Silverwing AEROPRAKT A22 FOXBAT, Руководство пользователя

Страница: 185 / 185

Page 186 - © SilverWing Aviation, 2005
10. Engine and monitoring instruments:
10.1. Rotax engine installation Checklist completed.
(This Checklist is supplied with the engine, file it with your Project records)
10.2.
Engine monitoring system checked as appropriate for type.
(Choice of several digital or analogue systems)
11. Propeller, backplate and spinner:
11.1. Standard prop is the 3-blade KievProp 283 series (71” diameter).
(For alternative propellers consult SilverWing Aviation)
11.2. Check security of prop-bolts, lock-wire, back-plate and spinner.
(Check this prior to engine test run, DO NOT run engine without prop)
12. Control deflections in degrees from the neutral position:
12.1. Tolerance allowed is plus or minus one degree in all cases.
12.2. Elevator: up 22, down 22.
12.3. Trim tab: up 20 (nose down), down 30 (nose up).
12.4. Rudder: 21 left, 21 right.
12.5. Ailerons: up 20, down 13.
12.6. Flaperon droop: First position 10, second position 20.
12.7. Re-confirm that items 12.2 to 12.6 are satisfactory.
13. C of G information, all units are metric:
13.1. Datum point is the front face of the Propeller Flange.
13.2. C of G range loaded is 1.5 to 1.7 aft of datum.
13.3. Nose wheel arm 0.48
13.4. Main wheel arm 1.80
13.5. Pilot/Passenger 1.6
13.6. Fuel 1.90
13.7. Baggage 2.20
13.8. Maximum empty weight 275 kgs
13.9. Maximum take off weight 525 kgs
13.10. Re-confirm that items 13.3 to 13.9 are satisfactory..
14. Airframe symmetry
14.1. Wingtips to prop flange are equal to within 5 mm.
14.2. Wingtips to elevator horn are equal to within 5 mm.
14.3. Wingtips to fuselage lift-strut mount are equal to within 3 mm.