P2006T - Tecnam.com

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