Tecnam P2006T Technical specifications

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Aircraft Flight Manual
Doc. No. 2006/044
4th Edition – Rev. 5
2018, January 12th
TECNAM P2006T
MANUFACTURER: COSTRUZIONI AERONAUTICHE TECNAM S.r.l.
AIRCRAFT MODEL: P2006T
EASA TYPE CERTIFICATE NO: A .185 (DATED 2009, JUNE 5TH)
SERIAL NUMBER: …………….................
BUILD YEAR: ……….………...................
REGISTRATION MARKINGS: ……………...
This Aircraft Flight Manual is approved by European Aviation Safety Agency
(EASA).
This Manual contains information required by the FAA to be furnished to the pilot
for operation in the U.S.A. plus information supplied by the manufacturer. It is
approved by EASA on behalf of the FAA per FAR 21.29.
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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4th Edition - Rev. 0
Aircraft Flight Manual
INDEX
SECTION 0
INDEX
1. RECORD OF REVISIONS ............................................................... 3
2. LIST OF EFFECTIVE PAGES ......................................................... 7
3. FOREWORD ................................................................................. 10
4. SECTIONS LIST........................................................................... 11

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4th Edition - 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 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 "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.
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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4th Edition - Rev. 5
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
D. Ronca
M. Oliva
M. Oliva
1
0-4,8
Amended ROR and LOEP
D. Ronca
M. Oliva
M. Oliva
Approved under the au-
thority of DOA,
ref. EASA.21J.335
(MOD2006/270.160429)
6-12
Amended Equipment List
9-1,2,5,7
Amended Supplement List
2
0-4,8
Amended ROR and LOEP
D. Ronca
M. Oliva
M. Oliva
Approved under the au-
thority of DOA,
ref. EASA.21J.335
(MOD2006/290.170316)
4-3,4,18,19
Amended General recommendations
and “Prior to Takeoff” procedure
5-16
Amended Cruise performances
9-1,2,4,5,7
Amended Supplement List Index
3
0-1,4,7
Amended cover page, ROR and
LOEP
A. Sabino
C. Caruso
M. Oliva
Approved under the au-
thority of DOA,
ref. EASA.21J.335
(MOD2006/315.170901)
6-11, 12, 13
Amended Equipment List
9-2,3,8
Amended Supplement List, Modi-
fied Introduction,
4
0-1,4,7, 12
Amended cover page, ROR and
LOEP. Blank page added.
A. Sabino
C. Caruso
M. Oliva
Approved under the au-
thority of DOA,
ref. EASA.21J.335
(MOD2006/318.171205)
4-3,11,16,
17,19,20,25
Amended “Pre-flight”, “Engine
starting”, “Prior to takeoff” and
“Parking/Shut down” checklists
5-23
Blank page removed
6-11, 12, 13
Amended Equipment List
5
0-1,4,7,12
Amended cover pages, ROR and
LOEP. Blank page added.
A. Sabino
C. Caruso
M. Oliva
Approved under the au-
thority of DOA,
ref. EASA.21J.335
(MOD2006/325.180112)
2-11
Amended caution on supplemental
oxygen use.
2-12
Integration of info formerly con-
tained in Supp. A27, G16, G18.
4-19,22
Amended procedures.
6-11,12,13
Amended equipment list.
9-all
Amended Supplement List.

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4th Edition - Rev. 5
Aircraft Flight Manual
LIST OF EFFECTIVE PAGES
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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.
Should the Supplements be embodied in accordance with approved instructions, make
reference to the LOEP addressed on the Supplements themselves.
Ed 1 Rev 0
May 25, 2009
Ed 3 Rev 4
May 5, 2014
Ed 2 Rev 0
March 29, 2010
Ed 3 Rev 5
June 10, 2015
Ed 2 Rev 1
April 27, 2010
Ed 4 Rev 0
July 25, 2015
Ed 2 Rev 2
November 12, 2010
Ed 4 Rev 1
April 6, 2016
Ed 2 Rev 3
March 4, 2011
Ed 4 Rev 2
March 16, 2017
Ed 3 Rev 0
December 22, 2011
Ed 4 Rev 3
September 1, 2017
Ed 3 Rev 1
October 15, 2012
Ed 4 Rev 4
December 5, 2017
Ed 3 Rev 2
June 4, 2013
Ed 4 Rev 5
January 12, 2018
Ed 3 Rev 3
February 13, 2014
Section
Pages
Revision
Section 0
2, 3, 5, 6, 8 thru 11
Rev 0
12
Rev 4
1, 4, 7
Rev 5
Section 1
1 thru 18
Rev 0
Section 2
1 thru 10, 13 thru 32
Rev 0
11,12
Rev 5
Section 3
1 thru 58
Rev 0
Section 4
1, 2, 5 thru 10, 12 thru 15, 18, 21,
23, 24, 26 thru 30
Rev 0
4
Rev 2
3, 11, 16, 17, 20, 25
Rev 4
19, 22
Rev 5
Section 5
1 thru 15,17 thru 22
Rev 0
16
Rev 2
Section 6
1 thru 10, 14
Rev 0
11 thru 13
Rev 5
Section 7
1 thru 44
Rev 0
Section 8
1 thru 10
Rev 0
Section 9
1 thru 8
Rev 5
Supplements LOEP: make reference to the Supplements Cover Pages

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Aircraft Flight Manual
FOREWORD
3. FOREWORD
Tecnam P2006T is a twin-engine four-seat aircraft with high cantilevered wing and tri-
cycle retractable landing gear.
Section 1 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:
COSTRUZIONI AERONAUTICHE TECNAM s.r.l.
Via MAIORISE
CAPUA (CE) - ITALY
 +39 (0) 823.62.01.34  www.tecnam.com

4th Edition - Rev. 0
Aircraft Flight Manual
SECTIONS LIST
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4. SECTIONS LIST
General
Section 1 (a non-approved Chapter)
Limitations
Section 2 - EASA Approved Chapter
Emergency Procedures
Section 3 (a non-approved Chapter)
Normal Procedures
Section 4 (a non-approved Chapter)
Performances
Section 5 (a non-approved Chapter)
Weight and Balance
Section 6 (a non-approved Chapter)
Airframe and Systems description
Section 7 (a non-approved Chapter)
Airplane Care and Maintenance
Section 8 (a non-approved Chapter)
Supplements
Section 9 (*)
(*) EASA approved parts, if any, are reported on the supplements

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Section 1 –General
INDEX
4th Edition, Rev 0
SECTION 1 - GENERAL
INDEX
1. Introduction .................................................................................. 3
2. Three-view and dimensions.......................................................... 4
3. Control Surfaces Travel Limits .................................................... 6
4. Engine ........................................................................................... 6
5. Propeller ....................................................................................... 6
6. Governor ....................................................................................... 7
7. Fuel ............................................................................................... 7
8. Lubrication.................................................................................... 7
9. Cooling .......................................................................................... 8
10. Maximum weights...................................................................... 8
11. Standard weights....................................................................... 8
12. Specific loadings ....................................................................... 8
13. Acronyms and terminology...................................................... 10
14. Unit conversion chart .............................................................. 15
15. Litres / US gallons conversion chart ....................................... 16

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Section 1 –General
4th Edition, Rev 0
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Section 1 –General
INTRODUCTION
4th Edition, Rev 0
1. INTRODUCTION
The Aircraft Flight Manual has been implemented to provide the owners with in-
formation for a safe and efficient use of the aircraft TECNAM P2006T.
Warning –Caution –Note
Following definitions apply to warnings, cautions and notes used in the Aircraft
Flight Manual.
WARNING
The non-observation of the corresponding procedure can lead, as
immediate effect, to a significant reduction of the flight safety.
CAUTION
The non-observation of the corresponding procedure can lead to
an equipment damage which leads to a reduction of the flight safe-
ty in a short or longer time interval.
Draws the attention to a procedure not directly related to safety of
flight.
.
NOTE

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Section 1 –General
THREE-VIEW AND DIMENSIONS
4th Edition, Rev 0
2. THREE-VIEW AND DIMENSIONS
P2006 T
GENERAL VIEW
Figure 1 – General views

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Section 1 –General
THREE-VIEW AND DIMENSIONS
4th Edition, Rev 0
Dimensions
Overall dimensions
Wingspan 11,4 m 37,4 ft
Length 8,7 m 28,5 ft
Overall height 2,58 m 8,46 ft
Wing
Wing surface 14,76 m2 158,9 ft2
Mean Geometric Chord 1,295 m 4,25 ft
Dihedral 1°
Aspect ratio 8,80
Main Landing Gear
Track 2.0 m
Wheelbase 2.9 m
Tire 6.00-6
Wheel rim assembly (Cleveland) P/N 40-59A
Nose Landing Gear
Tire 5.00 – 5
Wheel rim assembly (Cleveland) P/N 40-77C

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Section 1 –General
GENERAL FEATURES
4th Edition, Rev 0
3. CONTROL SURFACES TRAVEL LIMITS
Ailerons
Up 20° Down 17 ° ( 2°)
Stabilator (refer to Trailing Edge)
Up 4° Down 15° ( 2°)
Stabilator trim tab (refer to Trailing Edge)
Up 2°; Down 19° ( 2°)
Rudder
RH 26° LH 26° ( 2°)
Rudder trim tab
RH 20° LH 20° ( 2°)
Flaps
0°; 40° (- 2°)
4. ENGINE
Manufacturer
Bombardier-Rotax GmbH
Model
912 S3
Certification basis
FAR 33 - Amendment 15
Type Certificate
EASA TCDS no. E.121 dated 1 April
2008
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)
5. PROPELLER
Manufacturer
MT Propeller
Type Certificate
LBA 32.130/086 (MTV-21 series)
Model
MTV-21-A-C-F/CF178-05
Blades/hub
2 wood/composite blades – aluminum
hub
Diameter
1780 mm (no reduction allowed)
Type
Variable pitch - hydraulically controlled

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Section 1 –General
GENERAL FEATURES
4th Edition, Rev 0
6. GOVERNOR
Manufacturer
Mt Propeller
Model
P-875-12
Type
Hydraulic
7. FUEL
Approved fuel: MOGAS ASTM D4814
MOGAS EN 228 Super/Super plus
(min. RON 95)
AVGAS 100LL (ASTM D910)
(see also Section 2)
Fuel tanks
Two integrated tanks (one in each
wing) fitted with drainable sump
and drain valve
Capacity of each wing tan
100 litres (26,42 US gallons)
Tanks overall capacity
200 litres (52,8 US gallons)
Overall usable fuel
194.4 litres (51,35 US gallons)
Overall unusable fuel
5.6 litres (1,48 US gallons)
8. LUBRICATION
Lubrication system
Forced type with external reservoir
Oil
Use only oil with API classification “SG”
or higher. For additional info, refer to “Ro-
tax Operators Manual” – last issue -, “Op-
erating Media” Section.
Oil capacity
Max. 3.0 litres – min. 2.0 litres (per
tank)

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Section 1 –General
GENERAL FEATURES
4th Edition, Rev 0
9. COOLING
Cooling system
Ram-air cooled cylinders, liquid
cooled cylinder heads (closed and
pressurized circuit)
Coolant liquid
Certified for Water/Coolant mixture.
Make reference to “Rotax Operators
Manual” – last issue
Overall circuit capacity
1410 cm3
10. WEIGHTS
See Section 2.
11. STANDARD WEIGHTS
Empty Weight: see weighing record on Section 6
12. SPECIFIC LOADINGS
NOTE. Reference is made to both MTOW: 1180 kg and 1230 kg (if Supplement
A19 or G10 - Increased MTOW @1230 KG - is applicable).
MTOW 1180 kg (2601 lb)
MTOW 1230 kg (2712 lb)
Wing Loading
80 kg/m2 (16,37 lb/sqft )
83 kg/m2 (17,1 lb/sqft )
Power Loading
6.0 kg/hp (13,26 lb/hp )
6.28 kg/hp (13,84 lb/hp )