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Symphony Specifications |
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| Engine | |
| Manufacturer | Textron Lycoming |
| Model | O-320-D2A, 160 horsepower |
| Type | 4 cylinder, direct drive, horizontally opposed |
| Maximum RPM | 2,700 |
| Induction System | Carbureted |
| Oil Capacity | 8 quarts |
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| Fuel | |
| Type | 100 LL AVGAS |
| Capacity | 29.1 gal. Usable |
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Propeller - Standard (cruise) |
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| Manufacturer | MT-Propeller |
| Model | 86 R 140-3D P-244-3 |
| Composition | Composite with stainless steel leading edge |
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| Propeller - Optional (climb) | |
| Manufacturer | Sensenich Propeller |
| Model | 74DM6S11-1-56 |
| Composition | Aluminum |
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| Avionics and Instruments | |
| VFR Avionics | Garmin GNC-250XL GPS/COMM and GTX-320A Transponder, Vision Microsystems: VM 1000 Engine Instrumentation, EC-100 Caution Advisory System, Fuel Level Monitoring, OAT/CAT, and Chronometer |
| IFR Avionics | Garmin GNS-430 GPS/COMM/VOR/LOC/GS, GNC-420 GPS/COMM, and GI-106A VOR/LOC glide slope indicator. Also with Garmin GTX-327 Transponder and GMA-340 audio panel. Vision Microsystems: VM 1000 Engine Instrumentation, EC-100 Caution Advisory System, Fuel Level Monitoring, OAT/CAT, and Chronometer |
| Glass IFR Package | Avidyne Entegra EXP5000 Primary Flight Display (PFD), Entegra EXP5000 Multi-Function Display (MFD), EMax™, Engine Indication System, Garmin GNS-430 GPS/COMM/VOR/LOC/GS, GNC-420 GPS/COMM, GMA Audio Panel, and GTX 327 Transponder |
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| Performance at 2150 lbs. GW |
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| Service Ceiling |
16.400 ft. |
| Cruise (75% pwr @ 8,000 ft.) | 128 KTAS |
| Rate of Climb (MSL) Standard Prop | 710 fpm |
| Rate of Climb (MSL) Climb Prop | 915 fpm |
| Stall Vs (flaps up) | 60 KIAS |
| Stall Vs (flaps full) | 51 KIAS |
| Landing (MSL-over 50 ft. obstacle) | 1827 ft. |
| Landing (ground roll) | 715 ft. |
| Take-off (MSL-over 50 ft. obstacle) | 1309 ft. |
| Take-off (ground roll) | 982 ft. |
| VNE | 162 KIAS |
| Exterior noise (take-off) | 69 db |
| Limit loads | +3.8 to -1.5g (flaps up) |
Performance data is based on International Standard Atmospheric Conditions (ISA) |
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