Manuel de montage

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B14) trim sleeves and cables 357. Position the metallic sleeve end on the cable sleeves and slide Install into the sleeves. Position the sleeves on the airframe. Fit the metallic sleeve end so that the cables are lined up with the pulley Sleeves must be enough long at the tubes junction to permit cable movement. The cable goes two and a half laps around the pulley and is stopped by a parker screw. free A B14 s.a. ASSEMBLY MANUAL XAIR HANUMAN 2009, July, 21 ©Randkar 2009 Prohibited reproduction / Reproduction interdite KAR RAND Page 36 / 85 B14) gaines et câbles de trim 357. Positionner la butée de gaine sur les gaines et introduire le câble dans les Poser Positionner les gaines sur la cellule. Positionner la butée de gaine sur le tube 370 de façon à ce que les câbles soient dans l’axe des gorges de la poulie. Fixer la butée de gaine sur le tube avec les rivets. gaines. suffisamment de mou dans la gaine au niveau des articulations des tubes pour permettre le débattement. Le câble fait deux tours et demi autour de la poulie et est bloqué par une vis parker. Laisser 22 cm
C B15) and torque all the bolts already installed, except upper front fork bolt (A). Glue B15) harness cables in the fuselage(B15D). D shoulder Fit A B B15 et serrer toute la boulonnerie déjà installée sauf le boulon de fourche avant (A), Fixer les câbles des harnais Coller d’épaule dans le fuselage (B15D). RAND KAR s.a. ASSEMBLY MANUAL XAIR HANUMAN 2009, July, 21 ©Randkar 2009 Prohibited reproduction / Reproduction interdite Page 37 / 85
Page 1 and 2: Assembly manual Manuel de montage *
Page 3 and 4: IMPORTANTES RECOMMANDATIONS POUR L'
Page 5 and 6: A/ AIRFRAME ASSEMBLY A/ MONTAGE DE
Page 7 and 8: A3) the rear cockpit side tubes 341
Page 9 and 10: A7) cockpit front horizontal tube 3
Page 11 and 12: A10) rear under floor tube 362. Par
Page 13 and 14: A14) nylon housings with silicon gr
Page 15 and 16: A18 ) the plate 336 on the ground b
Page 17 and 18: A22) A22) aileron control system 35
Page 19 and 20: A24) the frame one side on the floo
Page 21 and 22: A26) A26) handles 337. throttle Ins
Page 23 and 24: A28) the wheel axels and install fr
Page 25 and 26: B2) frame 336 that bear the rudder
Page 27 and 28: B4) the stabilizer leading edge sup
Page 29 and 30: B7) longitudinal fuselage stiffener
Page 31 and 32: B9) longitudinal fuselage battens 3
Page 33 and 34: B11) the two plates from the tip of
Page 35: B13) B13) fork 319. Apply silicon g
Page 39 and 40: B17) sail 334377 with luggage rack
Page 41 and 42: C2) rudder horn on rudder (see draw
Page 43 and 44: C4) C4) if the aircraft must be equ
Page 45 and 46: D2) Position firewall 384 in front
Page 47 and 48: BC A D4) a stripe of 3cm wide of th
Page 49 and 50: B A D5-Jabiru RAND KAR s.a. ASSEMBL
Page 51 and 52: D8) D8) in its housing 386 Install
Page 53 and 54: D11) seats 380 in their railings. S
Page 55 and 56: ROTAX 582 RAND KAR s.a. ASSEMBLY MA
Page 57 and 58: E3) Install E2) the choke handle an
Page 59 and 60: A E6) E6) floor cover 377. under Fi
Page 61 and 62: F1C KAR s.a. ASSEMBLY MANUAL XAIR H
Page 63 and 64: F3) that the wing twist is similar
Page 65 and 66: F5) you have clean hands. Position
Page 67 and 68: F7) F7) sail tension at the wing ro
Page 69 and 70: F11) F11) cockpit sides 383 right a
Page 71 and 72: B G3) ailerons 306. Ailerons being
Page 73 and 74: H2) H2) spats 379 wheel Install H3)
Page 75 and 76: alance Weighing operation must be d
Page 77 and 78: Page 77 / 85 Centrage L’appareil
Page 79 and 80: DÉMONTAGE ET TRANSPORT préparatio
Page 81 and 82: RAND KAR s.a. ASSEMBLY MANUAL XAIR
Page 83 and 84: RAND KAR s.a. ASSEMBLY MANUAL XAIR
Page 85: FORMULAIRE DE GARANTIE A RETOURNER

Manuel de montage

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