P2006T - Tecnam.com

Courtesy Translation
INTERSTATE AVIATION COMMITTEE
AVIATION REGISTER
DATA SHEET
Type Certificate № CT319-P2006T
with Supplements №№ CT 319-P2006T/Д01,
CT 319-P2006T/Д02
Issue 07
27 th March 2014
Aircraft
Model P2006T
Type Certificate Holder:
Costruzioni Aeronautiche TECNAM S.r.l.
Via Tasso, 478
80127 Napoli, Italia
This data sheet which is the integral part of Type Certificate № CT319-P2006T defines Type Design and
prescribes conditions and limitations under which the product for which Type Certificate was issued meets airworthiness
requirements of Certification Basis, prescribed in paragraph 20 of this TCDS.
List of effective pages:
Page 1 2 3 4 5 6
Issue 06 06 06 06 07 06

Type Certificate Data Sheet № CT319-P2006T Issue 07, 27 th March 2014 Page. 2/6
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CONTENTS
Page
Model P2006T
1. Developer and Manufacturer 3
2. Brief aircraft description 3
3. Type Design
3
Definition
4. Engine 3
4.1. Engine Limitations 3
5. Propeller 3
5.1. Propeller Limitations 3
6. Approved types of fuel 3
7. Quantity of fuel 3
8. Quantity of oil 3
9. Minimum crew 3
10. Maximum occupants on board 3
11. Maximum weight 4
12. Maximum baggage weight 4
13. C.G. Range 4
14. Maximum operational altitude 4
15. Airspeed Limits 4
16. Airworthiness limits 5
17. Required equipment 5
18. Noise levels 5
19. Operational Limitations 5
20. Certification Basis 5
21. Supplements to Type Certificate № CT 319-P2006T 6
22. STC (Supplemental Type Certificate) approved by IAC AR 6
23. Notes 6

Type Certificate Data Sheet № CT319-P2006T Issue 07, 27 th March 2014 Page. 3/6
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Model P2006T
1. Developer and
Manufacturer
2. Brief aircraft
description
3. Type Design
Definition
Costruzioni Aeronautiche TECNAM S.r.l.
Via Tasso, 478
80127 Napoli
ITALIA
Normal category aircraft
Type Design is defined by:
а) basic design which is in compliance with Type Certificate № А.185, issued by
EASA, specified by Type Design Definition Doc. 2006/004, with installation of
the additional equipment according to SB 032-CS (aircraft with analog
instruments) and SB 033-CS (aircraft with GARMIN G950 EFDS)
b) operational documentation:
• Airplane Flight Manual (AFM) approved by EASA, Doc. 2006/044 with
“Supplement A16 for CIS countries operators” (aircraft with analog
instruments) or with “Supplement G7 for CIS countries operators” (for aircraft
with GARMIN G950 EFDS);
• Airplane Maintenance Manual (AMM) Doc. № 2006/045 with Section B,
Subsection 4 “Airworthiness Limitations”, approved by EASA
4. Engine Two BRP-Powertrain GmbH & Co. KG (Austria) piston engines model 912 S3
IAC AR Type Certificate № CT313-АМД dated 03 June 2010
4.1 Engine Limitations Established max power in MCA conditions on sea level: 73,5 kW (100 h.p.)
Other engine limitations are stated in the EASA approved Airplane Flight Manual,
Doc. No. 2006/044 and in the Type Certificate Data Sheet No. CT 313-АМД, Issue
01 and subsequent
5. Propeller Two MT-Propeller GmbH (Germany) MTV-21-A-C-F/CF178-05
IAC AR Type Certificate № СТ317-ВВ dated 20 September 2010
5.1. Propeller
Limitations
6. Approved types of
fuel
MTV-21-A-C-F/CF178-05 propeller limitations are stated in the EASA approved
Airplane Flight Manual, Doc. No. 2006/044 and in the Type Certificate Data Sheet
No. CT 317-BB, Issue 01 and subsequent
AVGAS 100LL (ASTM D910)
See EASA approved AFM Doc. No. 2006/044 for other approved fuel grades
7. Quantity of fuel Two wing fuel tanks: total volume 200 liter
unusable fuel 5.6 liter
8. Quantity of oil See the EASA approved Airplane Flight Manual, Doc. No. 2006/044
9. Minimum crew 1 pilot
10. Maximum
occupants on board
4 (including crew)

Type Certificate Data Sheet № CT319-P2006T Issue 07, 27 th March 2014 Page. 4/6
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11. Maximum weight Max. take off weight 1180 kg (2600 lb)
Max. zero fuel weight
1145 kg (2524 lb)
Max. landing weight
1180 kg (2600 lb)
With embodied modification MOD 2006/015 “Increment of the maximum take off
weight (1230 kg)”:
Max. take off weight
Max. zero fuel weight
Max. landing weight
1230 kg (2712 lb)
1195 kg (2635 lb)
1230 kg (2712 lb)
12. Maximum
baggage weight
80 kg (176 lb)
13. C.G. Range See the EASA approved AFM, Doc. No. 2006/044
14. Maximum
operational altitude
15. Airspeed Limits
3600 m
Conditions of flights on altitudes higher than 3000 m are specified in the
“Supplement A16 for CIS countries operators” (aircraft with analog instruments)
or in the “Supplement G7 for CIS countries operators” (aircraft with GARMIN
G950 EFDS)
KIAS
Max maneuvering speed, V A
Max speed with flaps extended, V FE:
T.O. position
LDG position (FULL)
Max landing gear operating speed, V LO: 93
Max speed with landing gear extended V LE:
93
Max cruise speed, V NO:
119
119
93
135
Never exceed speed, V NE: 167
With embodied modification MOD 2006/015 “Increment of the maximum
take off weight (1230 Kg)”:
Max maneuvering speed, V A
Max speed with flaps extended, V FE:
T.O. position
LDG position (FULL)
KIAS
Max landing gear operating speed, V LO: 93
Max speed with landing gear extended V LE:
93
122
122
93
Max cruise speed, V NO:
138
Never exceed speed, V NE:
171
With embodied modification MOD 2006/033 “V LE and V LO Increment”:
KIAS
Max landing gear operating speed, V LO: 122
Max speed with landing gear extended V LE: 122

Type Certificate Data Sheet № CT319-P2006T Issue 07, 27 th March 2014 Page. 5/6
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16. Airworthiness
limits
17. Required
equipment
Life time limits and other airworthiness limitations are contained in Section B,
Subsection 4: “Airworthiness Limitations” Maintenance Manual, approved by
EASA (AMM Doc. No. 2006/045).
1. In addition to the standard equipment list approved by EASA, the following
equipment must be installed on aircraft:
ADF;
Side-slip indicator (for airplanes with GARMIN G950 EFDS);
Emergency radio operating on 121,5 MHz and located so to be easily
accessible and removable in case of emergency landing. Availability and
installation of emergency radio on board is the responsibility of Operator.
2. All markings and instructions related to emergency equipment, except for
illuminated “EXIT” sign must be written in the language of the State of Operator
and in English language.
18. Noise levels Airplane is approved for compliance with Aviation Regulations, Part 36 (AP-36)
“Aircraft Noise Certification”, Chapter F, Issue 2, and ICAO Annex 16 standards,
Volume 1 “Aviation Noise”, Chapter 10:
Engine Propeller Max. take-off
weight, kg
Rotax 912 S3
Rotax 912 S3
MTV-21-A-C-
F/CF178-05
MTV-21-A-C-
F/CF178-05
Measured
noise level,
dBA
Limit noise
level, dBA
1180 67,07 85,6
1230 72,82 86,2
19. Operational
Limitations
20. Certification
Basis
1. Aircraft is not approved for flights in icing conditions.
2. Day and night IFR and VFR flights are allowed.
3. Cat. I ILS ICAO approaches are allowed in case installation of Fifty Five
X Autopilot is provided.
4. Aircraft operation is allowed at ambient air temperature near the ground
not lower than minus 25°C and not higher than +40°C.
5. Maximum airdrome elevation is 2400 m (8000 ft) pressure altitude.
6. Aircraft can be operated from dry or wet paved airfield, and from
unpaved runway with soil strength not less than 6 kg/cm 2 .
7. Flights over vast water areas are forbidden.
Other limitations are given in the EASA approved AFM, Doc. No.
2006/044 with “Supplement A16 for CIS countries operators” (aircraft
with analog instruments) or in the “Supplement G7 for CIS countries
operators” (aircraft with GARMIN G950 EFDS)
1. Airworthiness Requirements:
Aviation Regulations, Part 23 (AP-23) “Civil light aircraft airworthiness
regulations” through Amendment 4, paragraphs 23.1457 and 25.1459 through
Amendment 5, also Special technical conditions and equivalent safety findings
accepted by EASA and introduced in TCDS of TC № A.185 EASA.
2. Environmental requirements:
Aviation Regulation, Part 36 (AP-36) Chapter F, Issue 2, “Aircraft Noise
Certification” and Annex 16 ICAO, Volume 1 “Aviation Noise”, Chapter 10

Type Certificate Data Sheet № CT319-P2006T Issue 07, 27 th March 2014 Page. 6/6
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21. Supplements to Type Certificate № CT 319-P2006T:
Supplements to Type
Description of Type Design Change
Certificate № CT 319-P2006T
CT 319-P2006T/Д01 1. EASA Major Change Approval № 10037759 MOD 2006/015 “Increment of
the maximum take off weight (1230 Kg)”;
2. EASA Major Change Approval № 10037760 MOD 2006/121 “New Landing
Gear Emergency Accumulator”.
CT 319-P2006T/Д02 1. EASA Major Change Approval № 10041602 MOD 2006/033 “V LE and V LO
Increment”
22. STC (Supplemental Type Certificate) approved by IAC AR.
№№ STC Denomination STC Holder STC Number Note
1 Provisions for surveillance configuration Airborne Technologies 10034631 (1)
GmbH
(1) Foto equipment and its installation were not addressed in the framework of P2006T aircraft certification.
Passenger transportation is forbidden in case STC 10034631 is incorporated.
23. Notes 1. Aircraft Type Design does not provide installation of Flight Data Recorder
(FDR) and Cockpit Voice Recorder (CVR).
(Original document in Russian language signed by)
Evgeny Konyukhov
Chief, Small Airplanes Branch
***