Tech Specs
General
Capacity
 |
Engines
| Turbofans Thrust: | 6,100 lb (27.13 kN) |
|---|---|
| Flat rated to: | ISA + 15°C (86°F) |
Avionics
- Rockwell Collins Pro Line Fusion avionics suite, with three 15.1” (38.4 cm) Active Matrix Liquid Crystal Displays (AMLCD)
- Electronic Flight Instrument System (EFIS)
- Dual automatic Attitude Heading Reference System (AHRS)
- Integrated Flight Information System (IFIS) with electronic charts
- One Class II Electronic Flight Bag (EFB)
- Synthetic Vision System for Situational Awareness (SVS)
- Terrain Awareness and Warning System (TAWS)
- Dual Flight Management System (FMS)
- Weather Radar System
Performance
Range
| Maximum range (±5%): | 3,000 NM 3,455 SM 5,556 km |
|---|---|
| (Range with 2 crew, 4 passengers (200 lb each) and 100 NM NBAA IFR reserves. Assumes standard BOW,sea level departure and landing, unrestricted climb,cruise and descent with zero wind and standard (ISA) conditions en route.) | |
Speed
| Mach | kt | mph | km/h | |
| High-speed | 0.82 | 470 | 541 | 871 |
|---|---|---|---|---|
| (at 43,000 ft, 31,200 lb cruise weight, standard ISA conditions) | ||||
| Long-range speed (±3%) | 0.78 | 447 | 515 | 829 |
| (at 45,000 ft, 31,200 lb cruise weight, standard ISA conditions) | ||||
Airfield Performance
| Takeoff distance (±5%): | 4,800 ft 1,463 m |
|---|---|
| (SL, ISA, MTOW. Field lengths are based on a level hard surface, dry paved runway with zero wind.) | |
| Landing distance (±5%): | 2,700 ft |
| (SL, ISA, MLW, 14CFR 91. Field lengths are based on a level hard surface, dry paved runway with zero wind.) | |
Operating Altitude
| Maximum operating altitude: | 49,000 ft 14,935 m |
|---|---|
| Initial cruise ceiling: (SL, ISA, MTOW) |
43,000 ft 13,106 m |
Approximative Dimensions
External Dimensions
| Length: | 68.4 ft 20.84 m |
|---|---|
| Wingspan (overall): | 61.5 ft 18.75 m |
| Wing area (basic): | 401.0 ft² 37.25 m² |
| Height overall: | 19.6 ft 5.97 m |
Internal Dimensions
| Cabin length (±1%): (from cockpit divider to end of pressurized compartment) |
24.75 ft 7.54 m |
|---|---|
| Cabin width (±1%): (maximum) |
6.08 ft 1.85 m |
| Cabin height (±1%): (maximum over aisle) |
5.91 ft 1.80 m |
| Cabin volume: (from cockpit divider to aft lavatory bulkhead) |
665 ft³ 18.83 m³ |
Weights
| A. | Maximum ramp weight (±2%): |
33,750 lb 15,309 kg |
|---|---|---|
| B. | Maximum takeoff weight (±2%): |
33,500 lb 15,195 kg |
| C. | Maximum landing weight (±2%): |
30,150 lb 13,676 kg |
| D. | Maximum zero fuel weight (±2%): |
24,200 lb 10,977 kg |
| E. | Standard basic operating weight† (±2%): |
21,500 lb 9,752 kg |
| † Includes unusable fuel, oil, standard interior, standard avionics, paint and 2 crew. Actual weight will vary with individual aircraft as a result of customization and optional equipment. | ||
Disclaimer
The aircraft is currently under development and the design and the design tolerances remain to be finalized and certified. The aircraft is subject to change during the course of the design, manufacture and certification process. The statements about performance, design, design tolerances and the images shown in this document are solely based on projections and forecasts and are subject to change without notice. All competitive data is based upon public information derived from third party sources. This document and the information contained herein does not constitute an offer, commitment, representation or warranty of any kind with respect to the aircraft. The actual configuration and performance of the aircraft shall be subject of a purchase agreement between the buyer and Learjet.