1970 Swearingen SA26-AT Merlin II-B
Description
The Swearingen SA26-AT Merlin II-B is a light twin-engine business aircraft, designed and built by Swearingen Aircraft. It is a pressurized, all-metal aircraft, with retractable tricycle landing gear. It is powered by two Lycoming TIO-540-A1A turbocharged engines, each producing 300hp. It has a maximum cruise speed of 250 knots (288 mph), a range of 1,000 nautical miles, and a service ceiling of 25,000 feet. The aircraft has seating for up to five passengers, and is capable of operating from most airports. It is certified for single-pilot operation.
Features
- Total Time: 8333
- Left engine TPE331-1 w/ National Flight- Super One conversion (STC), 1560 hrs. since rebuild
- RH engine TPE331-1 w/ National Flight- Super One conversion (STC), 1560 hrs. since rebuild, 25 hrs on fresh hot section due to FOD event
- 8 hrs on both props since rebuild
- Com 1, Nav 1: Garman 530W, XM Weather, TISS
- Com 2, Nav 2: Garman 430W
- Com 3, Nav 2; Collins
- Garman GMA340 Audio Panel
- Dual Garman 330 transponders, #1 has ES (ADSB)
- HSI w/Flight Director
- Full co-pilot instrumentation
- Collins ADF
- Bendix: Fully Coupled Auto Pilot
- Bendix: Color Scan Weather Radar-inop
- Fuel Totalizer
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