Document ID: chunk:federal_register_of_legislation:F2006B08801:body:0:p5
Version: federal_register_of_legislation:F2006B08801
Segment Type: other
Provision Reference: 
Character Range: 10648–11590

doubler plates at the front and/or centre spar positions - within 1500 hours time in service since the last visual or X-ray inspection, for cracking at the inspection holes forward or aft of the front and centre spars.

                   (b)     Aircraft other than those specified in (a) above - initially within 8000 hours time in service since new or since rework in accordance with para. 2(b) of this Order and thereafter at intervals not exceeding 2500 hours time in service except that after rework in accordance with para. 2(b) of this Order, every second inspection may be made "in situ" by an X-ray technique approved by the Secretary.

               For Paragraphs 6(a) and 6(b): Initially within 8000 hours time in service since new and thereafter at intervals not exceeding 5000 hours time in service.

               For Paragraph 7(a): At intervals not exceeding 2000 hours time in service or two years whichever occurs first.