Division Beechcraft 1900 Series Aeroplanes - AD/BEECH 1900/2 Amdt 2 - Nose Gear Lower Shock Absorber Assembly - Beechcraft 1900 Series Aeroplanes

Beechcraft 1900 Series Aeroplanes

AD/BEECH 1900/2 Amdt 2	Nose Gear Lower ShockAbsorber Assembly	7/2007

Applicability:	Model 1900, serial numbers UA-1 through UA-3.Model 1900C, serial numbers UB-1 through UB-74, and UC-1 through UC-78.
Requirement:	1. Inspect, using fluorescent liquid penetrant or magnetic particle method, the nose landing gear fork assembly for cracks, in accordance with Part II of Raytheon Aircraft Company Mandatory Service Bulletin (MSB) SB 32-2102 Revision 7, Revised: July 2003.2. If cracks are found during the Requirement 1 inspection, incorporate Kit No.101-8030-1 S or Kit No. 114-8015-1 S, as applicable; as specified in MSBSB 32-2102 Revision 7, Revised: July 2003.3. If no cracks are found during the Requirement 1 inspection, repeat the inspection in accordance with Part II of MSB SB 32-2102 Revision 7, Revised: July 2003.Note 1: Incorporation of Kit No. 101-8030-1 S or Kit No. 114-8015-1 S, as applicable, is terminating action for the inspection requirements of this Directive.Note 2: FAA Corrected AD 2004-23-02 Amdt 39-13857 refers.
Compliance:	1.a. For aircraft affected by the previous issue of this Directive, initially inspect within 200 hours time in service after the last inspection required by the previous issue of this Directive.1.b. For aircraft not affected by the previous issue of this Directive, initially inspect within 200 hours time in service after 5 July 2007.2. Before further flight.3. At intervals not to exceed 200 hours time in service. If cracks are found during any inspection, incorporate Kit No. 101-8030-1 S or Kit No. 114-8015-1 S, as applicable.The compliance times for Requirements 2 and 3 remain unchanged by this issue of the Directive.

Applicability:

Model 1900, serial numbers UA-1 through UA-3.Model 1900C, serial numbers UB-1 through UB-74, and UC-1 through UC-78.

Requirement:

1. Inspect, using fluorescent liquid penetrant or magnetic particle method, the nose landing gear fork assembly for cracks, in accordance with Part II of Raytheon Aircraft Company Mandatory Service Bulletin (MSB) SB 32-2102 Revision 7, Revised: July 2003.2. If cracks are found during the Requirement 1 inspection, incorporate Kit No.101-8030-1 S or Kit No. 114-8015-1 S, as applicable; as specified in MSBSB 32-2102 Revision 7, Revised: July 2003.3. If no cracks are found during the Requirement 1 inspection, repeat the inspection in accordance with Part II of MSB SB 32-2102 Revision 7, Revised: July 2003.Note 1: Incorporation of Kit No. 101-8030-1 S or Kit No. 114-8015-1 S, as applicable, is terminating action for the inspection requirements of this Directive.Note 2: FAA Corrected AD 2004-23-02 Amdt 39-13857 refers.

Compliance:

1.a. For aircraft affected by the previous issue of this Directive, initially inspect within 200 hours time in service after the last inspection required by the previous issue of this Directive.1.b. For aircraft not affected by the previous issue of this Directive, initially inspect within 200 hours time in service after 5 July 2007.2. Before further flight.3. At intervals not to exceed 200 hours time in service. If cracks are found during any inspection, incorporate Kit No. 101-8030-1 S or Kit No. 114-8015-1 S, as applicable.The compliance times for Requirements 2 and 3 remain unchanged by this issue of the Directive.

	This Airworthiness Directive becomes effective on 5 July 2007.
Background:	The manufacturer required a mandatory inspection of the nose gear lower shock absorber for evidence of slippage at the intersection of the tube and fork assembly, and a dye check of the weld area on the fork assembly.Amendment 1 required the same inspection requirements by a different inspection method, but required incorporation of an improved nose landing gear fork kit anytime a crack is found; and added additional aircraft to applicability.Amendment 2 is issued to correct an error in Requirement 3, where Part III of the referenced Beech MSB should have been Part II. This error flowed from related FAA AD 2004-23-02.

This Airworthiness Directive becomes effective on 5 July 2007.

Background:

The manufacturer required a mandatory inspection of the nose gear lower shock absorber for evidence of slippage at the intersection of the tube and fork assembly, and a dye check of the weld area on the fork assembly.Amendment 1 required the same inspection requirements by a different inspection method, but required incorporation of an improved nose landing gear fork kit anytime a crack is found; and added additional aircraft to applicability.Amendment 2 is issued to correct an error in Requirement 3, where Part III of the referenced Beech MSB should have been Part II. This error flowed from related FAA AD 2004-23-02.

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David Punshon
Delegate of the Civil Aviation Safety Authority

9 May 2007

Beechcraft 1900 Series Aeroplanes

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