Tecnam P2008 JC Technical specifications

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Aircraft Flight Manual
Doc. No. 2008/100
Ed.1 – Rev. 0
2013, July 30th
TECNAM P2008 JC
MANUFACTURER: COSTRUZIONI AERONAUTICHE TECNAM S.r.l.
AIRCRAFT MODEL:P2008 JC
EASA TYPE CERTIFICATE NO:A.583 (DATED 2013, 27TH SEPTEMBER)
SERIAL NUMBER: …………..............
REGISTRATION MARKINGS: ………….………..
This Aircraft Flight Manual is approved by European Aviation Safety Agency
(EASA) and applies only EASA CS-VLA certified airplanes.
This Manual must be carried in the airplane at all times.
The airplane 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

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Aircraft Flight Manual
INDEX
SECTION 0
INDEX
1. RECORD OF REVISIONS.......................................................................................... 3
2. LIST OF EFFECTIVE PAGES .................................................................................... 8
3. FOREWORD.............................................................................................................11
4. SECTIONS LIST ......................................................................................................12

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Ed. 1, 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 iskept 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"; subsequentrevi-
sions are identified by the change of the code from "0" to "1" for the firstrevision
to the basic publication, "2" for the second one, etc.
Should be necessary tocompletely 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.
NOTE: It is the responsibility of the owner to maintain this handbook in a current
status when it is being used for operational purposes.

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Aircraft Flight Manual
RECORD OF REVISIONS
Rev
Revised
page Description of Revision Tecnam Approval
EASA Approval
or Under DOA
Privileges
DO OoA HDO
0 - First issue G. Paduano M. Landi M. Oliva
EASA approved as
part of Type
Investigation

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Aircraft Flight Manual
RECORD OF REVISIONS
Rev
Revised
page Description of Revision Tecnam Approval
EASA Approval
or Under DOA
Privileges
DO OoA HDO

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Aircraft Flight Manual
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Aircraft Flight Manual
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Aircraft Flight Manual
LOEP
Ed. 1, Rev. 0
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 orone variant of
these pages when the pages of some Supplementsare embodied.
Pages affected by the current revision are indicated by an asterisk (*) following the re-
vision code.
Edition 1, Rev 0 ..................... 30th July, 2013
Section Pages Revision
Section 0
Pages 1 thru 12
Rev 0
Section 1
Pages 1 thru 14
Rev 0
Section 2
Pages 1 thru 30
Rev 0
Section 3
Pages 1 thru 22
Rev 0
Section 4
Pages 1 thru 18
Rev 0
Section 5
Pages 1 thru 16
Rev 0
Section 6
Pages 1 thru 12
Rev 0
Section 7
Pages 1 thru 16
Rev 0
Section 8
Pages 1 thru 10
Rev 0
Section 9
Pages 1 thru 4
Rev 0

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Aircraft Flight Manual
FOREWORD
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3. FOREWORD
Tecnam P2008 JC is a single-enginetwo-seat aircraft with a strut braced high wingand-
fixedlanding 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 AERONAUTICHETECNAMs.r.l.
Via MAIORISE
CAPUA (CE) - ITALY
[phone]
[e-mail]

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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 (***) Section 9
(*) non-approved Section
(**) approved Section
(***) partially approved Section

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Section 1 – General
INDEX
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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
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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
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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

Section 1 – General
GENERAL FEATURES
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5. ENGINE
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 (98.6hp) @ 5800 rpm –5
minutes maximum.
69.0 kW (92.5hp) @ 5500 rpm (continu-
ous)
6. PROPELLER
Manufacturer GT Propeller
Model
GT-2/173/VRR-FW101 SRTC
Blades One-piece 2-blade fixed pitch, construct-
ed of wood materials, protective layer of
laminate.
Diameter 1730 mm (no reduction allowed)
Type Fixed pitch

Section 1 – General
GENERAL FEATURES
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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 630 kg (1388lb)
Wing Loading 51 kg/m2(10.6 lb/sqft )
Power Loading 6.29 kg/hp (14.09 lb/hp )

Section 1 – General
ACRONYMS AND TERMINOLOGY
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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.
VOOperating Manoeuvring speed is the speed above the which it is
not allowed to make full or abrupt control movement
VSStall Speed.
VS0 Stall Speed in landing configuration (flaps extended).
VS1 Stall speed in the given flap configuration.
VXBest Angle-of-Climb Speed is the speed which allows best ramp
climb performances.
VYBest Rate-of-Climb Speed is the speed which allows the best
gain in altitude over a given time.
VRRotation speed: is the speed at which the aircraft rotates about
the pitch axis during takeoff