TECNAM P2010 MKII Model Guide
TECNAM P2010 MKII · Model Guide
Overview
TECNAM P2010 MKII is a single-engine piston aeroplane. The supplied documents cover the P2010 and do not name the MKII separately, so confirm your aircraft's exact configuration. The Aircraft Flight Manual (AFM) lists a 180 hp Lycoming IO-360-M1A, normal category, with a maximum takeoff weight of 2557 lb. Registry data for the family shows up to 4 passengers.
- AFM powerplant: Lycoming IO-360-M1A, fuel injected, 180 hp at 2700 rpm. Maximum takeoff weight is 2557 lb.
- Standard prop is fixed pitch (74 in). A variable-pitch MT propeller (76 in) is covered by supplement D07.
- The GFC 700 autopilot is optional. It is 2-axis (roll and pitch) with pitch trim, and has no yaw or rudder trim control.
- Some P2010s have a Lycoming IO-390. A mandatory exhaust flame tube inspection (SB 937, AD 2026-0023) applies up to S/N 335.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 49 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Wing span (ft) ·
- 33.79
- Cabin width (ft) ·
- 3.74
- Engine power (hp) ·
- 180
- Overall height (ft) ·
- 8.66
- Overall length (ft) ·
- 26.15
- Propeller diameter (in) ·
- 74
- Max takeoff weight (lb) ·
- 2,557
Performance
- Family max range (nm) ·
- 715
- Family max cruise speed (kt) ·
- 133
- Family max service ceiling (ft) ·
- 13,000
Weight & balance
- Max takeoff weight (lb) ·
- 2,557
What engine does the TECNAM P2010 MKII use?
For the TECNAM P2010 MKII, the P2010 AFM lists a Lycoming IO-360-M1A producing 180 hp at 2700 rpm. Service bulletin SB 937 also refers to P2010 aircraft with a Lycoming IO-390, so confirm which engine is fitted.
Are the performance figures exact for this variant?
No. For the TECNAM P2010 MKII, the registry figures are family maxima: up to 715 nm range, 133 kt cruise and 13000 ft ceiling. Use the AFM performance section for your aircraft.
Does it come with an autopilot?
The TECNAM P2010 MKII documents describe the Garmin GFC 700 as optional equipment. It is a 2-axis autopilot (roll and pitch) with pitch trim, and has no yaw axis control.
What is the TECNAM P2010 MKII Model Guide?
The TECNAM P2010 MKII Model Guide is a model guide for the TECNAM P2010 MKII, dated 2026.
What year was the TECNAM P2010 MKII Model Guide published?
The TECNAM P2010 MKII Model Guide — the TECNAM P2010 MKII model guide on file — is dated 2026.
Common. More common than 89% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the TECNAM P2010 MKII.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Engine and propeller
The AFM lists a Lycoming IO-360-M1A: fuel injected, direct drive, four-cylinder, air cooled, 180 hp at 2700 rpm. The standard propeller is a fixed-pitch MT 188 R 145-4G, 74 in diameter. Supplement D07 lists a hydraulic-governed variable-pitch MTV-15-B/193-52, 76 in, with maximum continuous power of 173.3 hp at 2600 rpm. Check which propeller is fitted.
Size and certification
Wing span is 33.79 ft, length 26.15 ft and height 8.66 ft. The cabin is 3.74 ft wide and 7.54 ft long. The type is certified in the normal category under EASA CS-23, and also validated under 14 CFR part 23. The AFM must be carried in the airplane at all times, and the owner is responsible for keeping it current.
Autopilot and avionics option
The optional Garmin GFC 700 autopilot works with the G1000 and uses a GDU 1044 MFD. It has roll, pitch and pitch-trim servos. ESP (Electronic Stability and Protection) runs when hand-flying with GPS available and above 200 ft AGL, and the pilot can disable it. Check whether the aircraft has this option.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- SB 937 (mandatory by AD 2026-0023) covers IO-390 aircraft up to S/N 335. Initial and repeat inspections of the exhaust muffler flame tube are required.
- A blocked exhaust from a flame tube defect could cause engine malfunction or stoppage. Check the maintenance log for SB 937 compliance.
- The autopilot has no yaw axis control. ESP cannot work without GPS and is off when the A/P master switch is off.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
TECNAM P2010 MKII Model Guide TECNAM P2010 MKII is a single-engine piston aeroplane. The supplied documents cover the P2010 and do not name the MKII separately, so confirm your aircraft's exact configuration. The Aircraft Flight Manual (AFM) lists a 180 hp Lycoming IO-360-M1A, normal category, with a maximum takeoff weight of 2557 lb. Registry data for the family shows up to 4 passengers. • AFM powerplant: Lycoming IO-360-M1A, fuel injected, 180 hp at 2700 rpm. Maximum takeoff weight is 2557 lb. • Standard prop is fixed pitch (74 in). A variable-pitch MT propeller (76 in) is covered by supplement D07. • The GFC 700 autopilot is optional. It is 2-axis (roll and pitch) with pitch trim, and has no yaw or rudder trim control. • Some P2010s have a Lycoming IO-390. A mandatory exhaust flame tube inspection (SB 937, AD 2026-0023) applies up to S/N 335. Engine and propeller The AFM lists a Lycoming IO-360-M1A: fuel injected, direct drive, four-cylinder, air cooled, 180 hp at 2700 rpm. The standard propeller is a fixed-pitch MT 188 R 145-4G, 74 in diameter. Supplement D07 lists a hydraulic-governed variable-pitch MTV-15-B/193-52, 76 in, with maximum continuous power of 173.3 hp at 2600 rpm. Check which propeller is fitted. Size and certification Wing span is 33.79 ft, length 26.15 ft and height 8.66 ft. The cabin is 3.74 ft wide and 7.54 ft long. The type is certified in the normal category under EASA CS-23, and also validated under 14 CFR part 23. The AFM must be carried in the airplane at all times, and the owner is responsible for keeping it current. Autopilot and avionics option The optional Garmin GFC 700 autopilot works with the G1000 and uses a GDU 1044 MFD. It has roll, pitch and pitch-trim servos. ESP (Electronic Stability and Protection) runs when hand-flying with GPS available and above 200 ft AGL, and the pilot can disable it. Check whether the aircraft has this option. Safety notes: • SB 937 (mandatory by AD 2026-0023) covers IO-390 aircraft up to S/N 335. Initial and repeat inspections of the exhaust muffler flame tube are required. • A blocked exhaust from a flame tube defect could cause engine malfunction or stoppage. Check the maintenance log for SB 937 compliance. • The autopilot has no yaw axis control. ESP cannot work without GPS and is off when the A/P master switch is off.