P2006T - Tecnam.com
P2006T - Tecnam.com
P2006T - Tecnam.com
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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)
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