Tecnam P2010 2015 Technical specifications

Aircraft Flight Manual
Doc. No. 20101100
Ed.2 Rev.12
2019, October 21
TECNAM P2010
MANUFACTURER: rn\17ll n KJNI AHWNA1 f11 Cll H TECNAM .\ r I.
AIRCRAFT MODEL: P10/0
EASA TYPE CERTIFICATE No : EASA.A.576 (DATED 2014, SEPTEMBER 26
111
)
SERIAL NUMBER: .................. . ? . ?. ~ ... .... . ...... .
BUILD YEAR: ... . .... ..
2015
HB-KMT
REGISTRATION MARKING S :.. . . ...... .. . .
This manual 1s approved m accordance with 14 CFR 21 29 for US registered air-
craft, and is approved by the Federal Aviation A dn11mstrat1 on.
This Manual must be e arn ed m the airplane at all limes.
The a1rplane has lo be operated m compliance with procedures and lim1/alions
containedherein.
Costruzioni Aeronautiche TECNAM srl
Via Maiorisc
CAPUA (CE)-Italy
Tel. [phone]
WEB : www.tecnam.com

INDEX
1. RECORD OF REVISIONS ............................................................... 3
2. LIST OF EFFECTIVE PAGES .......................................................... 7
3. FOREWORD ................................................................................... 8
4. SECTIONS LIST ............................................................................ 9
Aircraft Flight Manual
INDEX
2"J Ed1t1on - Rev . 0

1. RECORD OF REVISIONS
Any revision to the present Manual, except actual weighing data, is recorded: a
Record of Revisions is provided at the front of this manual and the operator is ad-
vised to make sure that the record is kept up-to-date.
The Manual issue is identified by Edition and Revision codes reported on each
page, lower right side.
The revision code is numerical and consists of the number "O"; subsequent revi-
sions are identified by the change of the code from "O" to "I" for the first revision
to the basic publication, "2" for the second one, etc.
Should be necessary to completely reissue a publication for contents and format
changes, the Edition code will change to the next number ("2" for the second edi-
tion. "3" for the third edition ctc).
Additions, deletions and revisions to existing text will be identified by a revision
bar (black line) in the left-hand margin of the page, adjacent to the change.
When technical changes cause expansion or deletion of text which results in un-
changed text appearing on a different page, a revision bar will be placed in the
right-hand margin adjacent to the page number of all affected pages providing no
other revision bar appears on the page.
These pages will be updated to the current regular revision date.
NOTE: It is the responsibility of the owner to maintain this handbook in a current
status when it is being used for operational purposes.
Aircraft Flight Manual
RECORD OF REVISIONS
2"'
1 Edition, Rev. 0

Rev
Revised
page
0 -
2-5 thru 16
I 9-3
5-13 lhru 14
2
6-12chru 13
9-3
0-1, 4, 7
3-4
3 4-7
4-23
9-3
0-1, 0-4, 0-7
4 6-12,6-13
9-3
0-1. 0-4, 0-7
2-9
5 6-12
co 14
7-18
9-3
0-1, 0-4, 0-7
6 9-3
Description of
Tec:nam Approval
Revision DO OoA
New Ed111on D. Ronca C.
Caruso
Amended to add the wording
.. Approved'" m order lo belier D Ronca C. Caruso
1denlify the pages approved ac-
cordinc. to EASA ree.ulution
Supplemenl Lisi Index amended
D. Ronca C Caruso
Add Supplement 004
Amended cruise performance lo
add fuel consumpllon for differ-
ent power seuinA
Amended Equipment lisl D. Ronca C Caruso
Supplemenl Lisi Index amended
Add Supplemenl DOS
Cover, RoR and LOEP updaced.
Reforence airspeeds table added.
Airspeeds Cubie revised. A. Sabino C. Caruso
Glide Speed revised
Supplemenls lisl updated.
Cover, RoR and LOEP updated.
Amended equipmenc lisl A. Sabino
D. Ronca
Supplemenls D 12 10 D 15 added.
Cover, RoR and LOEP updated.
Caulion on supplemental oxygen
Equipment lisc update
A. Sabino D. Ronca
Descriptton wording
Supplemenls Lisi
Cover, RoR and LOEP updated. G. Valentino D. Ronca
Supplements List
Aircraft Flight Manual
RECORD OF REVISIONS
HOO
M. Oliva
M.Oliva
M. Oliva
M. Oliva
M Oliva
M Oliva
M. Oliva
M Ohva
Page 0 -4
EASA Approval
OrUnderDOA
Prlvile!!es
Approved under the
authority of DOA
rcr EASA21J 335
(MOD2010/067 15!030)
Approved under the
authority or DOA
ref. EASA 2IJ 335
(MOD2010/070 160118)
EASA approval
N"l0055692
Approved under the
authority or DOA
rer EASA 2IJ 335
(MOD2010/103 161026)
Approved under the
authoncy or DOA
rer EASA 2IJ 335
(MOD2010/131 180403)
Approved under the
authority or DOA
rcr EASA 2IJ 335
(MOD2010/140 180611)
Approved under the
authority or DOA
rer EASA 21J 335
(MOD2010/150 181022)
Approved under the
authonty or DOA
rer EASA 21J 335
(MOD2010/156 190404)
2"J Ed1110n, Rev. 6

Rev
Revised
page
0-1,5, 7
7
6-1,4.
7 lo 10, 12
9-3
0-1,5, 7
6-13
8 7-5,7,30
9-3
0-1,5. 7
1-9. II, 12
9 3-21
7-28, 33
9-3
0-1,5,7
5-7
10
7-8
9-3
0-1,5,7
1-10
2-9
II
3-11,13,16,19
4-19.
20,24,25,26
6-5.6
7-8
9-3
Description of
Tecnam Approval
Revision DO OoA
Cover, RoR and LOEP updated.
Weighing procedure and weighl
A. Sabino D Ronca
and balance procedure amended.
couiomenl list undated.
Sunnlemenls Lisi undated.
Cover, RoR and LOEP updated.
Equipment list updated
lnnating pressure values indico-
A. Sabmo
D Ronca
lions amended for compatibility
with different annroved tvres
Supplements list updated
Cover, RoR and LOEP updated.
Added acronyms
Typo errors G. Valentino
D. Ronca
Deleted call sigu, standord1Zed
ELT olacards
Supplements list updated
Cover, RoR and LOEP updated
Demonstrated crosswind increase
A. Glorioso
(OJT) D. Ronca
Typo errors G. Valentino
Supplements list updated
Cover, RoR and LOEP updated
Added avionics system acronyms
Typo error
Emergency procedures
improvement
A. Glorioso D Ronca
T .. rnn errors
Normal procedures improvement
Tvnn errors
Form update
System description 1mprovemcn1
Supplements list updated
Aircraft Flight Manual
RECORD OF REVISIONS
HOO
M.Oliva
M.Oliva
M Oliva
M.Oliva
M Oliva
Page 0 - 5
EASA Approval
OrUnder DO A
Privile11es
Approved under the
Rulhorily of DOA
ref EASA 211 31~
(MOD2010/166 190418)
Approved under lhe
authority of DOA
ref EASA.21J 315
(MOD2010/170 190522)
Approved under the
authority of DOA
ref EASA 211 335
(MOD2010/173 190705)
Approved under the
authority of DOA
ref EASA 21J 335
(MOD2010/176 190913)
Approved under the
authon1y of DOA
ref EASA 211 335
(MOD2010/181 191017)
2"'
1 Edition, Rev.
12

Rev
12
Rtvised D~rlption of
Tecnam Approval
page Revision
0-1,5,6,7 Cover, RoR nnd LOEP updated
6-5,6 Typo errors
9-3 Typo error
DO: Design Organization
OoA: Office of Airworthiness
HOO: Head of Design Organization
DO
OoA
A. Glorioso D. Ronca
Aircraft Flight Manual
RECORD OF REVISIONS
HOO
M Oliva
EASA Approval
OrUnderDOA
Prlvileees
Approved under 1he
authority or DOA
ref. EASA.2 IJ 335
(MOD20I0/185 191021)
2"J Ed1110n, Rev. 12

2. LIST OF EFFECTIVE PAGES
The List of Effective Pages (LOEP), applicable to manuals or every operator, lists all the basic
AFM pages: each manual could contain either basic pages or one variant or these pages when
the pages or some Supplements are embodied.
Pages afTected by the current revision are indicated by an asterisk (*) following the revision
code.
Should supplements be embodied in accordance with approved instructions, make reference to
the LOEP addressed on Supplements themselves.
lst Edition.••.•.....•..•...•.•• September 26, 2014
2•d Edition •••.••...•.....•••.•• October 30, 2015
Section
Pages
Section 0 2, 3, 8, 9,
IO
4
I, 5, 6, 7
Section I I thru 8,
13 thru 16
9, 11, 12
10
Section 2 I thru 4
5 thru 8, IO thru 16
9
Section 3 3, 5 thru
IO, 12, 14, 18, 20, 22 thru 24, 26, 28, 30
1,2,,4, 15, 17,25,27,29
21
11, 13, 16, 19
Section 4 I thru 6, 8 thru
18, 21, 22
7,23
19,20,24,25,26
Section 5 I thru
12
13 thru 14
15 thru 17
Section 6 2 thru 3, 4,
11
14
I, 4, 7 thru 10, 12
13
5,6
Section 7 I thru 4, 6, 9 thru
17, 19 thru 27, 29, 31 thru 38
18
5, 7, 30
28,33
8
Section S I thru
16
Sunnlement List
Section 9 I, 2, 4
3
Revision
Re\ ' 0
Rev 6
Rev 12
RevO
Rev9
Rev II
RevO
Rev I
Re\' II
RevO
Rev3
Rev9
Rev II
RevO
Rev3
Rev II
RevO
Rev 2
RevO
RevO
Rev 5
Rev 7
Revs
Rev.12
RevO
Rev 5
Revs
Rev 9
Rev II
RevO
RevO
Rev 12
Suoolements LOEP: make reference to the Suonlements Cover Pa~es
Aircraft Flight Manual
LIST OF EFFECTIVE PAGES
2"J Edition, Rev. 12

3. FOREWORD
Section I supplies general information and it contains definitions, symbols explana-
tions, acronyms and terminology used.
Before using the airplane, you are recommended to read carefully this manual: a deep
knowledge of airplane features and limitations will allow you for operating the airplane
safely.
For further information, please contact:
C'OSJ'/IUZIONI Al :" llONAlrtlCHl i TECNAM s.r.I.
Via MAIORISE
CAPUA ( CE) - ITALY
'1 +390823.99.75.38
m [e-mail]
, :;;. ,www.tecnam.com
Aircraft Flight Manual
FOREWORD
2" JEdllwn, Rev. 0

4. SECTIONS LIST
General(*)
Section I
Limitations (**) Section 2
Emergency Procedures (*) Section 3
Normal Procedures(*) Section 4
Performances (*) Section 5
Weight and Balance(*) Section 6
Airframe and Systems description (*) Section 7
Airplane Care and Maintenance(*) Section 8
Supplements(***)
(•) non-approvtd Sttlion
c••) approvtd Sttlion
Section 9
(•••)partially approvtd Stclion -appro\-cd pam, if any, art rtporttd in lht suppltmtnls .
Aircraft Flight Manual
SECTIONS LIST
2"J Edl/ton, Rev. 0

INTENTIONALLY LEFT BLANK
2"J Ed11wn, Rev. 0
Aircraft Flight Manual

SECTION 1 - GENERAL
INDEX
1. INTRODUCTION ............................................................................... 3
2. CERTIFICATION BASIS .................................................................... 3
3. WARNING- CAUTION-NOTE ......................................................... 3
4. THREE-VIEW AND DIMENSIONS ..................................................... 4
5. ENGINE ............................................................................................ &
6. PROPELLER ...................................................................................... 6
7. FLIGHT CONTROL SURFACES TRAVEL .......................................... 7
B. SPECIFIC LOADINGS •••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••7
9. ACRONYMS AND TERMINOLOGY .................................................... 9
10. UNIT CONVERSION CHART ........................................................... 14
11. LITRES I US GALLONS CONVERSION CHART .............................. 15
Section 1 - General
INDEX
l"d Edition, Rev .O

INTENTIONALLY LEFT BLANK
Section 1 - General
:znd Edrt10n, Rev.O

1. INTRODUCTION
The Aircraft Flight Manual has been prepared to provide pilots and instructors
with information for the safe and efficient operation of this aeroplane.
This manual also contains supplemental data supplied by the aeroplane manufac-
turer.
2. CERTIFICATION BASIS
This type of aircraft has been approved by the European Aviation Safety Agency
in accordance with CS-23 including Amendment 2 and the Type Certificate No .
EASA.A.576 has been issued on 26
111
September 2014.
Category of Airworthiness: Normal.
Noise Certification Basis: EASA CS 36 Amendment 2.
This type of aircraft has been validated also in the normal category of 14 CFR
part 23 and part 36
3. WARNING - CAUTION - NOTE
Following definitions apply to warnings, cautio ns and notes used in the Aircraft
Flight Manual.
I
.
means that the non-observation of the corresponding procedure
leads to an immediate or important degradation of the flight safety.
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
Draws the attention to any special item not directly related to safety
but which is important or unusual.
Pagel-3
Section 1 - General
2 "'
1Edlflon, Rev.O
INTRODUCTION

4. THREE-VIEW AND DIMENSIONS
Cl
.....
~~
D. >
::E ...I
c( ~
Zw
(,) z
w w
.... Cl
!i
>
....
z
0
a:
...
Figu"' I - General views
Section 1 - General
THREE-VIEW AND DIMENSIONS
2"d Edition, Rev. 0

Dimensions
Overall dimensions
Wing Span ... ....... ..... ........ ... ......... .... 10.30 m / 33.79 ft
Overall Length .......... ,...... .. .. .. ....... ... 7. 97 mI 26.15 ft
Overall height ........ ................... .. ....... 2. 64 mI 8. 66 ft
Stabilator Span .. ...................... . ......... 3. 35 m/ 10 . 99 ft
Wing
Wing surface .......... ... .. . ....... . ........ .. 13.9 m2 I 149 .6 ft2
Mean Geometric Chord .. .... ... .. .... .. ....... 1.349 m I 4.427 ft
Dihedral .......................................... 1°
Aspect ratio ................................ ..... 7. 63
Fuselage
Cabin width .................................... .
Cabin length .. .. ....... ....... ............ .. .....
Landing Gear
1.14 m / 3.74 ft
2.3 m / 7. 54 ft
Wheels Track ....... ........ .............. ...... 2.1m I 6. 89 ft
Wheels base .................................. .. 2. 15 m 17 . 05 ft
Main Gear Tire .......... ....... .. .......... .. 6. 00-6
NoseGearTire ............................. .. 5. 00-5
Section 1 - General
THREE-VIEW AND DIMENSIONS
2' "1Edition, Rev.O

AFMS N·Do7 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
~TECNAM ~~@11@
0
&lkr@[i'~ l:PD~@OuQ 1!'1J@[]i)(![]@0 Page APV I-6
5.ENGINE
Manufacturer ..... .. ....... .. .... ....... .... Lycoming Engines
Model ............ .... .. .. .... ... .... . ... .... .. .10-360-MIA
Type Certificate ...................... ... ....EASA TCDS no. IM.E.032
Engine type Fuel injected (10), direct drive, four
cylinder horizontally opposed, air
cooled with down exhaust outlets.
Maximum power 134.0 kW (180hp)@2700 rpm
Maximum continuous power ... ...... ......129.2 kW (I 73 . 3hp)@2600 rpm
6. PROPELLER
Manufacturer ...... ...... .. ... ... .... ... .. ..MT Propeller
Model ............ .. .. .. ............ .. .... ....MTV-15-8/193-52
Type Certificate .... .. ............ ... . ... ... EASA TCDS no. P.098
Blades/hub ... ............ ......... ..... . .... wood/composite 2-blades -aluminum hub
Diameter . ........ .. ....... ...... .... . ...... 1930 mm (76 in) (no reduction is permitted)
Type ... ... .. . .. ....... ... ..... . ... ... Variable pitch
GOVERNOR
Manufacturer ... ..... ... ... ...... ... ... MT Propeller
Model ... .. . .. . ............ .. .... ......... P-860-23:
Type ... .. .. ............. ... .... .. Hydraulic
Section 1 - General
Ed. 2, R ev. O
GENERAL FEATURES

7. FLIGHT CONTROL SURFACES TRAVEL
Ailerons Up 19°; Down
14 ° (± 2°)
Stabilator• Up 6°; Down 17°
(± 2°)
Stabilator trim tab Up 3°; Down 15°
(± 1°)
Rudder RH 25°; LH 25°
(± 2°)
Rudder trim tab
RH 20°; LH 20° (± 2°)
Flaps 0°; 20°; 40°
{± I0)
*degrees are measured from the Stabilator Leading Edge.
8. SPECIFIC LOADINGS
MTOW 1160 kg (2557 lb)
Wing Loading 83.45 kg/m2 (17.09
Jb/ft2)
Power Loading 6.44 kg/hp (14.21 lb/hp)
Section 1 - General
2' "1 Edition, Rev .a
GENERAL FEATURES

INTENTIONALLY LEFT BLANK
Section 1 - General
2"d Edition, Rev. 0

9. ACRONYMS AND TERMINOLOGY
KCAS
KIAS
KTAS
Vo
Vs
Vso
Vx
Calibrated Airspeed is the indicated airspeed expressed in knots,
corrected taking into account the errors related to the instrument
itself and its installation.
Indicated Airspeed is the speed shown on the airspeed indicator
and it is expressed in knots.
True Airspeed is the KCAS airspeed corrected taking into ac-
count altitude and temperature.
Design Manoeuvring speed is the speed above the which it is not
allowed to make full or abrupt control movement.
Maximum Flap Extended speed is the highest speed permissible
with flaps extended.
Maximum Structural Cruising Speed is the speed that should not
be exceeded, except in smooth air and only with caution.
Never Exceed Speed is the speed limit that may not be exceeded
at any time.
Operating Manoeuvring speed is the speed above the which it is
not allowed to make full or abrupt control movement
Stall Speed.
Stall Speed in landing configuration (flaps and landing gear ex-
tended).
Stall speed in clean configuration (flaps 0°).
Best Angle-of-Climb Speed is the speed which results in the
greatest gain of altitude with respect to a given horizontal dis-
tance.
Vv Best Rate-of-Climb Speed is the speed which results in the great-
est gain in altitude in a given time.
VR Rotation speed: is the speed at which the aircraft rotates about
the pitch axis during takeoff
VwF Lift off speed: is the speed at which the aircraft generally lifts off
from the ground.
V oo. Obstacle speed (screen speed. V son}: is the speed at which the
aircraft flies over a I 5m obstacle during takeoff or landing.
V
6
1;c1c Glide speed: is the speed of maximum efficiency (to fly the long-
est distance per unit of altitude lost)
Page I - 9
Section 1 - General
2"" Edition. Rev.9
ACRONYMS AND TERMINOLOGY

Meteorological terminology
ISA International Standard Atmosphere: is the air atmospheric standard
condition at sea level, at 15 °C (59 °F) and at 1013. 25 hPa
(29.92 inHg).
QFE Official atmospheric pressure at airport level: it indicates the air-
craft absolute altitude with respect to the official airport level.
QNH Theoretical atmospheric pressure at sea level: is the atmospheric
pressure reported at the medium sea level, through the standard air
pressure-altitude relationship, starting from the airport QFE.
OAT Outside Air Temperature is the air static temperature expressed in
degrees Celsius (°C).
Ts Standard Temperature is 15 °C at sea level pressure altitude and
decreased by 2 °C for each I OOO ft of altitude.
Hp Pressure Altitude is the altitude read from an altimeter when the
barometric subscale has been set to I013 mb.
Avionics System Acronyms
XPDR
Transoonder
Pagel-JO
Section 1 - General
2"d Edition, Rev. II
ACRONYMS AND TERMINOLOGY