{"content":[{"text":"Fiberglas-Technik \n Rudolf Lindner \n EASA AP.161","bbox":{"left":0.132256,"top":0.042716,"width":0.134174,"height":0.044196000000000006}},{"text":"Repair Instructions (RI-G01) \n „Standard Repairs“","bbox":{"left":0.346773,"top":0.042716,"width":0.210727,"height":0.030133}},{"text":"Grob \n Sailplanes \n EASA.A.250","bbox":{"left":0.625803,"top":0.042716,"width":0.094082,"height":0.043816}},{"text":"Page 5 of 8","bbox":{"left":0.732255,"top":0.042716,"width":0.08681499999999998,"height":0.01645}},{"text":"Edition 22.07.2014","bbox":{"left":0.732256,"top":0.070082,"width":0.14077699999999993,"height":0.016449999999999992}},{"text":"REPAIR INSTRUCTIONS No. RI-G01 \n I. TECHNICAL DETAILS \n 1. Aircraft affected:","bbox":{"left":0.118952,"top":0.107004,"width":0.647338,"height":0.09485199999999998}},{"text":"Grob Sailplanes (TCDS EASA.A.250), \n all models, all serial numbers","bbox":{"left":0.118952,"top":0.215092,"width":0.323252,"height":0.033692}},{"text":"i.e. the following models:","bbox":{"left":0.118952,"top":0.261556,"width":0.205252,"height":0.018015000000000003}},{"text":"ASTIR CS / ASTIR CS 77 / ASTIR CS JEANS / STANDARD ASTIR II / CLUB ASTIR II / \n G 102 STANDARD ASTIR III / G 102 CLUB ASTIR III / G 102 CLUB ASTIR IIIb","bbox":{"left":0.118952,"top":0.292343,"width":0.722046,"height":0.03340799999999999}},{"text":"SPEED ASTIR II / SPEED ASTIR IIb","bbox":{"left":0.118952,"top":0.338523,"width":0.301822,"height":0.018015000000000003}},{"text":"TWIN ASTIR / TWIN ASTIR TRAINER / G 103 TWIN II / G 103A TWIN II ACRO / \n G 103C TWIN III ACRO / G 103C TWIN III","bbox":{"left":0.118952,"top":0.36931,"width":0.669068,"height":0.033408999999999967}},{"text":"G 103C TWIN III SL","bbox":{"left":0.118952,"top":0.41549,"width":0.16550000000000004,"height":0.018015000000000003}},{"text":"2. Subject","bbox":{"left":0.118952,"top":0.446627,"width":0.08838800000000002,"height":0.018054999999999988}},{"text":"ATA-Code:","bbox":{"left":0.11895,"top":0.477637,"width":0.09245799999999998,"height":0.018015000000000003}},{"text":"51 \n Standard Practices and Structures – General \n Approved Repair Instructions according to Part-21 and Part-M","bbox":{"left":0.2399,"top":0.477637,"width":0.512172,"height":0.04880200000000001}},{"text":"3. Introduction \n This Repair Instruction is issued for the purpose to prevent single approvals for commonly \n used standard repairs, which are not covered in the corresponding Maintenance Manuals. \n Standard Repairs are repairs, that restore the original design without change by application of \n approved slice ratios, materials und curing procedures. Following the information listed in para. \n 4 „Accomplishment/ Instructions“ repairs may be regarded as approved by the manufacturer in \n the sense of the EASA regulation Part-21 para. 21.A.433.","bbox":{"left":0.11895,"top":0.53956,"width":0.783673,"height":0.11059799999999997}},{"text":"Prepared:","bbox":{"left":0.11895,"top":0.914987,"width":0.065409,"height":0.015971999999999986}},{"text":"Verified:","bbox":{"left":0.385079,"top":0.914987,"width":0.06088100000000002,"height":0.015971999999999986}},{"text":"Complies:","bbox":{"left":0.650803,"top":0.914987,"width":0.069214,"height":0.015971999999999986}}],"images_bbox":[{"left":0.21774,"top":0.909921,"width":0.114514,"height":0.037343}],"images_bbox_not_text_overlap":[{"left":0.21774,"top":0.909921,"width":0.114514,"height":0.037343}]}