- Total time
- 11,365 hr
- Year
- 1981
Specifications
Airframe
- Total time ·
- 11,365 hr
Performance (across variants)
- Range ·
- 1,400 nm
- Cruise ·
- 236 kt
- Service ceiling ·
- 32,500 ft
- MTOW ·
- 5,000 kg
- Passengers ·
- Up to 11
Description
Technical specifications Fuselage Dimensions Length : Height : Wing Span : Cabin Dimensions Length : Height : Width : Cabin Volume : Baggage Volume : Typical Configuration Crew : Passengers : Pressurization : Fuel Capacity Standard : Standard : Optional : Optional : Weight Max. Ramp : Max. Takeoff : Zero Fuel : Basic Operating : Max. Landing : Speed Vs Clean : Vso Landing : Normal Cruise TAS : Vmo (Max Op) IAS : V1 Takeoff : VFE Max Flap Ext : VLE Max Land Gear Ext : IFR Certification (IFR) : Climb Normal : Engine Out : Ceiling : Landing Performance FAA Field Length : Takeoff Performance SL ISA BFL : 5000' +20C BFL : Range Range : Tanks Full : Seats Full : Range (4 PAX) : Range (8 PAX) : Engines Number of : Make/Model(s) : Thrust (per engine) : Shaft (per engine) : Common TBO Hours : CHEYENNE IIXL US standard Model Market Summary 36.7 (ft) 12.8 (ft) 42.7 (ft) 12' 6'' (ft)(in) 4' 3'' (ft)(in) 4' 2'' (ft)(in) 197 (cb ft) 38 (cb ft) 2 8 5.5 (psi) 2,559 (lbs) 382 (gal) 0 0 9,540 (lbs) 9,474 (lbs) 7,600 (lbs) 5,875 (lbs) 9,000 (lbs) 86 (kn) 77 (kn) 265 (kn) 242 (kn) 96 (kn) 148 (kn) 153 (kn) Unknown 1,750 (fpm) 470 (fpm) 32,000 (ft) 2,446 (ft) 2,940 (ft) 4,100 (ft) 1,175 (nm) 0 (nm) 0 (nm) - 1,175 (nm) 2 Pratt & Whitney Canada Corporation PT6A-135A Pratt & Whitney Canada Corporation PT6A-135 0 (lbs) 750 (hp)
