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General Info
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| Make: | Mooney | Registration Number: | N3479X |
| Model: | M20E | Serial Number: | 1153 |
| Model Year: | 1966 | Engine: | I0-360-A1A (200 HP) |
| Location: | Robbinsville, NJ (N87) | Gear: | Retractable (manual) |
| Prop: | Constant Speed | ||
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Summary Info
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| Beautiful and fast M20E with 201 cowl, 201 windshield, gap seals, fairings, etc. (aka short-body 201); Garmin GNS 430W coupled to S-TEC 30 autopilot with altitude hold and GPSS (roll steering). |
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Logbook Time
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| Total Time: (Hours since New) | 3386 | Log books |
Complete |
| Engine: (Hrs SMOH) |
1356 | Prop: (Since Overhaul ) | 416 |
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Maintenance Info
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| Annual Due: (Date) | Nov 2019 | ||
| IFR Certification Due: | Oct 2019 | ||
| AD’s complete: |
Yes | ||
| Recent Maintenance Items: | Recently overhauled fuel servo and fuel divider (Feb 2019) | ||
| Other: | New main gear tires and new Powerflow Exhaust (Nov 2018), new Vertical Compass Card (Aug 2018)) | ||
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Features
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| 201 SWTA cowl | Wing root, horizontal, dorsal fin, flap, rudder, & elevator hinge fairings; flap & aileron gap seals; brake cylinder rotation | ||
| 201 windshield | Hartzell Top Prop conversion | ||
| 201 Yokes | Dual USB jacks | ||
| Polished spinner | Electric flaps | ||
| Retractable step | Factory Oxygen Option (needs bottle and clamps) | ||
| Pilot seat armrest mod | LED landing light | ||
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Avionics
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| Make / Model | |
| Nav/Com/GPS 1: | Garmin GNS 430W |
| Nav/Com 2: | King KX 155 |
| Autopilot: | S-TEC 30 with altitude hold and GPSS (roll steering) |
| Transponder: | King KT 76A |
| Audio Panel: | King KMA 24 |
| Intercom: | Precision Engineering PM 1000II |
| Engine Monitor: | JPI EDM 700 with fuel flow |
| Other: | Davtron M303 Digital OAT and voltmeter, avionics master switch |
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Exterior
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| Color(s): | White w/ Teal Green & Black trim |
| Paint Condition: (1 to 10, 10 being the highest) |
8 |
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Interior
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| Color(s): | Green |
| Fabric: | Leather |
| Condition: (1 to 10, 10 being the highest) |
8 |
| Glass: | Good |
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Performance
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| Cruise Speed: (at 75% power) | 150 kts * | ||
| Useful Load: (remaining after full fuel) | 970 lbs * | ||
| Fuel Capacity: | 52 gal | ||
| Fuel burn: (average) | 10.5 GPH * | ||
| Range: | 650 nm * | ||
| Specific Range: ((Efficiency = Cruise Speed ÷ Lbs per hour of fuel burn) (The higher the number, the better the efficiency)) | 2.41 | ||
| *Note: Performance figures are estimates based on best available information (from POH, Vref, etc.) and may not be exact for this particular aircraft. | |||
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Comments
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