Tecnam P92 Echo MK2 Technical specifications

P92 LSA
Flight Manual
1
FLIGHT MANUAL
US-LSA
P92 Echo MK2
Manufacturer
COSTRUZIONI AERONAUTICHE TECNAM S.p.A.
Serial number: ________________
Build year: ___________________
Registration: __________________
Introduction
This manual contains information to be furnished to the pilot as required by the FAA in addition to further information
supplied by the manufacturer.
This manual must always be present on board the aircraft.
The aircraft is to be operated in compliance with information and limitations contained herein. All sections follow the
ASTM guidelines.
Doc. No. 92/269
Ed. 1 Rev. 4- 18/06/2021

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Flight Manual
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Record of Revisions
Any revisions to the present Manual, except actual weighing data, must be recorded in the following table.
New or amended text in the revised pages will be indicated by a black vertical line in the left-hand margin;
Log of Revisions
Revision No.
Date released
Chapters
Approved By
00
30/07/2020
All
TECNAM
01
09/11/2020
1
TECNAM
02
03/05/2021
2, 4
TECNAM
03
07/06/2021
1
TECNAM
04
18/06/2021
1, 2, 6, 8, 9
TECNAM

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List of Effective Pages
Page
Rev.
9 thru 22
25, 27 thru 39, 41 thru
71
S01-1 thru 3
0
23, 24
1
1 thru 8, 26, 40
2
1 thru 3, 23
3
1 thru 3, 30, 58, 59, 65
thru 72
4

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Table of Contents
P92 Echo MK2 .................................................................................................................................................................. 1
Unit Conversion Chart .................................................................................................................................................... 12
SECTION 1 GENERAL........................................................................................................................................................13
1.1 Introduction ............................................................................................................................................................ 13
1.2 Certification Basis ................................................................................................................................................... 13
1.3 Descriptive Data ..................................................................................................................................................... 15
1.3.1 Airframe.......................................................................................................................................................... 15
1.4 Powerplant ............................................................................................................................................................. 16
1.4.1 Engine............................................................................................................................................................. 16
1.4.2 Propeller ......................................................................................................................................................... 16
1.4.3 Oil System....................................................................................................................................................... 16
1.4.4 Cooling............................................................................................................................................................ 16
1.4.5 Fuel................................................................................................................................................................. 16
1.5 Weights................................................................................................................................................................... 17
1.5.1 Maximum Weights ......................................................................................................................................... 17
1.5.2 Standard Weights ........................................................................................................................................... 17
1.5.3 Specific Loadings............................................................................................................................................. 17
1.6 Standard Equipment............................................................................................................................................... 17
1.6.1 Flight Instruments .......................................................................................................................................... 17
1.6.2 Engine instruments......................................................................................................................................... 17
1.6.3 Warning Lights and Indicators........................................................................................................................ 17
1.6.4 Controls .......................................................................................................................................................... 17
1.6.5 Interior............................................................................................................................................................ 17
1.6.6 Exterior ........................................................................................................................................................... 17
1.6.7 Powerplant and Accessories........................................................................................................................... 18
1.7 Airframe.................................................................................................................................................................. 19
1.7.1 Wing ............................................................................................................................................................... 19
1.7.2 Fuselage.......................................................................................................................................................... 19
1.7.3 Empennage..................................................................................................................................................... 19
1.7.4 Flight controls................................................................................................................................................. 19
1.7.5 Instrument Panel ............................................................................................................................................ 20
1.7.6 Seats ............................................................................................................................................................... 20
1.7.7 Doors .............................................................................................................................................................. 20
1.7.8 Baggage compartment ................................................................................................................................... 20
1.8 Powerplant ............................................................................................................................................................. 21
1.8.1 Engine............................................................................................................................................................. 21
1.8.2 Propeller ......................................................................................................................................................... 21
1.8.3 Fuel system..................................................................................................................................................... 21
1.9 Electrical System..................................................................................................................................................... 23
1.10 Landing Gear .......................................................................................................................................................... 24
1.10.1 Brake System .................................................................................................................................................. 25

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SECTION 2 OPERATING LIMITATIONS ..............................................................................................................................26
2Introduction ............................................................................................................................................................26
2.1.1 Airspeed Limitations....................................................................................................................................... 26
2.1.2 Airspeed Indicator Markings .......................................................................................................................... 26
2.1.3 Powerplant Limitations .................................................................................................................................. 27
2.1.4 Temperatures ................................................................................................................................................. 27
2.1.5 Oil Pressure..................................................................................................................................................... 27
2.1.6 Operating & starting temperature range ....................................................................................................... 27
2.1.7 Fuel Pressure .................................................................................................................................................. 27
2.1.8 Lubricant......................................................................................................................................................... 28
2.1.9 Coolant ........................................................................................................................................................... 28
2.1.10 Propellers........................................................................................................................................................ 28
2.1.11 Fuel................................................................................................................................................................. 28
2.1.12 Approved Fuel ................................................................................................................................................ 28
2.1.13 Powerplant Instrument Markings................................................................................................................... 29
2.1.14 Other Instrument Markings............................................................................................................................ 29
2.1.15 Weights........................................................................................................................................................... 29
2.1.16 Center of Gravity Limits.................................................................................................................................. 29
2.1.17 Approved Maneuvers ..................................................................................................................................... 29
2.1.18 Maneuvering Load Factor Limits .................................................................................................................... 30
2.1.19 Flight Crew...................................................................................................................................................... 30
2.1.20 Kinds of Operations ........................................................................................................................................ 30
2.1.21 VFR Day........................................................................................................................................................... 30
2.1.22 VFR Night........................................................................................................................................................ 30
2.1.23 IFR................................................................................................................................................................... 30
2.1.24 Demonstrated Crosswind Safe Operations .................................................................................................... 31
2.1.25 Maximum operating altitude.......................................................................................................................... 31
2.1.26 Limitation Placards ......................................................................................................................................... 31
SECTION 3 WEIGHT & BALANCE ......................................................................................................................................32
3Introduction ............................................................................................................................................................32
3.1 Aircraft weighing procedures ................................................................................................................................. 32
3.1.1 Preparation..................................................................................................................................................... 32
3.1.2 Calculate empty weight Weighing.................................................................................................................. 32
3.1.3 Determination of C.G. location....................................................................................................................... 32
3.2 Weighing report ..................................................................................................................................................... 33
3.2.1 Center of Gravity Limits.................................................................................................................................. 34
3.2.2 Distances from the datum.............................................................................................................................. 34
3.3 Weight and Balance ............................................................................................................................................... 35
3.3.1 Loading ........................................................................................................................................................... 37
SECTION 4 PERFORMANCE ..............................................................................................................................................38
4Introduction ............................................................................................................................................................38
4.1 Use of Performance Charts..................................................................................................................................... 38
4.2 Airspeed Indicator System Calibration.................................................................................................................... 38

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4.3 ICAO Chart .............................................................................................................................................................. 39
4.4 Stall Speeds............................................................................................................................................................. 40
4.5 Crosswind ............................................................................................................................................................... 41
4.6 Takeoff Performance .............................................................................................................................................. 42
4.7 Landing Distance .................................................................................................................................................... 45
4.8 Climb Performance ................................................................................................................................................. 48
4.9 Cruise ...................................................................................................................................................................... 49
SECTION 5 EMERGENCY PROCEDURES.............................................................................................................................50
Introduction....................................................................................................................................................................50
5.1 Engine Failures........................................................................................................................................................ 51
5.1.1 Engine Failures on Ground ............................................................................................................................. 51
5.1.2 Engine Failure during Flight ............................................................................................................................ 51
5.2 Engine Securing ...................................................................................................................................................... 52
5.3 In flight engine restart ............................................................................................................................................ 52
5.4 Smoke and Fire ....................................................................................................................................................... 53
5.4.1 Engine Fire while parked ................................................................................................................................ 53
5.4.2 Engine Fire during Takeoff.............................................................................................................................. 53
5.4.3 Engine Fire in-flight......................................................................................................................................... 53
5.4.4 Cabin Fire / Electrical smoke in cabin during Flight........................................................................................ 53
5.4.5 Electrical smoke/fire in cabin on the ground ................................................................................................. 54
5.5 Landing Emergency ................................................................................................................................................ 54
5.6 Stall Recovery ......................................................................................................................................................... 54
5.7 Recovery from Unintentional Spin .......................................................................................................................... 55
5.8 Airplane Alerts ........................................................................................................................................................ 55
5.8.1 Alternator failure............................................................................................................................................ 55
5.8.2 Electrical fuel pump failure............................................................................................................................. 55
5.9 Trim System Failure ................................................................................................................................................ 56
5.9.1 LOCKED CONTROL .......................................................................................................................................... 56
5.9.2 RUNAWAY....................................................................................................................................................... 56
5.10 Airplane Evacuation................................................................................................................................................ 56
5.11 Other Emergencies ................................................................................................................................................. 56
5.11.1 UNINTENTIONAL FLIGHT INTO ICING CONDITIONS........................................................................................ 56
SECTION 6 NORMAL PROCEDURES ..................................................................................................................................57
6Introduction ............................................................................................................................................................57
6.1 Checklist Procedures............................................................................................................................................... 57
6.1.1 Pre-Flight Inspection....................................................................................................................................... 57
SECTION 7 GROUND HANDLING & SERVICE.....................................................................................................................63

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7Introduction ............................................................................................................................................................63
7.1 Aircraft Inspection Periods...................................................................................................................................... 63
7.2 Aircraft Alterations or Repairs ................................................................................................................................ 63
7.3 Ground Handling .................................................................................................................................................... 63
7.3.1 Towing ............................................................................................................................................................ 63
7.3.2 Parking and Tiedown ...................................................................................................................................... 63
7.3.3 Jacking ............................................................................................................................................................ 63
7.3.4 Leveling........................................................................................................................................................... 63
7.3.5 Road Transport............................................................................................................................................... 63
7.3.6 Cleaning and Care........................................................................................................................................... 64
8PLACARDS & MARKINGS..........................................................................................................................................65
8.1.1 Magnetic compass compensation table......................................................................................................... 65
8.1.2 Engine throttle friction ................................................................................................................................... 65
8.1.3 Cabin heat....................................................................................................................................................... 65
8.1.4 Trim switch ..................................................................................................................................................... 66
8.1.5 Breakers.......................................................................................................................................................... 66
8.1.6 Flaps................................................................................................................................................................ 67
8.1.7 Generator, Master, Starter............................................................................................................................. 67
8.1.8 Choke.............................................................................................................................................................. 67
8.1.9 Generator light ............................................................................................................................................... 67
8.1.10 Fuel selector valve.......................................................................................................................................... 68
8.1.11 Baggage compartment ................................................................................................................................... 68
8.1.12 Oil tank reservoir ............................................................................................................................................ 68
8.1.13 Identification plate ......................................................................................................................................... 69
8.1.14 Fuel Tank ........................................................................................................................................................ 69
8.1.15 Limitation Placards ......................................................................................................................................... 69
9SUPPLEMENT LIST....................................................................................................................................................71
9.1 Introduction ............................................................................................................................................................ 71
9.2 Supplements list...................................................................................................................................................... 71

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INTENTIONALLY LEFT BLANK

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WARNINGS - CAUTIONS - NOTES
The following definitions apply to warnings, cautions and notes used in the Flight Manual.
WARNING
Means that the non-observation of the corresponding procedure leads to an immediate or important degradation of the flight
safety
CAUTION
Means that the non-observation of the corresponding procedure leads to a minor or to a more or less long-term degradation
of the flight safety
NOTE
Draws the attention to any special item not directly related to safety but which is important or unusual.

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Abbreviations & Terminology
Airspeed Terminology
KCAS
Calibrated Airspeed is the indicated airspeed corrected for position and
instrument error and expressed in knots.
KIAS
Indicated Airspeed is the speed shown on the airspeed indicator and
expressed in knots.
KTAS
True Airspeed is the airspeed expressed in knots relative to undisturbed
air, which is KCAS, corrected for altitude and temperature.
VA
Design maneuvering speed
VC
Design cruising speed is the speed above the which it is not allowed to
make full or abrupt control movement
VFE
Maximum Flap Extended Speed is the highest speed permissible with
wing flaps in a prescribed extended position.
VH
Max Speed in level flight with Max continuous power
VLO
Lift off speed: is the speed at which the aircraft generally lifts off from the
ground.
VNE
Never Exceed Speed is the speed limit that may not be exceeded at any
time.
VNO
Maximum Structural Cruising Speed is the speed that should not be
exceeded except in smooth air, then only with caution.
VS
Stalling Speed or minimum steady flight speed flaps retracted
VS0
Stalling speed or minimum steady flight speed in landing configuration
VS1
Stalling speed in clean configuration (flap 0°)
VX
Best Angle-of-Climb Speed is the speed, which results in the greatest gain
of altitude in a given horizontal distance.
VY
Best Rate-of-Climb Speed is the speed, which results in the greatest gain
in altitude in a given time.
VR
Rotation speed: is the speed at which the aircraft rotates about the pitch
axis during takeoff.
Meteorology Terminology
OAT
Outside Air Temperature is the free air static temperature expressed in
degrees Celsius (°C).
TS
Standard Temperature is 15°C (59F) at sea level pressure altitude and
decreased by 2°C for each 1000 ft of altitude.
HP
Pressure Altitude is the altitude read from an altimeter when the
barometric subscale has been set to 29.92”
Engine Power Terminology
RPM
Revolutions Per Minute: is the number of revolutions per minute of the
engine.

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Airplane Performance and Flight Planning Terminology
Crosswind
Velocity
is the velocity of the crosswind component for which adequate control of the airplane
during takeoff and landing is guaranteed
Usable fuel
is the fuel available for flight planning
Unusable fuel
is the quantity of fuel that cannot be safely used in flight
g
is the acceleration of gravity
Weight and Balance Terminology
Datum
“Reference datum” is an imaginary vertical plane from which all horizontal
distances are measured for balance purposes
Arm
is the horizontal distance from the reference datum to the center of gravity
(C.G.) of an item
Moment
is the product of the weight of an item multiplied by its arm
C.G.
Center of Gravity is the point at which the airplane, or equipment, would
balance if suspended. Its distance from the reference datum is found by
dividing the total moment by the total weight of the airplane
Empty Weight
Empty Weight is the weight of the airplane with engine fluids and oil at
operating levels
Useful Load
is the difference between takeoff weight and the empty weight
Maximum Takeoff Weight
is the maximum weight approved for the start of the takeoff run
Maximum Landing Weight
is the maximum weight approved for the landing touch down
Tare
is the weight of chocks, blocks, stands, etc. used when weighing an airplane,
and is included in the scale readings; tare is then deducted from the scale
reading to obtain the actual (net) airplane weight

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Unit Conversion Chart
Multiplying
by 
Yields
Temperature
Fahrenheit
[°F]
 
5
932 F
Celsius
[°C]
Celsius
[°C]
9
532




C
Fahrenheit
[°F]
Forces
Kilograms
[kg]
2.205
Pounds
[lbs]
Pounds
[lbs]
0.4536
Kilograms
[kg]
Speed
Meters per second
[m/s]
196.86
Feet per minute
[ft/min]
Feet per minute
[ft/min]
0.00508
Meters per second.
[m/s]
Knots
[kts]
1.852
Kilometers / hour
[km/h]
Kilometers / hour
[km/h]
0.5396
Knots
[kts]
Pressure
Atmosphere
[atm]
14.7
Pounds / sq. in
[psi]
Pounds / sq. in
[psi]
0.068
Atmosphere
[atm]
Length
Kilometers
[km]
0.5396
Nautical miles
[nm]
Nautical miles
[nm]
1.852
Kilometers
[km]
Meters
[m]
3.281
Feet
[ft]
Feet
[ft]
0.3048
Meters
[m]
Centimeters
[cm]
0.3937
Inches
[in]
Inches
[in]
2.540
Centimeters
[cm]
Volume
Liters
[l]
0.2642
U.S. Gallons
[US Gal]
U.S. Gallons
[US Gal]
3.785
Liters
[l]
Area
Square meters
[m2]
10.76
Square feet
[sq ft]
Square feet
[sq ft]
0.0929
Square meters
[m2]
Torque
foot-pounds
1.3558
Newton-meters
foot-pounds
0.1383
kilogram-meters
foot-pounds
12.0
inch-pounds
inch-pounds
0.0115
kilogram-meters
inch-pounds
0.1130
Newton-meters
inch-pounds
0.0833
foot-pounds
kilogram-meters
7.233
foot-pounds
kilogram-meters
86.7964
inch-pounds
kilogram-meters
9.8067
Newton-meters
Newton-meters
0.7376
foot-pounds
Newton-meters
8.8508
inch-pounds
Newton-meters
0.1020
kilogram-meter

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SECTION 1
GENERAL
1.1 Introduction
The P92 is a twin seat, single engine light aircraft with a strut braced high wing and tricycle fixed landing gear with steerable
nose wheel.
It is an ASTM compliant airplane designed to be flown by sport pilot rated pilots as well as higher rated pilots.
This aircraft is designed and built in Italy and as such, was built using the metric system. Therefore, the primary numbers are
in metric and the US conversion is in parenthesis for your information.
This Flight Manual has been prepared to ASTM standards to provide pilots and instructors with information for the safe and
efficient operation of this aircraft.
This Flight Manual contains the following sections:
1. General Information
2. Operating Limitations
3. Weight & Balance
4. Performance
5. Emergency Procedures
6. Normal Procedures
7. Aircraft Ground Handling and Servicing
8. Required Placards and Markings
1.2 Certification Basis
This aircraft is certificated as a Special Light Sport Aircraft under FAR part 21.190 and complies with all applicable ASTM
standards.

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THREE VIEW DRAWING
Figure 1-1 General Views
Wing Span
8.77 m
(28.77 ft)
Length
6.81 m
(22.34 ft)
Tail height
2.66 m
(8.72 ft)
Propeller ground clearance
336 mm
(1.10 ft)

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1.3 Descriptive Data
1.3.1 Airframe
1.3.1.1 Wing
Wing Span
8.77 m (28.77 ft)
Wing Area
12.1 m2(130.24 ft2)
Aspect Ratio
6.35
Mean geometric chord
1.40 m (4.59 ft)
1.3.1.2 Fuselage
Overall length
6.81 m (22.34 ft)
Overall height
2.66 m (8.72 ft)
1.3.1.3 Landing Gear
Wheel track
1.84 m (6.04 ft)
Wheel base
1.74 m (5.70 ft)
Main gear tire
5.00-5
Nose Gear tire
5.00-5

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1.4 Powerplant
1.4.1 Engine
Manufacturer
Bombardier Rotax GmbH
Model
912 ULS2
Engine type
4 cylinder horizontally-opposed twins with
overall displacement of 1352 c.c., mixed cooling,
(water-cooled heads and air-cooled cylinders),
twin carburetors, integrated reduction gear with
torque damper.
Maximum power (at declared rpm)
73.5kW (98.5hp) @5800rpm (max.5’)
69.0kW (92.5hp) @5500rpm (cont.)
1.4.2 Propeller
Manufacturer
Sensenich
Model
W68T2ET-70J
Number of blades:
2
Diameter
1730 mm (no reduction allowed)
Type
Fixed pitch –wood
1.4.3 Oil System
Oil system
Forced type with external reservoir
Oil
Lubricant specifications and grade are detailed into the
“Rotax Operators Manual” and in its related documents.
Oil capacity
Max. 3 litres –min. 2.0 litres
1.4.4 Cooling
Cooling system
Mixed air and liquid pressurized closed circuit system
Coolant liquid
Coolant type and specifications are detailed into the
“Rotax Operator’s Manual” and in its related documents.
1.4.5 Fuel
Fuel tanks
Two wing tanks integrated within the wing’s leading
edge. Equipped with finger strainers outlet and with
drain fittings.
Capacity of each wing tank
45 litres
Tanks overall capacity
90 litres
Approved fuel
MOGAS ASTM D4814
MOGAS EN 228 Super/Super Plus (MIN RON 95)
AVGAS 100LL (ASTM D910)

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1.5 Weights
1.5.1 Maximum Weights
Maximumtake-off
weight:
600 kg (1320 lb )
Maximumlanding
weight:
600 kg (1320 lb )
Maximumbaggage
weight
20 kg (44 lb )
1.5.2 Standard Weights
Empty weight
380 kg
(837.78)
1.5.3 Specific Loadings
Wing loading
49.6 kg/m2
Power loading
6.1 kg/hp
NOTE
Standard weights are estimates based on standard equipment.
1.6 Standard Equipment
1.6.1 Flight Instruments
Airspeed Indicator, Altimeter, Vertical Speed Indicator, Compass
1.6.2 Engine instruments
Tachometer, Oil Pressure, Fuel Pressure, Oil Temperature, Cylinder Head Temperature, Left and Right Fuel
Quantity, Volt Meter
1.6.3 Warning Lights and Indicators
Trim Indicator, Flap Indicator, Generator Warning Light
1.6.4 Controls
Dual Stick Flight Controls and Rudder Pedals, Single Throttle, Throttle Friction Control, Engine Choke,
Electric Flaps, Hydraulic Disc Brakes with Parking Brake and toe brakes on both seats, Left and Right Fuel
Selector Valve, Direct Nose Wheel Steering (or pivoting NLG with differential breaking system)
1.6.5 Interior
Adjustable Pilot and Copilot Seats, reclining for baggages compartment access, Acoustic Cabin Soundproofing,
Adjustable Cabin Air Intakes, Cabin Heat and Windshield Defrost, 12V Power Outlet, Composite Instrument
Panel
1.6.6 Exterior
Composite fuselage structure, Composite wing tip and horizontal tail tip, Composite engine cowling, Landing
Light, Strobe Light, Fixed Landing Gear, Nose Gear Strut Fairing, Nose and Main Wheel Fairings

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1.6.7 Powerplant and Accessories
Rotax 912 ULS Engine (100 hp), Composite Covered Wood / Composite Propeller with Spinner , 12Volt 18 Ah
Battery, 18 Amp Alternator, Engine Driven Fuel Pump, Electric Starter, Engine Exhaust Muffler, Gascolator
with Quick Drain, Integral Wing Fuel Tanks with sump and quick drain, Integral INOX hoses and AN Fittings
for fuel line, All Electric Circuits Fuse Protected

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1.7 Airframe
1.7.1 Wing
The wing is of a rectangular planform, with a small tapering of the leading edge near the cabin, allowing an improved
visibility, also in steep turn. Its structure consists of a single spar metal torsion box. The aircraft is equipped with half-span
slot flaps, with the flap hinge positioned on the lower part of the wing. The wing box incorporates the integral fuel tanks of
45 liters each.
1.7.2 Fuselage
The fuselage is mainly made by carbon fibers composite materials. The fuselage is made by two main shells that are later
assembled bonding the two main bodies and the floor and adding aluminum stiffeners that allow the connection of the main
landing gear, seats, wing and instrument panel.
1.7.3 Empennage
The horizontal trimmable tail plane is all-moving type, which allows a high control authority and a better stick free stability.
The vertical tail is conventional fin and rudder type. Both horizontal and rudder structures are aluminum light alloy (2024-
T3 and 6061-T6), except fin, which is a carbon fiber unique body with the fuselage, and tips, which are in fiberglass.
1.7.4 Flight controls
The control surfaces are manually operated using a control stick for ailerons and stabilator and rudder pedals for the rudder;
Stabilator is actuated by push-pull rods and cables. Ailerons are actuated by push-pull rods on wing and cables in fuselage.
The flap control system is actuated by means of a linear electrical actuator connected to rods transmitting the movement to
the flap surfaces.
Longitudinal trim is provided by push/pull rod-type system controlled by an electrical actuator.

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1.7.5 Instrument Panel
Fig. 1-2 Instrument Panel
1.7.6 Seats
The Pilot and co-pilot seats are characterized by aluminium manufactured by Tecnam. It is covered by a cushion and
connected to the fuselage structure.
1.7.7 Doors
Two doors are provided on pilot and co-pilot side. Since the propeller is located on the nose of the aircraft and there are not
chances to endanger persons using those exits, the doors are also considered as emergency exits.
1.7.8 Baggage compartment
The baggage compartment is located behind the seats. Baggage shall be uniformly distributed on utility shelf and its weight
shall not exceed 20 kg. The c.g. must be computed before flight.