TWIN PISTON
Tecnam P2006T
One model from FAA type certificate data sheet A62CE. Every figure below is quoted from the sheet. Open any “Source” to see the words it comes from.
THE DATA SHEET
- Authority
- Federal Aviation Administration (United States)
- Sheet
- Type Certificate Data Sheet A62CE
- Revision
- 10
- Date
- November 30, 2022
- Holder
- Costruzioni Aeronautiche Tecnam S.P.A.
- Licence
- US Government work, public domain (17 U.S.C. 105)
Open the sheet on the FAA Dynamic Regulatory System (opens in a new tab)
Earlier revision. This is revision 10 of the data sheet. A later revision exists that we have not checked yet.
Performance figures (stall speeds, take-off and landing distances, climb, cruise and fuel burn) are in the aircraft's flight manual (POH/AFM), which we cannot reproduce. Always use the flight manual for the aircraft you fly.
This is a United States Federal Aviation Administration sheet. We show it as a US certification document, not as an Australian or New Zealand rule. Units are the sheet's own: pounds, US gallons and quarts, and knots or mph as stated.
How we copied the sheet. Quotes are from our stored text copy of the sheet, taken from the text layer of the FAA's online viewer. We rebuilt lines from the text positions, joined wrapped lines, marked wide gaps between table cells with |, removed page headers and footers, and replaced symbol-font characters with the symbols they print as. Check the original sheet before relying on any figure.
Models not shown. The sheet covers one model, and it is included.
SPEC SHEET
Tecnam P2006T: P2006T
The sheet's heading for this modelModel P2006T (Normal Category)
Source for the model heading
I - Model P2006T (Normal Category), Approved November 10, 2010
Engine
- Engine
- Bombardier-Rotax 912 S3two of this engine
Source for Engine
Engines | Two Bombardier-Rotax 912 S3 (TC E00051EN)
- Rated power
- 98.6 hpeach engine, 5 min limit
Source for Rated power
Engine Limits | Max rotational speed (5 min) 5800 r.p.m. (98.6 hp)
- Engine speed limit
- 5,800 rpm5 min limit, engine shaft
Source for Engine speed limit
Engine Limits | Max rotational speed (5 min) 5800 r.p.m. (98.6 hp)
- Propeller
- MT Propeller MTV-21-A-C-F/CF178-05
Source for Propeller
Propeller and | Two MT Propeller MTV-21-A-C-F/CF178-05 (TC P16BO)
Fuel and oil
- Fuel capacity
- 52.8 US gal≈ 200 L (converted)
Source for Fuel capacity
Fuel Capacity | 52.8 US Gal (+ 29.7 in) Usable 51.35 US Gal
- Usable fuel
- 51.35 US gal≈ 194 L (converted)
Source for Usable fuel
Fuel Capacity | 52.8 US Gal (+ 29.7 in) Usable 51.35 US Gal
- Oil capacity
- 0.79 US galeach engine, maximum≈ 3 L (converted)
Source for Oil capacity
Oil Capacity (each engine) | Maximum: | 0.79 US Gal
Weights and loading
- Maximum weight
- Normal category2,600 lb≈ 1,179 kg (converted)
Source for Maximum weight, Normal category
Maximum Weight | Take-off | 2600 lbs
- Seats
- 4
Source for Seats
Number of Seats | 4
- Baggage limit
Left out. The sheet gives a "Maximum Compartments Weights" figure and does not call it a baggage limit.
- C.G. range
- 8.7 in (16.5 % MAC) to 16.34 in (31.0 % MAC)
Source for C.G. range
Center of Gravity (C.G.) Range | 8.7 in (16.5 % MAC) to 16.34 in (31.0 % MAC)
Airspeed limits
- Never exceed speed (Vne)
- 167 kt IASThe table's first column is KIAS, the second KCAS. We show KIAS.
Source for Never exceed speed (Vne)
V NE (Never Exceed Speed) | 167 | 168
- Maximum structural cruising speed (Vno)
- 135 kt IASThe table's first column is KIAS, the second KCAS. We show KIAS.
Source for Maximum structural cruising speed (Vno)
V NO (Maximum Structural Cruising Speed) | 135 | 134
- Manoeuvring speed (Va)
- 119 kt IASThe table's first column is KIAS, the second KCAS. We show KIAS.
Source for Manoeuvring speed (Va)
V A (Design Manoeuvring Speed) | 119 | 117
- Maximum flap extended speed (Vfe)
- take-off flap119 kt IASThe table's first column is KIAS, the second KCAS. We show KIAS.
Source for Maximum flap extended speed (Vfe), take-off flap
119 | 117 Take Off
landing flap93 kt IASThe table's first column is KIAS, the second KCAS. We show KIAS.Source for Maximum flap extended speed (Vfe), landing flap
V FE (Flap Extended Speed) | 93 | 92 Landing
Reference
- Datum
- Wing leading edge
Source for Datum
Datum | Wing leading edge (MAC = 52.72 in)
- Certification basis
- 14 CFR Part 23 effective February 1, 1965, including amendments 23-1 through 23-57
Source for Certification basis
14 CFR Part 23 effective February 1, 1965 including amdt 23-1 through 23-57
COCKPIT
The P2006T limits on an airspeed indicator
Where the sheet gives them in knots, the dial shows Vne as a red line, the caution range from Vno to Vne as a yellow arc, a green tick at Vno and white ticks at the flap limit speeds (Vfe). The sheet gives flap limits, not instrument markings, and the stall speeds where the green and white arcs start are not in it.
- Airspeed indicator
- Attitude indicator
- Altimeter
- Turn coordinator
- Heading indicator
- Vertical speed indicator
- Tachometer
- Oil temperature
- Oil pressure
- Fuel quantity
- Suction gauge
What the dial shows
- Red line: never exceed speed (Vne)167 kt IAS
Source for the red line
V NE (Never Exceed Speed) | 167 | 168
- Yellow arc: caution rangeFrom Vno to Vne, 135 kt IAS to 167 kt IAS
- Green tick: Vno, top of the green arc135 kt IAS
Source for the green tick
V NO (Maximum Structural Cruising Speed) | 135 | 134
- White tick: Vfe, take-off flap, a flap limit speed119 kt IAS
Source for the white tick, take-off flap
119 | 117 Take Off
- White tick: Vfe, landing flap, a flap limit speed93 kt IAS
Source for the white tick, landing flap
V FE (Flap Extended Speed) | 93 | 92 Landing
- Marks are drawn at the sheet's speeds in knots IAS.
- White ticks mark the flap limit speeds (Vfe) the sheet gives. The sheet gives flap limits, not instrument markings, so the flight manual says where this aircraft's white arc ends.
- The low ends of the white and green arcs are stall speeds. They come from the flight manual, so we have left them unmarked.
The other instruments are drawn at rest and are not linked to this aircraft. Learn what each instrument shows in the cockpit explorer.
For learning only. Not for flight planning or use in flight. Figures are certification limits from Federal Aviation Administration, Type Certificate Data Sheet A62CE, Revision 10, retrieved 31 October 2026. Conversions marked “converted” are our own arithmetic. No manufacturer images are used. The instruments are drawn by us. Back to all aircraft.