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AD/BELL 205/70 Amdt 1 - Tail Rotor Blade Fwd Tip Weight Retention Block and Aft Tip Closure
Bell Helicopter Textron 205 Series HelicBell Helicopter Textron 205 Series Helicopters
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Bell Helicopter Textron 205 Series Helicopters
| AD/BELL 205/70 Amdt 1 | Tail Rotor Blade Fwd Tip WeightRetention Block and Aft Tip Closure | 13/2007 |
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| Applicability: | Model 205A, 205A-1, and 205B helicopters with a tail rotor blade part number212-010-750-009 through -129, all serial numbers, except serial numbers with a prefix of “A” or “AFS” and the number 11926, 13351, 13367, 13393, 13400, 13402, 13515, 13540, 13568, 13595 through 13602, 13619, and subsequent assigned numbers, installed. |
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| Requirement: | 1. Inspect the tail rotor blade forward tip weight retention block and aft tip closure for adhesive bond voids. Remove any tail rotor blade with a void in excess of that allowed by the Component Repair and Overhaul Manual limitations.2. Inspect the forward tip weight retention block attachment countersink screws in four locations to determine if the head of each countersink screw is flush with the surface of the abrasion strip. The locations of these four screws are depicted on Figure 1 of Bell Helicopter Textron Inc. Alert Service Bulletin (ASB) 205-00-80 Revision D or 205B-00-34 Revision D, or later FAA approved revisions, as applicable. If any of these screws are set below the surface of the abrasion strip or are covered with filler material, install shear pins in accordance with the Accomplishment Instructions, Part A, Shear Pin Installation paragraphs, of ASB 205-00-80 Revision D or 205B-00-34 Revision D, or later FAA approved revisions, as applicable.3. Install the aft tip closure rivets, re-identify the modified blade by adding an “FM”, and dynamically balance the tail rotor hub assembly in accordance with the Accomplishment Instructions, Part B, Aft Tip Closure Rivet Installation paragraphs, of ASB 205-00-80 Revision D or 205B-00-34 Revision D, or later FAA approved revisions, as applicable.Note: FAA AD 2007-22-02 Amdt 39-15238 refers. |
| Compliance: | Within 100 hours time in service after 20 December 2007, unless already accomplished. |
| This Amendment becomes effective on 20 December 2007. |
| Background: | The FAA received reports of five occurrences of missing tail rotor blade forward tip weight retention blocks or aft tip closures that resulted in minor to substantial damage. Such damage could result in loss of a tail rotor blade, and subsequent loss of control of the helicopter.Amendment 1 is issued in response to a new FAA AD, which expands the applicability to include other part and serial-numbered blades. Additionally, the AD clarifies the requirement to re-identify the modified blade by adding “FM” after the part number, and requires dynamically balancing the tail rotor. |
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