CTHIn ForceLegislation
AD/EMB-110/53 Amdt 2 - Nose Landing Gear Rotating Cylinder Assembly
Embraer EMB-110 (Bandeirante) Series AerEmbraer EMB-110 (Bandeirante) Series Aeroplanes
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Embraer EMB-110 (Bandeirante) Series Aeroplanes
| AD/EMB-110/53 Amdt 2 | Nose Landing GearRotating Cylinder Assembly | 13/2006 |
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| Applicability: | All Model EMB-110 aircraft. |
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| Requirement: | 1. Inspect the nose landing gear rotating cylinder assembly, externally using dye-penetrant method and internally using a boroscope, in accordance with Embraer Service Bulletin (SB) No. 110-32-0088 Revision 03.a. If any cracks are evident during the inspection, replace the rotating cylinder assembly before further flight.b. If severe corrosion but no cracks are evident during the inspection, before further flight, perform a Requirement 2 detailed bench inspection of the rotating cylinder assembly.c. If light corrosion but no cracks are evident during the inspection, return the rotating cylinder assembly to service and repeat Requirement 1 inspections at the times specified in Compliance 1.c.2. If no corrosion or cracks are evident during the Requirement 1 inspection, perform a detailed bench inspection of the rotating cylinder assembly in accordance with SB No. 110-32-0088 Revision 03.a. If severe corrosion or cracks are evident during the inspection, replace the rotating cylinder assembly before further flight.b. If no corrosion or cracks are evident during the inspection, before further flight, apply a protection on the internal area of the rotating cylinder assembly in accordance with SB No. 110-32-0088 Revision 03.c. If light corrosion, but no cracks are evident during the inspection, before further flight, apply a protection on the internal area of the rotating cylinder assembly in accordance with SB No. 110-32-0088 Revision 03, and repeat the Requirement 1 inspections at the times specified in Compliance 2.c.; until the required replacement.Note: Brazil CTA AD 2004-04-01 R1 refers. |
| Compliance: | 1. Within 150 flight hours or 120 calendar days after 28 July 2004, whichever occurs first.1.c. At intervals not to exceed 150 flight hours or 120 calendar days, whichever occurs first, until accumulating 600 flight hours or 12 calendar months after 28 July 2004, whichever occurs first; when a Requirement 2 detailed bench inspection is required.2. Within 600 flight hours or 12 calendar months after 28 July 2004, whichever occurs first.2.c. At intervals not to exceed 600 flight hours or 9 calendar months, whichever occurs first; until replacement of the rotating cylinder assembly, which must be accomplished before accumulating 3,000 flight hours or 36 months after 28 July 2004, whichever occurs first.The compliance times remain unchanged except for Requirement 3, which was deleted and incorporated into Compliance 2.c., by this issue of the Directive. |
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