TECNAM P-2006T Model Guide
TECNAM P-2006T · Model Guide
Overview
The TECNAM P-2006T is a twin-engine, four-seat piston aircraft with a high cantilevered wing and tricycle retractable landing gear, built by Costruzioni Aeronautiche Tecnam in Capua, Italy. It is EASA type certificated, and its flight manual is also approved on behalf of the FAA. Registry data for the P2006T family lists up to 135 kt cruise and up to 620 nm range.
- Twin-engine, four-seat, retractable-gear piston aircraft. Registry family data lists up to 2100 kg MTOW and a 16000 ft service ceiling.
- Registry family figures: up to 135 kt cruise and up to 620 nm range. Confirm real numbers in the AFM performance section.
- Gear operating/extended speed VLO/VLE is 122 KIAS under Supplement G11. Check the placard is fitted and the supplement is in the AFM.
- Tecnam issued a service bulletin on a cracked exhaust pipe. Confirm it was done and logged.
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.
Performance
- Family max range (nm) ·
- 620
- Family max cruise speed (kt) ·
- 135
- Family max service ceiling (ft) ·
- 16,000
- South african afm max operating altitude (ft) ·
- 14,000
V-speeds
- ROTATION_SPEED_KTS ·
- 64
- MAX_FLAPS_FULL_VFE_KTS ·
- 97
- FINAL_APPROACH_SPEED_KTS ·
- 75
- MAX_FLAPS_TAKEOFF_VFE_KTS ·
- 124
- MAX_GEAR_OPERATING_VLO_VLE_KTS ·
- 122
What kind of aircraft is the TECNAM P-2006T?
The TECNAM P-2006T is a twin-engine, four-seat aircraft with a high cantilevered wing and tricycle retractable landing gear, per the Aircraft Flight Manual foreword.
What is the gear speed limit?
For the TECNAM P-2006T, Supplement G11 shows a placard of maximum landing gear operating speed VLO/VLE = 122 KIAS. An operator checklist also lists gear down below VLO 122 KIAS.
Is there a known exhaust issue?
Tecnam service bulletin SB 170 applies to all P2006T aircraft after a cracked exhaust pipe was found. It calls for inspecting the exhaust pipes and contacting Tecnam if cracks or deformation are found. Ask for proof it was done.
What is the TECNAM P-2006T Model Guide?
The TECNAM P-2006T Model Guide is a model guide for the TECNAM P-2006T, dated 2026.
What year was the TECNAM P-2006T Model Guide published?
The TECNAM P-2006T Model Guide — the TECNAM P-2006T 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 P-2006T.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
TECNAM P-2006T for sale now
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More TECNAM P-2006Tmanuals & documents
- SPECTRUM AIRWAYS TECNAM P2006T NORMAL PROCEDURESChecklist
- CHECK LISTChecklist
- TECNAM P2006T CHECK LISTChecklist
- Normal Check List P2006TChecklist
- Aircraft Flight ManualPilot's Operating Handbook
- Aircraft Flight ManualPilot's Operating Handbook
- SERVICE BULLETIN N° SB 170 – CS – Ed 1 Rev 1Service Bulletins
- Section 9 - Supplements - Delta AviationFlight Manual Supplement
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In this document
Pre-buy inspection points
Use the manufacturer walk-around. Check coolant level in the expansion tank (at least 2/3) and overflow bottle, and turn the propeller by hand for 15° or 30° of free play. Check oil level, drain the gascolator and sumps, and look for hydraulic leaks at the gear. Check emergency gear extension pressure (low limit 20 bar).
Engine figures from an operator checklist
One operator's normal-procedures checklist (not a substitute for the AFM) lists run-up at 1650 RPM with a magneto drop of 130 max and 50 difference. Oil temperature is 90° to 100°C, CHT is 50° to 135°C, and cruise propeller setting is 1900 to 2250 RPM. Climb propeller setting is 2250 RPM.
Documents and configuration
The current AFM seen here is 4th Edition, Rev. 14 (March 03, 2020). Supplement G13 covers 70A alternators replacing the standard 40A ones (MOD 2006/202). A South African AFM supplement limits operating altitude to 14000 ft. Check that the aircraft's installed modifications match its AFM supplements.
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
- Service bulletin SB 170: inspect all exhaust pipes on both engines for cracks or deformation within 25 flight hours or 30 days of issue. A cracked pipe was found in a pre-flight inspection.
- The AFM must be carried in the airplane at all times, and the airplane must be operated within its procedures and limitations.
- South African AFM supplement: above 12 000 feet, supplemental oxygen is required for the aircrew.
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 P-2006T Model Guide The TECNAM P-2006T is a twin-engine, four-seat piston aircraft with a high cantilevered wing and tricycle retractable landing gear, built by Costruzioni Aeronautiche Tecnam in Capua, Italy. It is EASA type certificated, and its flight manual is also approved on behalf of the FAA. Registry data for the P2006T family lists up to 135 kt cruise and up to 620 nm range. • Twin-engine, four-seat, retractable-gear piston aircraft. Registry family data lists up to 2100 kg MTOW and a 16000 ft service ceiling. • Registry family figures: up to 135 kt cruise and up to 620 nm range. Confirm real numbers in the AFM performance section. • Gear operating/extended speed VLO/VLE is 122 KIAS under Supplement G11. Check the placard is fitted and the supplement is in the AFM. • Tecnam issued a service bulletin on a cracked exhaust pipe. Confirm it was done and logged. Pre-buy inspection points Use the manufacturer walk-around. Check coolant level in the expansion tank (at least 2/3) and overflow bottle, and turn the propeller by hand for 15° or 30° of free play. Check oil level, drain the gascolator and sumps, and look for hydraulic leaks at the gear. Check emergency gear extension pressure (low limit 20 bar). Engine figures from an operator checklist One operator's normal-procedures checklist (not a substitute for the AFM) lists run-up at 1650 RPM with a magneto drop of 130 max and 50 difference. Oil temperature is 90° to 100°C, CHT is 50° to 135°C, and cruise propeller setting is 1900 to 2250 RPM. Climb propeller setting is 2250 RPM. Documents and configuration The current AFM seen here is 4th Edition, Rev. 14 (March 03, 2020). Supplement G13 covers 70A alternators replacing the standard 40A ones (MOD 2006/202). A South African AFM supplement limits operating altitude to 14000 ft. Check that the aircraft's installed modifications match its AFM supplements. Safety notes: • Service bulletin SB 170: inspect all exhaust pipes on both engines for cracks or deformation within 25 flight hours or 30 days of issue. A cracked pipe was found in a pre-flight inspection. • The AFM must be carried in the airplane at all times, and the airplane must be operated within its procedures and limitations. • South African AFM supplement: above 12 000 feet, supplemental oxygen is required for the aircrew.