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General Info
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| Make: | Piper | Registration Number: | N13LM |
| Model: | PA-34-200T | Serial Number: | 34-7870075 |
| Model Year: | 1978 | Engines: (200 HP – turbocharged) |
TSIO 360E LTSIO 360E |
| Location: | Trenton-Robbinsville (N87) | Gear: | Retractable |
| Props: | Constant Speed |
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Summary Info
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| Well-equipped panel: GNS 530W & 430W, HSI, EFIS, GTX 330, Strikefinder, autopilot, and more. Inexpensive path to light twins. Flies great! |
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Logbook Time
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| Total Time: (Hours since New) | 4730 | Log books |
Complete |
| Engine: (Since Overhaul) |
R: 1540 L: 1540 |
Props: (Since Major Overhaul) |
R: 1540 L: 1540 |
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Maintenance Info
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| Annual due: (Date) | Due |
| IFR Certification Due: | Due |
| AD’s complete? (Yes / No) | Yes |
| Type of Engine Overhaul: | Field |
| Damage History: | No known damage history |
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Features
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| Club seating | Inflatable door seal |
| Counter-rotating props | Auxilary audio input |
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Avionics
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| Make / Model | |
| NAV/COM #1: | Garmin GNS 530W |
| NAV/COM #2: | Garmin GNS 430W w/ 2nd Glideslope |
| HSI: | Century NSD 360 |
| EFIS: | Dynon EFIS-D60 |
| Autopilot: | Altimatic IIIC |
| Transponder: | Garmin GTX 330 |
| Audio Panel: | PS Engineering PMA6000M-C |
| Weather: | Insight Strikefinder |
| Engine Monitoring: | JPI EDM 760 w/ Fuel Flow |
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Exterior
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| Color(s): | Light Gray w/ Blue Trim |
| Paint Condition: (1 to 10, 10 being the highest) |
5 |
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Interior
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| Color(s): | Light Gray |
| Fabric: | Fabric |
| Condition: (1 to 10, 10 being the highest) |
6 |
| Glass condition: | Fair |
| Other: |
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Performance
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| Cruise Speed: (at 75% power) | 170 kts * |
| Useful Load: (remaining after full fuel) | 1171 lbs * |
| Fuel Capacity: | 93 gal |
| Fuel burn: (average) | 24 GPH total * |
| Range: | 650 nm * |
| Specific Range: ((Efficiency = Cruise Speed ÷ Lbs per hour of fuel burn) (The higher the number, the better the efficiency)) | 1.19 |
| * 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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Piper introduced the Seneca II in 1975 with upgraded control surfaces, the addition of a rudder anti-servo tab, and a stabilator bobweight to improve handling qualities. Additionally, the PA-34-200"T" was powered by turbocharged, six cylinder Continental TSIO L/TSIO-360E engines for improved performance, particularly at higher altitudes. The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca I. The Seneca II also introduced optional "club seating" whereby the two center-row seats face rearwards and the two back seats face forward allowing more legroom in the passenger cabin. This Seneca has a well-equipped panel with dual WAAS GPS’s, HSI, EFIS, audio panel, autopilot, and Strikefinder…and it’s Garmin GTX 330 provides an economical path for upgrading to ADS-B to meet the January 2020 requirements. While the engines in this Seneca are past ‘recommended’ TBO, they run well and have normal compressions and oil consumptions. All in all, this airplane is priced right and provides an economical entry into the realm of light twins. |
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Contact Us About This Aircraft
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Please call Dave Mathiesen at 609-259-2400 |
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