Bombardier Challenger 601-3R
The 601-3R is basically a 601-3A model with improved CF34-3A1 engines and both the fuselage tailcone tank and 2000 lb. gross weight increase options of the 601-3A as standard equipment. The major improvement incorporated in the CF34-3A1 engines is the designed airliner-type reliability necessary for its use on Canadair’s RJ regional jetliner version of the Challenger.The aircraft can be RVSM certified when service bulletin SB-601-0484 is complied with.
| Bombardier Challenger 601 3R | Specifications |
|---|---|
| Fuselage Dimensions | US standard |
| Length : | 68.5 (ft) |
| Height : | 20.8 (ft) |
| Wing Span : | 64.4 (ft) |
| Cabin Dimensions | |
| Length : | 28' 3'' (ft)(in) |
| Height : | 6' 0'' (ft)(in) |
| Width : | 8' 2'' (ft)(in) |
| Typical Configuration | |
| Crew : | 2 |
| Passengers : | 11 |
| Pressurization : | 8.8 (psi) |
| Fuel Capacity | |
| Standard : | 17,695 (lbs) |
| Standard : | 2,641 (gal) |
| Optional : | 0 |
| Optional : | 0 |
| Weight | |
| Max. Ramp : | 45,250 (lbs) |
| Max. Takeoff : | 45,100 (lbs) |
| Zero Fuel : | 31,000 (lbs) |
| Basic Operating : | 26,250 (lbs) |
| Max. Landing : | 36,000 (lbs) |
| Speed | |
| Vs Clean : | 123 (kn) |
| Vso Landing : | 103 (kn) |
| Normal Cruise TAS : | 476 (kn) |
| Vmo (Max Op) IAS : | 365 (kn) |
| Climb | |
| Normal : | 4,259 (fpm) |
| Engine Out : | 1,207 (fpm) |
| Ceiling : | 41,000 (ft) |
| Landing Performance | |
| FAA Field Length : | 3,300 (ft) |
| Takeoff Performance | |
| SL ISA BFL : | 6,050 |
| 5000' +20C BFL : | 11,094 |
| Range | |
| Range : | 3,580 (nm) |
| Engines | |
| Number of : | 2 |
| Model(s) : | CF34-3A1 |
| CF34-3B | |
| Thrust (per engine) : | 8,729 (lbs) |
| Shaft (per engine) : | 0 (hp) |
| Common TBO Hours : | 6,000 |
| Direct Cost Per Hour (US Standard) | Dollar (US) |
|---|---|
| Fuel | $1,438.4 |
| Fuel Cost Per Gallon | $4.64 |
| Additive Cost Per Gallon | 0 |
| Burn Rate (Gallons Per Hour) | 310 |
| Maintenance | $334 |
| Labor Cost Per Hour | $159 |
| Parts Cost Per Hour | $175 |
| Engine Overhaul | $433.33 |
| Thrust Reverse Overhaul | 13 |
| Miscellaneous Flight Expenses | 0 |
| Landing-Parking Fee | 0 |
| Crew Expenses | 0 |
| Supplies-Catering | 0 |
| Total Direct Costs | $2218.73 |
| Block Speed Statute Miles Per Hour | 408 |
| Total Cost Per Statute Mile | $5.44 |
| Annual Fixed Costs (US Standard) | Dollar (US) |
|---|---|
| Crew Salaries | $265,550 |
| Capt. Salary | $148,000 |
| Co-pilot Salary | $87,000 |
| Benefits | $30,550 |
| Hangar Cost | $97,000 |
| Insurance | $28,354 |
| Hull | $6,354 |
| Legal Liability | $22,000 |
| Misc. Overhead | $79,834 |
| Training | $45,667 |
| Modernization | $31,967 |
| Nav. Equipment | $2,200 |
| Depreciation | $132,375 |
| Total Fixed Costs | $603,113 |
| Annual Budget (US Standard) | Dollar (US) |
|---|---|
| Number of Seats | 11 |
| Miles | 200000 |
| Hours | 490 |
| Total Direct Costs | $1,087,178 |
| Total Fixed Costs | $603,113 |
| Total Cost (Fixed & Direct) | $1,690,291 |
| Cost/Hour | $3,449.57 |
| Cost/Statute Mile | $8.45 |
| Cost/Seat Mile | $0.77 |
| Total Cost (No Depreciation) | $1,557,916 |
| Cost/Hour | $3,179.42 |
| Cost/Statute Mile | $7.79 |
| Cost/Seat Mile | $0.71 |
