective: Sep 21, 1989 Category: aircraft Compliance: within the next 25 hours time-in-service after the effective date of this AD, unless already acco...

Why matched: Airworthiness Directives; GULFSTREAM AEROSPACE CORPORATION Models AA-5, AA-5A, AA-5B, and GA-7 Airplanes

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

85-26-05

final rule

Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes

Unsafe Condition: Failure of the rudder torque tube due to corrosion or cracks.

Effective: Jan 3, 1986 Category: aircraft Compliance: within 50 hours time-in-service after the effective date of this AD unless previously accomplished

Why matched: Airworthiness Directives; GULFSTREAM AEROSPACE Model GA-7 (Cougar) Airplanes

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

79-05-06

final rule

Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes

Unsafe Condition: Chafing and possible leakage of the main fuel feed line by the propeller control cable behind the firewall in the left hand engine nacelle.

Effective: Mar 9, 1979 Category: aircraft Compliance: Within the next 25 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes

79-05-07

final rule

Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes

Unsafe Condition: Fuel leakage from cracks in the inboard fuel tank ribs at Wing Station (W.S.) 109, at the forward fuel tank outlet fittings in the left and right wings.

Effective: Mar 9, 1979 Category: aircraft Compliance: within the next 25 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream American (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes

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

79-03-06

final rule

Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes

Unsafe Condition: Partial loss of rudder control due to excessive freeplay in the rudder assembly exceeding maximum allowed limits (.040 inches or 1 degree).

Effective: Feb 15, 1979 Category: aircraft Compliance: within 10 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation) Model GA-7 Airplanes

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

78-22-06

final rule

Airworthiness Directives; Gulfstream American Corporation (GAC) Model GA-7 Airplanes

Unsafe Condition: Failure of the elevator trim control master chain and loss of elevator trim control

Effective: Nov 2, 1978 Category: aircraft Compliance: within 5 flight hours of the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) Model GA-7 Airplanes

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

78-20-09

final rule

Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation (GAAC) Model GA-7 Airplanes

Unsafe Condition: Excessive force required to move the fuel selector valve from one position to another position creates a hazard to the airplane.

Effective: Oct 9, 1978 Category: aircraft Compliance: within the next 25 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Gulfstream American Corporation (GAC) (Formerly Grumman American Aviation Corporation (GAAC) Model GA-7 Airplanes

77-15-14

final rule

Airworthiness Directives; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes

Unsafe Condition: Cracks in the landing gear wheels, P/N 3760-A, could lead to wheel failure.

Effective: Aug 29, 1977 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; Morane Saulnier (Socata) Model MS 760 (Paris 1) and MS 760A (Paris 1A) Airplanes

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

76-06-07

final rule

Airworthiness Directives; Morane Saulnier Model 760B Paris II Airplanes

Unsafe Condition: Inflight fire caused by overpressure in the auxiliary fuel tanks.

Effective: Mar 25, 1976 Category: aircraft Compliance: Within the next 10 hours' time in service after the effective date of this AD (for some actions) ...

Why matched: Airworthiness Directives; Morane Saulnier Model 760B Paris II Airplanes

66-08-05

final rule

Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes

Unsafe Condition: Failure of the aluminum alloy rudder control system rod (P/N 0176-27.1.191) between Stations 5 and 10 could result in loss of rudder control.

Effective: Apr 16, 1966 Category: aircraft Compliance: within the next 300 hours' time in service after the effective date of this AD unless already acc...

Why matched: Airworthiness Directives; Morane-Saulnier Models M.S. 760, M.S. 760 A, and M.S. 760B Airplanes

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