P2006T - Tecnam.com
P2006T - Tecnam.com
P2006T - Tecnam.com
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Courtesy Translation<br />
INTERSTATE AVIATION COMMITTEE<br />
AVIATION REGISTER<br />
DATA SHEET<br />
Type Certificate № CT319-<strong>P2006T</strong><br />
with Supplements №№ CT 319-<strong>P2006T</strong>/Д01,<br />
CT 319-<strong>P2006T</strong>/Д02<br />
Issue 07<br />
27 th March 2014<br />
Aircraft<br />
Model <strong>P2006T</strong><br />
Type Certificate Holder:<br />
Costruzioni Aeronautiche TECNAM S.r.l.<br />
Via Tasso, 478<br />
80127 Napoli, Italia<br />
This data sheet which is the integral part of Type Certificate № CT319-<strong>P2006T</strong> defines Type Design and<br />
prescribes conditions and limitations under which the product for which Type Certificate was issued meets airworthiness<br />
requirements of Certification Basis, prescribed in paragraph 20 of this TCDS.<br />
List of effective pages:<br />
Page 1 2 3 4 5 6<br />
Issue 06 06 06 06 07 06
Type Certificate Data Sheet № CT319-<strong>P2006T</strong> Issue 07, 27 th March 2014 Page. 2/6<br />
_____________________________________________________________________________________________<br />
CONTENTS<br />
Page<br />
Model <strong>P2006T</strong><br />
1. Developer and Manufacturer 3<br />
2. Brief aircraft description 3<br />
3. Type Design<br />
3<br />
Definition<br />
4. Engine 3<br />
4.1. Engine Limitations 3<br />
5. Propeller 3<br />
5.1. Propeller Limitations 3<br />
6. Approved types of fuel 3<br />
7. Quantity of fuel 3<br />
8. Quantity of oil 3<br />
9. Minimum crew 3<br />
10. Maximum occupants on board 3<br />
11. Maximum weight 4<br />
12. Maximum baggage weight 4<br />
13. C.G. Range 4<br />
14. Maximum operational altitude 4<br />
15. Airspeed Limits 4<br />
16. Airworthiness limits 5<br />
17. Required equipment 5<br />
18. Noise levels 5<br />
19. Operational Limitations 5<br />
20. Certification Basis 5<br />
21. Supplements to Type Certificate № CT 319-<strong>P2006T</strong> 6<br />
22. STC (Supplemental Type Certificate) approved by IAC AR 6<br />
23. Notes 6
Type Certificate Data Sheet № CT319-<strong>P2006T</strong> Issue 07, 27 th March 2014 Page. 3/6<br />
_____________________________________________________________________________________________<br />
Model <strong>P2006T</strong><br />
1. Developer and<br />
Manufacturer<br />
2. Brief aircraft<br />
description<br />
3. Type Design<br />
Definition<br />
Costruzioni Aeronautiche TECNAM S.r.l.<br />
Via Tasso, 478<br />
80127 Napoli<br />
ITALIA<br />
Normal category aircraft<br />
Type Design is defined by:<br />
а) basic design which is in <strong>com</strong>pliance with Type Certificate № А.185, issued by<br />
EASA, specified by Type Design Definition Doc. 2006/004, with installation of<br />
the additional equipment according to SB 032-CS (aircraft with analog<br />
instruments) and SB 033-CS (aircraft with GARMIN G950 EFDS)<br />
b) operational documentation:<br />
• Airplane Flight Manual (AFM) approved by EASA, Doc. 2006/044 with<br />
“Supplement A16 for CIS countries operators” (aircraft with analog<br />
instruments) or with “Supplement G7 for CIS countries operators” (for aircraft<br />
with GARMIN G950 EFDS);<br />
• Airplane Maintenance Manual (AMM) Doc. № 2006/045 with Section B,<br />
Subsection 4 “Airworthiness Limitations”, approved by EASA<br />
4. Engine Two BRP-Powertrain GmbH & Co. KG (Austria) piston engines model 912 S3<br />
IAC AR Type Certificate № CT313-АМД dated 03 June 2010<br />
4.1 Engine Limitations Established max power in MCA conditions on sea level: 73,5 kW (100 h.p.)<br />
Other engine limitations are stated in the EASA approved Airplane Flight Manual,<br />
Doc. No. 2006/044 and in the Type Certificate Data Sheet No. CT 313-АМД, Issue<br />
01 and subsequent<br />
5. Propeller Two MT-Propeller GmbH (Germany) MTV-21-A-C-F/CF178-05<br />
IAC AR Type Certificate № СТ317-ВВ dated 20 September 2010<br />
5.1. Propeller<br />
Limitations<br />
6. Approved types of<br />
fuel<br />
MTV-21-A-C-F/CF178-05 propeller limitations are stated in the EASA approved<br />
Airplane Flight Manual, Doc. No. 2006/044 and in the Type Certificate Data Sheet<br />
No. CT 317-BB, Issue 01 and subsequent<br />
AVGAS 100LL (ASTM D910)<br />
See EASA approved AFM Doc. No. 2006/044 for other approved fuel grades<br />
7. Quantity of fuel Two wing fuel tanks: total volume 200 liter<br />
unusable fuel 5.6 liter<br />
8. Quantity of oil See the EASA approved Airplane Flight Manual, Doc. No. 2006/044<br />
9. Minimum crew 1 pilot<br />
10. Maximum<br />
occupants on board<br />
4 (including crew)
Type Certificate Data Sheet № CT319-<strong>P2006T</strong> Issue 07, 27 th March 2014 Page. 4/6<br />
_____________________________________________________________________________________________<br />
11. Maximum weight Max. take off weight 1180 kg (2600 lb)<br />
Max. zero fuel weight<br />
1145 kg (2524 lb)<br />
Max. landing weight<br />
1180 kg (2600 lb)<br />
With embodied modification MOD 2006/015 “Increment of the maximum take off<br />
weight (1230 kg)”:<br />
Max. take off weight<br />
Max. zero fuel weight<br />
Max. landing weight<br />
1230 kg (2712 lb)<br />
1195 kg (2635 lb)<br />
1230 kg (2712 lb)<br />
12. Maximum<br />
baggage weight<br />
80 kg (176 lb)<br />
13. C.G. Range See the EASA approved AFM, Doc. No. 2006/044<br />
14. Maximum<br />
operational altitude<br />
15. Airspeed Limits<br />
3600 m<br />
Conditions of flights on altitudes higher than 3000 m are specified in the<br />
“Supplement A16 for CIS countries operators” (aircraft with analog instruments)<br />
or in the “Supplement G7 for CIS countries operators” (aircraft with GARMIN<br />
G950 EFDS)<br />
KIAS<br />
Max maneuvering speed, V A<br />
Max speed with flaps extended, V FE:<br />
T.O. position<br />
LDG position (FULL)<br />
Max landing gear operating speed, V LO: 93<br />
Max speed with landing gear extended V LE:<br />
93<br />
Max cruise speed, V NO:<br />
119<br />
119<br />
93<br />
135<br />
Never exceed speed, V NE: 167<br />
With embodied modification MOD 2006/015 “Increment of the maximum<br />
take off weight (1230 Kg)”:<br />
Max maneuvering speed, V A<br />
Max speed with flaps extended, V FE:<br />
T.O. position<br />
LDG position (FULL)<br />
KIAS<br />
Max landing gear operating speed, V LO: 93<br />
Max speed with landing gear extended V LE:<br />
93<br />
122<br />
122<br />
93<br />
Max cruise speed, V NO:<br />
138<br />
Never exceed speed, V NE:<br />
171<br />
With embodied modification MOD 2006/033 “V LE and V LO Increment”:<br />
KIAS<br />
Max landing gear operating speed, V LO: 122<br />
Max speed with landing gear extended V LE: 122
Type Certificate Data Sheet № CT319-<strong>P2006T</strong> Issue 07, 27 th March 2014 Page. 5/6<br />
_____________________________________________________________________________________________<br />
16. Airworthiness<br />
limits<br />
17. Required<br />
equipment<br />
Life time limits and other airworthiness limitations are contained in Section B,<br />
Subsection 4: “Airworthiness Limitations” Maintenance Manual, approved by<br />
EASA (AMM Doc. No. 2006/045).<br />
1. In addition to the standard equipment list approved by EASA, the following<br />
equipment must be installed on aircraft:<br />
ADF;<br />
Side-slip indicator (for airplanes with GARMIN G950 EFDS);<br />
Emergency radio operating on 121,5 MHz and located so to be easily<br />
accessible and removable in case of emergency landing. Availability and<br />
installation of emergency radio on board is the responsibility of Operator.<br />
2. All markings and instructions related to emergency equipment, except for<br />
illuminated “EXIT” sign must be written in the language of the State of Operator<br />
and in English language.<br />
18. Noise levels Airplane is approved for <strong>com</strong>pliance with Aviation Regulations, Part 36 (AP-36)<br />
“Aircraft Noise Certification”, Chapter F, Issue 2, and ICAO Annex 16 standards,<br />
Volume 1 “Aviation Noise”, Chapter 10:<br />
Engine Propeller Max. take-off<br />
weight, kg<br />
Rotax 912 S3<br />
Rotax 912 S3<br />
MTV-21-A-C-<br />
F/CF178-05<br />
MTV-21-A-C-<br />
F/CF178-05<br />
Measured<br />
noise level,<br />
dBA<br />
Limit noise<br />
level, dBA<br />
1180 67,07 85,6<br />
1230 72,82 86,2<br />
19. Operational<br />
Limitations<br />
20. Certification<br />
Basis<br />
1. Aircraft is not approved for flights in icing conditions.<br />
2. Day and night IFR and VFR flights are allowed.<br />
3. Cat. I ILS ICAO approaches are allowed in case installation of Fifty Five<br />
X Autopilot is provided.<br />
4. Aircraft operation is allowed at ambient air temperature near the ground<br />
not lower than minus 25°C and not higher than +40°C.<br />
5. Maximum airdrome elevation is 2400 m (8000 ft) pressure altitude.<br />
6. Aircraft can be operated from dry or wet paved airfield, and from<br />
unpaved runway with soil strength not less than 6 kg/cm 2 .<br />
7. Flights over vast water areas are forbidden.<br />
Other limitations are given in the EASA approved AFM, Doc. No.<br />
2006/044 with “Supplement A16 for CIS countries operators” (aircraft<br />
with analog instruments) or in the “Supplement G7 for CIS countries<br />
operators” (aircraft with GARMIN G950 EFDS)<br />
1. Airworthiness Requirements:<br />
Aviation Regulations, Part 23 (AP-23) “Civil light aircraft airworthiness<br />
regulations” through Amendment 4, paragraphs 23.1457 and 25.1459 through<br />
Amendment 5, also Special technical conditions and equivalent safety findings<br />
accepted by EASA and introduced in TCDS of TC № A.185 EASA.<br />
2. Environmental requirements:<br />
Aviation Regulation, Part 36 (AP-36) Chapter F, Issue 2, “Aircraft Noise<br />
Certification” and Annex 16 ICAO, Volume 1 “Aviation Noise”, Chapter 10
Type Certificate Data Sheet № CT319-<strong>P2006T</strong> Issue 07, 27 th March 2014 Page. 6/6<br />
_____________________________________________________________________________________________<br />
21. Supplements to Type Certificate № CT 319-<strong>P2006T</strong>:<br />
Supplements to Type<br />
Description of Type Design Change<br />
Certificate № CT 319-<strong>P2006T</strong><br />
CT 319-<strong>P2006T</strong>/Д01 1. EASA Major Change Approval № 10037759 MOD 2006/015 “Increment of<br />
the maximum take off weight (1230 Kg)”;<br />
2. EASA Major Change Approval № 10037760 MOD 2006/121 “New Landing<br />
Gear Emergency Accumulator”.<br />
CT 319-<strong>P2006T</strong>/Д02 1. EASA Major Change Approval № 10041602 MOD 2006/033 “V LE and V LO<br />
Increment”<br />
22. STC (Supplemental Type Certificate) approved by IAC AR.<br />
№№ STC Denomination STC Holder STC Number Note<br />
1 Provisions for surveillance configuration Airborne Technologies 10034631 (1)<br />
GmbH<br />
(1) Foto equipment and its installation were not addressed in the framework of <strong>P2006T</strong> aircraft certification.<br />
Passenger transportation is forbidden in case STC 10034631 is incorporated.<br />
23. Notes 1. Aircraft Type Design does not provide installation of Flight Data Recorder<br />
(FDR) and Cockpit Voice Recorder (CVR).<br />
(Original document in Russian language signed by)<br />
Evgeny Konyukhov<br />
Chief, Small Airplanes Branch<br />
***