Manuel de montage

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B1) fuselage upper tubes 318R and L and lower tubes 317R and L on the airframe. Fit B1) fin leading edge 321 on one of tubes 318, then on the second and then on tubes 317. NOTE:Do not apply loctite on the screws fitted in the nutserts. the Fit D A B1 B/ FUSELAGE B C KAR s.a. ASSEMBLY MANUAL XAIR HANUMAN 2009, July, 21 ©Randkar 2009 Prohibited reproduction / Reproduction interdite B1C B1D RAND Page 24 / 85 les tubes de fuselage arrière supérieurs 318 (droit et gauche) et inférieurs 317 (droite et gauche) sur la cellule. Fixer le bord de fuite 321 sur un des tubes 318, puis sur l’autre, puis sur les tubes 317. NOTE:Les vis fixées dans les inserts ne doivent pas être collées. Fixer B1A B1B
B2) frame 336 that bear the rudder cables and the rear elevator control tube. Install B2 A B2) le cadre 336 qui supporte les câbles de direction et la commande de profondeur. Poser B2A RAND KAR s.a. ASSEMBLY MANUAL XAIR HANUMAN 2009, July, 21 ©Randkar 2009 Prohibited reproduction / Reproduction interdite Page 25 / 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: A28) the wheel axels and install fr
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 and 36: B13) B13) fork 319. Apply silicon g
Page 37 and 38: C B15) and torque all the bolts alr
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
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Manuel de montage

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