Tecnam P2008 JC Technical specifications

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Aircraft Flight Manual
Doc. No. 2008/100
Ed. 2 – Rev. 2
2018, August 02th
TECNAM P2008 JC
MANUFACTURER: C. A.TECNAM S.r.l.
AIRCRAFT MODEL: P2008 JC
EASA TYPE CERTIFICATE NR.: A.583 (DATED 2013, 27 SEPTEMBER)
SERIAL NUMBER: ……………................
BUILD YEAR: ……………................
REGISTRATION MARKINGS: ……………................
This Aircraft Flight Manual is approved and applies only to EASA CS-VLA certified
airplanes.
This Manual must be carried in the airplane at all times.
This aeroplane has to be operated in compliance with procedures and limitations contained
herein.
Costruzioni Aeronautiche TECNAM srl
Via Maiorise
CAPUA (CE) – Italy
Tel. [phone]
WEB: www.tecnam.com
1112
2018
G-JACN
Updated AFM incorporating Supplements for G-JACM
Based on Dec No 2008/100 Ed 2 - Rev 1 2018, March 12th
FOR REFERENCE ONLY - ORIG AFM IS DEFINITIVE
Updated AFM incorporating Supplements
Based on Dec No 2008/100
Ed 2 - Rev 1 2018, March 12th
FOR REFERENCE ONLY
ORIGINAL AFM IS DEFINITIVE

Ed. 2, Rev. 0
Aircraft Flight Manual
INDEX
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SECTION 0
INDEX
1.RECORD OF REVISIONS.......................................................................................... 3
2.LIST OF EFFECTIVE PAGES .................................................................................... 7
3.FOREWORD.............................................................................................................. 9
4.SECTIONS LIST ......................................................................................................10

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Ed. 2, Rev. 0
Aircraft Flight Manual
RECORD OF REVISIONS
1. RECORD OF REVISIONS
Any revision to the present Manual, except actual weighing data, is recorded: a
Record of Revisions is provided in this Section and the operator is advised 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 “0”; subsequent revi-
sions are identified by the change of the code from “0” to “1” 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 etc).
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.
It is the responsibility of the owner to maintain this handbook
in a current status when it is being used for operational pur-
poses.
NOTE

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Ed. 2, Rev. 2
Aircraft Flight Manual
RECORD OF REVISIONS
Rev
No
Revised
page
Description of
Revision
Tecnam Approval
EASA Approval or
Under DOA
Privileges
DO OoA HDO
0 all Editorial revision. A. Sabino C. Caruso M. Oliva
Approved under the
authority of DOA,
ref. EASA.21J.335
(MOD2008/097.180126)
1
0-1,4,7 Cover, RoR and LOEP updated.
A. Sabino C. Caruso M. Oliva
.Approved under the
authority of DOA,
ref. EASA.21J.335
(MOD2008/103.180312)
2-6
Airspeed indicator markings
amended; the indication is now
proper for both analogue and dig-
ital instruments.
3-20 Note amended.
4-3, 4-4
Note amended; information have
been added to airspeed for nor-
mal operations table; paragraph
shifted from page 3 to page 4.
4-9,
4-12 thru 17
Checklists amended; note to PFI
revised; speed information have
been moved to page 4-3.
6-9 W&B calculation sample.
6-11 thru 13 Equipment list.
7-1,5 thru 16 Contents rearranged.
9-3 Supplements list updated.
2
0-1,4,7 Cover, RoR and LOEP updated.
G.Valentino D.Ronca M. Oliva
Approved under the
authority of DOA,
ref. EASA.21J.335
(MOD2008/111.180802)
4-12 Added check of pitot heating sys-
tem (if installed)
6-11 thru 13 Equipment list.
9-3 Supplements list updated: added
Supplement S14

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Aircraft Flight Manual Ed. 2, Rev. 0
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Aircraft Flight Manual
LOEP
Ed. 2, Rev. 2
2. LIST OF EFFECTIVE PAGES
The List of Effective Pages (LOEP), applicable to manuals of every operator, lists all
the basic AFM pages: each manual could contain either basic pages or one variant of
these pages when the pages of some Supplements are embodied.
Pages affected by the current revision are indicated by an asterisk (*) following the re-
vision code.
Edition 1, Rev 0 30 July 2013
Edition 1, Rev 1 25 March 2015
Edition 1, Rev 2 7 April 2015
Edition 1, Rev 3 13 April 2015
Edition 1, Rev 4 14 July 2015
Edition 1, Rev 5 15 December 2015
Edition 1, Rev 6 20 December 2016
Edition 2, Rev 0 15 January 2018
Edition 2, Rev 1 12 March 2018
Edition 2, Rev 2 02 August 2018
Section Pages Revision
Section 0 2, 3, 5, 6, 8,9, 10 Rev 0
1, 4, 7 Rev 2
Section 1 1 thru 14 Rev 0
Section 2 1 thru 5, 7thru 30 Rev 0
6 Rev 1
Section 3 1 thru 19, 21, 22 Rev 0
20 Rev 1
Section 4 1, 2, 5 thru 11, 13, 14, 18 Rev 0
3, 4, 15 thru 17 Rev 1
12 Rev 2
Section 5 1 thru 16 Rev 0
Section 6 1 thru 8, 10, 14 Rev 0
9 Rev 1
11 thru 13 Rev 2
Section 7 2 thru 4 Rev 0
1, 5 thru 16 Rev 1
Section 8 1 thru 10 Rev 0
Section 9 1, 2 and 4 Rev 0
3 Rev 2

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Ed. 2, Rev. 0
Aircraft Flight Manual
FOREWORD
3. FOREWORD
Tecnam P2008 JC is a single-engine two-seat aircraft with a strut braced high wing and
fixed landing gear.
Section 1 provides 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:
COSTRUZIONI AERONAUTICHE TECNAMs.r.l.
Via MAIORISE
CAPUA (CE) - ITALY
[phone]
[email protected]

Ed. 2, Rev. 0
Aircraft Flight Manual
SECTIONS LIST
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4. SECTIONS LIST
General (*) Section 1
Limitations (**) Section 2
Emergency Procedures (**) Section 3
Normal Procedures (**) Section 4
Performance (***) Section 5
Weight and balance (*) Section 6
Airframe and Systems description (*) Section 7
Ground Handling and Service (*) Section 8
AFM Supplements list (*) Section 9
(*) non-approved Section
(**) approved Section
(***) approved Section except for pages 5-1 thru 5-4, 5-6, 5-11 thru 5-13

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Section 1 –General
INDEX
Ed. 2, Rev 0
SECTION 1 - GENERAL
INDEX
1. INTRODUCTION .................................................................................................. 3
2. CERTIFICATION BASIS ....................................................................................... 3
3. WARNINGS –CAUTIONS –NOTES ...................................................................... 3
4. THREE-VIEW AND DIMENSIONS ......................................................................... 4
5. ENGINE ............................................................................................................... 6
6. PROPELLER......................................................................................................... 6
7. FLIGHT CONTROL SURFACES TRAVEL.............................................................. 7
8. SPECIFIC LOADINGS........................................................................................... 7
9. ACRONYMS AND TERMINOLOGY ....................................................................... 8
10. UNIT CONVERSION CHART .............................................................................. 13
11. LITRES / US GALLONS CONVERSION CHART .................................................. 14

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Section 1 –General
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Section 1 –General
INTRODUCTION
Ed. 2, Rev 0
1. INTRODUCTION
The Flight Manual has been prepared to provide pilots and instructors with in-
formation for the safe and efficient operation of this very light airplane.
This manual includes the material required to be furnished to the pilot of CS-
VLA. It also contains supplemental data supplied by the airplane manufacturer.
2. CERTIFICATION BASIS
This type of aircraft has been approved by the European Aviation Safety Agency
in accordance with CS-VLA including Amendment 1 and the Type Certificate
No.EASA.A.583 has been issued on (date) 27th September 2013.
Category of Airworthiness: Normal
Noise Certification Basis: EASA CS 36 Amendment 2.
3. WARNINGS –CAUTIONS –NOTES
Following definitions apply to warnings, cautions and notes used in the Aircraft
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.
draws the attention to any special item not directly related to safety but
which is important or unusual.
.
NOTE

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Section 1 –General
THREE-VIEW AND DIMENSIONS
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4. THREE-VIEW AND DIMENSIONS
Figure 1 – General views

Section 1 –General
GENERAL FEATURES
Ed. 2, Rev 0
Page 1 - 5
Dimensions
Wing
Wing Span
9.00 m (29.5 ft)
Wing Area
12.16 m2 (130.9 ft2)
Aspect Ratio
6.7
Taper Ratio
0.8
Wing chord
1.373 m (4.5 ft)
Fuselage
Overall length
6.93 m (22.9 ft)
Overall width
1.20 m (3.9 ft)
Overall height
2.67 m (8.8 ft)
Empennage
Stabilator span
2.90 m (9.51 ft)
Stabilator area
2.03 m2 (21.8 ft2)
Vertical tail area
1.06 m2 (11.4 ft2)
Landing Gear
Wheel track
1.8 m (5.9 ft)
Wheel base
1.94 m (6.4 ft)
Main gear tire
5.00-5
Nose Gear tire
5.00-5

AFMS S9 - MTV-34 Propeller for aircraft with MTOW Increment at 650 kg
Page MT1-6
Ed 2, Rev. 0
Section 1 - General -
GENERAL FEATURES
5ENGINE
Manufacturer
Bombardier-Rotax GmbH
Model
912 S2
Engine type
4 cylinders horizontally opposed with
1352 c.c. of overall displacement, liquid
cooled cylinder heads, ram-air cooled
cylinders, two carburetors, integrated re-
duction gear box with torsional shock ab-
sorber and overload clutch.
Maximum power (at declared rpm)
73.5 kW (98.6 hp) @ 5800 rpm
5 minutes maximum.
69.0 kW (92.5 hp) @ 5500 rpm
maximum continuous.
6PROPELLER
Manufacturer
MT Propeller
Model
MTV-34-1-A/170-202
Number of blades
3
Construction
Laminated hard wood with epoxy fibre glass cover
Diameter
1700 mm
Type
Fixed pitch

AFMS S9 - MTV-34 Propeller for aircraft with MTOW Increment at 650 kg
Page MT1-7
Ed 2, Rev. 0
Section 1 - General -
GENERAL FEATURES
7. FLIGHT CONTROL SURFACES TRAVEL
Ailerons
Up 22° Down 14 ° ( 2°)
Stabilator (refer to Trailing Edge)
Up 4° Down 15° ( 2°)
Stabilator trim tab (refer to Trailing Edge)
Up 2°; Down 12° ( 1°)
Rudder
RH 25° LH 25° ( 2°)
Flaps
0°; 35° ( 1°)
8. SPECIFIC LOADINGS
MTOW 650 kg (1433lb)
Wing Loading
53.5 kg/m2 (10.9 lb/sqft )
Power Loading
6.59 kg/hp (14.53 lb/hp )

Section 1 –General
ACRONYMS AND TERMINOLOGY
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0
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9. ACRONYMS AND TERMINOLOGY
KCAS
Calibrated Airspeed is the indicated airspeed expressed in knots,
corrected taking into account the errors related to the instrument
itself and its installation.
KIAS
Indicated Airspeed is the speed shown on the airspeed indicator
and it is expressed in knots.
KTAS
True Airspeed is the KCAS airspeed corrected taking into ac-
count altitude and temperature.
VA
Design Manoeuvring 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 flaps extended.
VNO
Maximum Structural Cruising Speed is the speed that should not
be exceeded, except in smooth air and only with caution.
VNE
Never Exceed Speed is the speed limit that may not be exceeded
at any time.
VO
Operating Manoeuvring speed is the speed above the which it is
not allowed to make full or abrupt control movement
VS
Stall Speed.
VS0
Stall Speed in landing configuration (flaps extended).
VS1
Stall speed in the given flap configuration.
VX
Best Angle-of-Climb Speed is the speed which allows best ramp
climb performances.
VY
Best Rate-of-Climb Speed is the speed which allows the best
gain in altitude over a given time.
VR
Rotation speed: is the speed at which the aircraft rotates about
the pitch axis during takeoff

Section 1 –General
ACRONYMS AND TERMINOLOGY
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0
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Meteorological terminology
ISA
International Standard Atmosphere: is the air atmospheric standard
condition at sea level, at 15°C (59°F) and at 1013.25hPa
(29.92inHg).
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 1000 ft of altitude.
HP
Pressure Altitude is the altitude read from an altimeter when the
barometric subscale has been set to 1013 mb.

Section 1 –General
ACRONYMS AND TERMINOLOGY
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0
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Aircraft performance and flight planning terminology
Crosswind Velocity
is the velocity of the crosswind component
for the which adequate control of the air-
plane during takeoff and landing is assured.
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.
TOR
is the takeoff distance measured from actual
start to wheel liftoff point.
TOD
is total takeoff distance measured from start
to 15m obstacle clearing.
GR
is the distance measured during landing
from actual touchdown to stop point.
LD
is the distance measured during landing,
from 15m obstacle clearing to actual stop.
S/R
is the specific range, that is the distance (in
nautical miles) which can be expected at a
specific power setting and/or flight configu-
ration per kilogram of fuel used.