1977 Learjet 36A
Description
The Learjet 36A is a light business jet aircraft produced by Learjet in the 1970s. The Learjet 36A is based on the Learjet 35, with a modified wing and a more powerful engine. The Learjet 36A is powered by two Garrett TFE731-2-2B engines, each producing 3300 lbf of thrust. The aircraft has a maximum speed of 440 knots and a range of 1,830 nm. The Learjet 36A can carry up to eight passengers and two crew members. The aircraft has a maximum takeoff weight of 14,000 lbs and a maximum landing weight of 12,500 lbs. The Learjet 36A has a service ceiling of 45,000 feet.
Features
- Total Time: 15600
- SMPI 130.9/413.5
- SCZI 130.9/3295.8
- Excellent records and maintenance history
- Dual Collins VHF 22 Communication Radios, 8.33 MHz frequency spacing
- Dual Collins VIR 30 Navigation Radios
- Dual Collins DF-206 ADF
- Collins FD-108Y Flight Director
- Jet PN101 Flight Director Co-Pilot
- Primus 40 Color Weather Radar
- Dual Apollo 2101 GPS with world wide data base
- Dual Avtech 1250 Audio Systems
- Dual Collins TDR 90 Transponders
- Dual Collins DME 40
- Collins 7180 High Frequency Transceiver
- Sunair ASB 500 High Frequency Transceiver
- Dual Collins 332E-10 RMI
- IDC II Altitude Alerting and Reporting
- Jet FC-110 Auto Pilot
- Landmark TAWS
- RVSM
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