Velocity Edge GX570 Bedienungsanleitung Seite 1

Specification &DescriptionPreliminaryAugust 2011 Units 525-0800 to TBDExhibit APA No. _________________Please Sign and Date:Purchaser: __________

8August 2011, Preliminary7. LANDING GEARThe main and nose landing gear each use a singlewheel assembly. The landing gear retraction system iselectrica

August 2011, Preliminary9respective FADEC to deliver high pressure fuel to theengine. Some of that high pressure fuel from the FDU isrouted back to a

10August 2011, Preliminary10.1 GeneralThe Citation M2 features the Garmin G3000 advancedavionics system, a large-format glass cockpit with inte-grated

August 2011, Preliminary111 - Power Panel2 - Radio Call Placard3 - Master Caution / Warning Annunciators4 - Display Control Unit5 - Standby Flight Dis

12August 2011, Preliminary10. FLIGHT COMPARTMENT, INSTRUMENTATION AND AVIONICS(Continued)10.3 AvionicsDescribed below is the Citation M2 standard avio

August 2011, Preliminary1310. FLIGHT COMPARTMENT, INSTRUMENTATION AND AVIONICS(Continued)F. Air Data and Attitude informationThe pitot-static system i

14August 2011, Preliminary10. FLIGHT COMPARTMENT, INSTRUMENTATION AND AVIONICS(Continued)The GMC 710 Mode Controller, located just below theglareshiel

August 2011, Preliminary1510. FLIGHT COMPARTMENT, INSTRUMENTATION AND AVIONICS(Continued)T. Avionics Dispatch SwitchA Dispatch Power switch in the Ele

August 2011, Preliminary11. INTERIOR3FIGURE IV — CITATION M2 STANDARD FLOORPLANCABINDOORDEMERGENCYEXITD1109(#3)876542141312111210119(#6)9(#5)9(#4)1615

August 2011, Preliminary1711.2 Standard Interior ConfigurationThe following items are standard in the Citation M2.Numbered items refer to the cabin di

SPECIFICATION AND DESCRIPTIONUNITS 525-0800 TO TBDAUGUST 2011PRELIMINARYCitation MarketingCessna Aircraft CompanyP.O. Box 7706Wichita, Kansas 67277-77

18August 2011, Preliminary15. DOCUMENTATION AND TECHNICAL PUBLICATIONS14. EMERGENCY EQUIPMENT13. ADDITIONAL EQUIPMENT12. EXTERIOR•• U.S. Standard Airw

17. LIMITED WARRANTIESThe standard Citation M2 Aircraft Limited Warrantywhich covers the aircraft, other than Williams enginesand associated engine ac

20August 2011, Preliminary17. LIMITED WARRANTIES (Continued)service facility or a Citation service facility authorized byCessna to perform service on

18. CITATION M2 CREW TRAINING AGREEMENTAugust 2011, Preliminary21Training for one (1) Citation M2 crew will be furnished toFirst Retail Purchaser (her

Citation Marketing Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706, Telefax 316-517-6640

August 2011, Preliminary1INTRODUCTIONThis document is published for the purpose of providinggeneral information for the evaluation of the design, per-

2August 2011, PreliminaryTABLE OF CONTENTSCessna Citation M2 Specification and DescriptionSection Page1. General Description . . . . . . . . . . . . .

August 2011, Preliminary3MANUFACTURER CESSNA AIRCRAFT COMPANYMODEL 5251. GENERAL DESCRIPTIONThe Cessna Citation M2 is a low-wing aircraft withretracta

4August 2011, Preliminary1. GENERAL DESCRIPTION (Continued)13 ft 9 in(4.19 m)46 ft 11 in (14.30 m)18 ft 5 in (5.61 m)42 ft 7 in (12.98 m)15 ft 4 in (4

August 2011, Preliminary5FIGURE II — CITATION M2 INTERIOR DIMENSIONS1. GENERAL DESCRIPTION (Continued)57 in(1.45 m)107 in(2.72 m)25 in(.64 m)20 in (.5

6August 2011, Preliminary2. PERFORMANCE1. GENERAL DESCRIPTION (Continued)1.3 Design Weights and CapacitiesMaximum Ramp Weight . . . . . . . . . . . .

August 2011, Preliminary74. FUSELAGE3. STRUCTURAL DESIGN CRITERIAThe Citation M2 airframe is conventional in design,incorporating aluminum alloys, ste