CTHIn ForceLegislation
AD/ROBIN/32 Amdt 2 - Wing Spars
Robin Aviation Series AeroplanesRobin Aviation Series Aeroplanes
Start here
Get a plain-English read of Robin Aviation Series Aeroplanes
Turn the raw legal text into a practical explanation grounded in AD/ROBIN/32 Amdt 2 - Wing Spars.
Robin Aviation Series Aeroplanes
| AD/ROBIN/32 Amdt 2 | Wing Spars | 6/2008 |
|---|
| Applicability: | All Model HR 100 series aircraft.Model HR200/100, HR200/100S, HR200/120, HR200/120B, and HR200/160 aircraft, serial numbers 001 through 378.Model R2100, R2100A, R2112, R2120U, and R2160D aircraft, serial numbers 001 through 378.Model R2160 aircraft, serial numbers 001 through 378, and serial number160A-06001 and subsequent.Model R2160i aircraft, serial numbers 001 through 378, and serial numbers160Ai-07007 and subsequent. |
|---|---|
| Requirement: | Remove the main landing gear legs and all the wing inspection panels in accordance with the instructions in the aircraft maintenance manual, and inspect the visible parts of the spar web and the upper and lower boom angles (top and bottom spar caps), in accordance with Avions Pierre Robin Service Letter (SL) No. 19 and Service Bulletin (SB) No. 99.If corrosion is found on the rear face of the spar web or the upper and lower boom angles, then inspect the front face of the spar for corrosion in accordance with SL No. 19 and SB No. 99. It may be necessary to cut inspection holes or remove the wings to inspect the front face of the spar. Inspection holes must be prepared to an approved repair scheme.Treat corrosion in accordance with SL No. 19 and SB No. 99, before further flight.If corrosion is found which exceeds the limits specified in SL No. 19, before further flight, repair in accordance with an approved repair scheme.If the spars are replaced, the inspections at intervals of 24 months must be resumed within 60 months from the date of replacement. |
| The requirements of this Directive are not applicable to aircraft that have been inspected within the last 72 months or are less than 72 months old, provided that these aircraft are maintained and continued to be maintained to an approved Alpha Aviation Design Ltd maintenance programme.Note: NZ CAA AD DCA/R2000/37B and EASA AD 2005-0028, refer. | |
|---|---|
| Compliance: | Within 60 months after aircraft date of manufacture and within 6 months for aircraft which are older than 60 months, unless accomplished within the last 24 months, and thereafter at intervals not to exceed 24 months. |
| This Amendment becomes effective on 5 June 2008. |