Do not make full or abrupt control movement above
this speed, because under certain conditions the aircraftmay be overstressed by full control movement.
| | | VO | Operating Manoeuvring Speed | | | | | | VLE | Maximum Landing Gear Extended Speed | 93 | 92 | Do not exceed this speed with the landing gear extended. | | | VLO | Maximum Landing Gear Operating Speed | 93 | 92 | Do not exceed this speed when operating the landing gear. | | | VFE | Maximum Flaps Extended Speed | FULL | 93 | 92 | Do not exceed this speed for indicated flaps setting. | | T.O. | 119 | 117 | | | | | VMC | Aircraft Minimum Controls Speed with one engine inoperative | 62 | 62 |Do not reduce speed below this value in event of one
engine inoperative condition.
| | *** ### Airspeed Indicator Markings | **MARKING** | **KIAS** | **EXPLANATION** | | ----------- | --------- | ------------------------------------------------------------------------------------------------------------------------------------------------------- | | White arc | 53 – 93 | Lower limit is VSO, upper limit is the maximum allowable speed with flaps extended in FULL position. | | Red line | 62 | Minimum aircraft control speed with one engine inoperative and flaps set to T.O. | | Green arc | 66 – 135 | Normal aircraft operating range (lower limit is VS1, stall speed in “clean” configuration, and upper limit is the maximum structural cruise speed VNO). | | Blue line | 80 | Best rate-of-climb speed with one engine inoperativeat sea level. | | Yellow arc | 135 – 167 | Speed range where manoeuvres must be conducted with caution and only in smooth air. | | Red line | 167 | Maximum speed for all operations. | *** ### Powerplant Limitations Following table reports the operating limitations for both engines installed: **Engine Manufacturer:** Bombardier Rotax GmbH. **Engine Model:** 912 S3 **Maximum Power:** | |Max Power
kW (hp)
|Max rpm.
Prop. rpm (engine)
|Time max.
(minutes)
| | -------------- | ---------------------------------------------------------------- | -------------------------------------------------------------------------- | ------------------------------------------------------------------ | | **Max. T.O.** | 73.5 (98.6) | 2388 (5800) | 5 | | **Max. Cont.** | 69 (92.5) | 2265 (5500) | - | **Temperatures:** * **Max CHT:** 135°C * **Max CT:**120°C * **Min/Max Oil:** 50°C / 130°C * **Oil normal operating range (approx.):** 90°C / 110°C **Oil Pressure (below 1400 rpm prop):** * **Minimum:** 0.8 Bar / 12 psi * Normal: 2-5 Bar / 29-73 psi * Maximum: 7 Bar / 102 psi **Fuel pressure:** * **Minimum:** 0.15 Bar / 2.2 psi * **Maximum** 0.40 Bar / 5.8 psi *** ### Maximum Operating Altitude Maximum operating altitude is 14000 ft (4260 m) MSL. *** ### Ambient Temperature Ambient temperature: from -25°C to +50°C. Flight in expected and/or known icing conditions is forbidden. *** ### Powerplant Instruments Markings | **INSTRUMENT** |RED LINE
Minimum limit
|GREEN ARC
Normal operating
|YELLOW ARC
Caution
|RED LINE
Maximum limit
| | | -------------- | ---------------------------------------------------- | -------------------------------------------------------- | ------------------------------------------------ | ---------------------------------------------------- | ---- | | Propeller | RPM | ---- | 580 - 2265 | 2265 - 2388 | 2388 | | Oil temp. | °C | 50 | 90 – 110 | 50 – 90 | 130 | | CT | °C | ---- | 50 – 120 | ---- | 120 | | CHT | °C | ---- | 50 – 135 | ---- | 135 | | Oil pressure | Bar | 0.8 | 2 – 5 | 0.8 – 2 | 7 | | Fuel press. | Psi | 2.2 | 2.2 – 5.8 | ---- | 5.8 | | Fuel Qty. | litres | 0\* | ---- | ---- | ---- | "0" Indication Shows the unusable fuel quantity (2,8 litres for each fuel tank). *** ### Other Instruments Markings | **INSTRUMENT** |RED LINE
Minimum limit
|GREEN ARC
Normal operating
|YELLOW ARC
Caution
|RED LINE
Maximum limit
| | -------------- | ---------------------------------------------------- | -------------------------------------------------------- | ------------------------------------------------ | ---------------------------------------------------- | | Voltmeter | 10,5 Volt | 12 - 14 Volt | ---- | ---- | *** ### Warnings, Cautions and Advisories Lights | **Warnings (RED)** | **Cause** | | ------------------------------------------------------------------------------------------------------------------------ | ------------------------------------------------------------------------------------------------------------------------------- | | LH OVERVOLT | LH electric system overvoltage | | RH OVERVOLT | RH electric system overvoltage | | MAIN DOOR OPEN ALERT | Main door open and/or unlocked | | REAR DOOR OPEN ALERT | Rear door open and/or unlocked | | LH LOW COOLANT | Left engine - coolant liquid low level | | RH LOW COOLANT | Right engine - coolant liquid low level | | LH ENGINE FIRE | Left engine compartment: fire detected | | RH ENGINE FIRE | Right engine compartment: fire detected | |LG TRANSITION
(warning light installed near the
landing gear control lever)
|One or more legs are in transition phase and/or
the selected retracted/extended position is not yet
reached.
| | **Cautions (Amber)** | **Cause** | | LH GENERATOR | LH generator failure | | RH GENERATOR | RH generator failure | | EXT POWER | External electrical supply connected | | PITOT HEAT | Pitot heating system failure/not activated | | GEAR PUMP ON | LG pump electrically supplied | | **Advisories (Green)** | **Indication** | | LH FUEL PUMP | Left engine - electrical fuel pump ON | | RH FUEL PUMP | Right engine - electrical fuel pump ON | | PITOT HEAT | Pitot heating system ON | |LG Down & Locked
(3 advisory lights, one for each leg, installed
near the landing gear control lever)
| Landing gear extended and locked | *** ### Weights | **Condition** | **Weight** | | | ----------------------------- | ---------- | ------- | | Maximum takeoff weight | 1180 kg | 2601 lb | | Maximum landing weight | 1180 kg | 2601 lb | | Maximum zero wing fuel weight | 1145 kg | 2524 lb | *** ### Approved Maneuvers The aircraft is certified in normal category in accordance with EASA CS-23 regulation. Non aerobatic operations include: * Any manoeuvre pertaining to “normal” flight * Stalls (except whip stalls) * Lazy eights * Turns in which the angle of bank is not more than 60° * Chandelle *** ### Maneuvers Load Factor Limits | Maneuver load factors limits are as follows: | | | ---------------------------------------------------------------- | ------------ | | **Positive** | **Negative** | | **+ 3.8 g** | - **1.78 g** | | Maneuver load factors limits with flaps extended are as follows: | | | **Positive** | **Negative** | | **+ 2 g** | **0 g** | *** ### Flight Crew * **Minimum crew:** 1 pilot * Maximum number of occupants: 4 people (including the pilot) *** ### Flight Conditions The aircraft can be equipped for following flight operations: * VFR Day and Night * IFR Day and Night including IMC Flight in expected and/or known icing conditions, in proximity of storms or severe turbulence is forbidden. *** ### Fuel * **2 Tanks:** 100 litres each one (26.42 US gallons) * **Maximum Capacity:** 200 litres (52.8 US gallons) * **Maximum Usable Fuel:** 194.4 litres (51.35 US gallons) * **Approved Fuel:** MOGAS / AVGAS --- # Agent Instructions: Querying This Documentation If you need additional information that is not directly available in this page, you can query the documentation dynamically by asking a question. Perform an HTTP GET request on the current page URL with the `ask` query parameter: ``` GET https://docs.flightsim-studio.com/tecnam-p2006t/aircraft-and-systems/section-2-limitations.md?ask=