Type Certificate Data Sheet EASA A.185 P2006T
TECNAM P-2006T · Pilot's Operating Handbook
Overview
This document is the Type Certificate Data Sheet for the Tecnam P-2006T, issued by the European Aviation Safety Agency (EASA). It provides essential information regarding the aircraft's certification, technical characteristics, operational limitations, and maintenance instructions.
- The Tecnam P-2006T is a twin-engine, four-seated aircraft.
- It features a cantilever high wing design and retractable tricycle landing gear.
- The aircraft is certified under EASA CS-23 Normal Category.
- Maximum take-off weight is 1180 kg (2600 lb), with an option for 1230 kg (2712 lb) under certain conditions.
- The aircraft has a maximum speed of 167 KIAS (Never Exceed Speed).
- It is certified for VFR Day, VFR Night, and IFR operations.
- The aircraft uses Bombardier-Rotax GmbH 912 S3 engines.
- Fuel capacity is 200 liters (52.8 US Gallon), with 194.4 liters (51.4 US Gallon) usable.
Document
Source
Originally published by tecnam.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Year ·
- 2013
- File size ·
- 3.6 MB
- Publisher ·
- tecnam.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Span m ·
- 11.4
- Height m ·
- 2.85
- Length m ·
- 8.7
- Wing area m2 ·
- 14.76
- Usable fuel l ·
- 194.4
- Oil capacity l ·
- 3.0
- Fuel capacity l ·
- 200
Performance
- Max speed kias ·
- 167
- Design manoeuvring speed kias ·
- 119
- Max landing gear extended speed kias ·
- 93
- Max landing gear operation speed kias ·
- 93
V-speeds
- VA_KIAS ·
- 119
- VFE_KIAS ·
- 93
- VLE_KIAS ·
- 93
- VLO_KIAS ·
- 93
- VMC_KIAS ·
- 62
- VNE_KIAS ·
- 167
- VNO_KIAS ·
- 135
Weight & balance
- Zero fuel kg ·
- 1145
- Max takeoff kg ·
- 1180
- Cg rear limit m ·
- 0.415
- Landing weight kg ·
- 1180
- Cg forward limit m ·
- 0.221
What is the Type Certificate Data Sheet EASA A.185 P2006T?
The Type Certificate Data Sheet EASA A.185 P2006T is a pilot's operating handbook for the TECNAM P-2006T, dated 2013.
Where does the Type Certificate Data Sheet EASA A.185 P2006T come from?
This copy of the Type Certificate Data Sheet EASA A.185 P2006T was originally published by tecnam.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the Type Certificate Data Sheet EASA A.185 P2006T published?
The Type Certificate Data Sheet EASA A.185 P2006T — the TECNAM P-2006T pilot's operating handbook on file — is dated 2013.
Most owners only have the POH. Here's the essential set for the TECNAM P-2006T.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P-2006Tmanuals & documents
- SPECTRUM AIRWAYS TECNAM P2006T NORMAL PROCEDURESChecklist
- CHECK LISTChecklist
- TECNAM P2006T CHECK LISTChecklist
- Aircraft Flight ManualPilot's Operating Handbook
- Normal Check List P2006TChecklist
- Aircraft Flight ManualPilot's Operating Handbook
- P2006T Specification and DescriptionPilot's Operating Handbook
In this document
General Information
The Tecnam P-2006T is a twin-engine aircraft with a certification basis under EASA CS-23. It was certified on June 5, 2009.
Technical Characteristics
The aircraft has a wingspan of 11.4 m, a length of 8.7 m, and a height of 2.85 m. It is constructed of aluminum.
Operational Limitations
The aircraft is prohibited from flying into expected or actual icing conditions. It has specific airspeed limitations for various operations.
Weight and Balance
The maximum take-off weight is 1180 kg, with a zero fuel weight of 1145 kg. The center of gravity limits are defined.
Operating Instructions
The document references the Aircraft Flight Manual and other maintenance documents necessary for operation and airworthiness.
Administrative Information
The document includes a change record detailing updates and amendments to the Type Certificate Data Sheet.
Safety notes
- Flight into expected or actual icing conditions is prohibited.
- Refer to the Aircraft Flight Manual for detailed operating instructions.
- Ensure compliance with airworthiness limitations as specified in the maintenance manual.
Full document text
TCDS A.185 P2006T Page 1 of 9 Issue 04, 21 November 2013 EASA Form NR 90 Issue 01 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.185 P2006T Type Certificate Holder Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA Issue 4: 21 November 2013 TCDS A.185 P2006T Page 2 of 9 Issue 04, 21 November 2013 CONTENT SECTION A: P2006T A.I. General A.II. Certification Basis A.III. Technical Characteristics and Operational Limitations A.IV. Operating and Service Instructions A.V. Notes ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record III. Change Record TCDS A.185 P2006T Page 3 of 9 Issue 04, 21 November 2013 SECTION A: P2006T A.I. General Data Sheet No.: EASA A.185 Issue: 04 Date: 21 November 2013 1. a) Type: P2006T c) Model: ------ b) Variant: ------ 2. Airworthiness Category: CS-23 Normal Category 3. Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA 4. Manufacturer: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA 5. Certification Application Date: 12 December 2005 6. EASA Type Certification Date: 5 June 2009 A.II. EASA Certification Basis 1. Reference Date for determining the applicable requirements: 12 December 2006 2. Reserved 3. Reserved 4. Certification Basis: As defined in CRI A-01, latest issue See Note 2 5. Airworthiness Requirements: EASA CS-23 (Decision no. 2003/14/RM of the Executive Director of the Agency of 14 November 2003) 6. Requirements elected to comply: None 7. EASA Special Conditions: CRI F-01, HIRF Protection See Note 2 8. Exemptions: None 9. Equivalent Safety Findings: CS23.807(e) Ditching Emergency Exits (CRI D-01); CS23.783(b), Main door (CRI D-02); CS23.865, Fire protection of flight controls, engine mounts and other flight structure (CRI D-03); CS23.1061(b), CS23.1063, Liquid Cooling – Coolant tank (CRI E-01). TCDS A.185 P2006T Page 4 of 9 Issue 04, 21 November 2013 10. EASA Environmental Standards: ICAO, Annex 16, Volume I, 4th Edition, July 2005; EASA CS-36, Decision No. 2003/4/RM, 17 October 2003 A.III. Technical Characteristics and Operational Limitations 1. Type Design Definition: C.A. Tecnam Aircraft P2006T report “Type design definition” No. 2006/004 1st ed. Rev 2 dated May 25th 2009. 2. Description: Twin engine, four-seated cantilever high wing airplane, aluminium construction, retractable tricycle landing gear. 3. Equipment: Equipment list, AFM, Doc. 2006/044, Section 6, 4. Dimensions: Span 11.4 m (37.4 ft) Length 8.7 m (28.5 ft) Height 2.85 m (9.35 ft) Wing Area 14.76 m² (158.9 sqft) 5. Engines: No.2 Bombardier-Rotax GmbH 912 S3 Certification Basis: FAR 33 Amdt. 15 plus FAA NPRM Doc. # 24922, Notice no. 92-14 EASA TCDS n° E.121 dated 1 April 2008 5.1 Engine Limits: Max rotational speed (5 min) 5800 r.p.m. Max continuous rotational speed 5500 r.p.m (Engine shaft r.p.m) Powerplant limits, AFM, Doc. 2006/044, Section 2, 6. Reserved 7. Propeller: No.2 MT Propeller MTV-21-A-C-F/CF178-05 Two blades, constant speed, variable pitch with feathering capability, wood construction. Type Certificate No. LBA 32.130/086 Diameter : 1780 mm 8. Fluids: 8.1 Fuel: - MOGAS (Min. RON 95/AKI 91) EN 228 Super EN 228 Super Plus ASTM D4814 - AVGAS 100LL (ASTM D910) (see Rotax Operator’s Manual OM-912) 8.2 Oil: Lubricant specifications and grade are detailed into the “Rotax Operator’s Manual OM-912” and in its related documents. 8.3 Coolant: Water / Cooler Protection For more details see AFM, 2006/044, Section 2 TCDS A.185 P2006T Page 5 of 9 Issue 04, 21 November 2013 9. Fluid capacities: 9.1 Fuel: Total: 200 liters (52.8 US Gallon) Usable: 194.4 liters (51.4 US Gallon) 9.2 Oil (each engine): Maximum: 3.0 liters (3.2 qts) Minimum: 2.0 liters (2.1 qts) 10. Air Speeds: Design Manoeuvring Speed VA:119 KIAS (117 KCAS) Flap Extended Speed VFE: 93 KIAS (92 KCAS) Landing 119 KIAS (117 KCAS) Take Off Minimum Control Speed VMC 62 KIAS (62 KCAS) Maximum Landing Gear Operation Speed VLO: 93 KIAS (92 KCAS) Maximum Landing Gear Extended Speed VLE: 93 KIAS (92 KCAS) Maximum Structural Cruising Speed VNO: 135 KIAS (134 KCAS) Never Exceed Speed VNE: 167 KIAS (168 KCAS) The following values apply when EASA Major Change Approval n. 10037759 “Increment of the maximum take off weight (1230 Kg)” as per C.A. Tecnam MOD2006/015 is installed (Other Air Speeds remain unchanged): Design Manoeuvring Speed VA:122 KIAS (119KCAS) Flap Extended Speed VFE: 93 KIAS (93 KCAS) Landing 122 KIAS (119 KCAS)Take Off Maximum Structural Cruising Speed VNO: 138 KIAS (136 KCAS) Never Exceed Speed VNE: 171 KIAS (172 KCAS) The following values apply when EASA Major Change Approval n. 10041602 “VLE and VLO increment” as per C.A. Tecnam MOD2006/033 is installed (Other Air Speeds remain unchanged): Maximum Landing Gear Operation Speed VLO: 122 KIAS (119 KCAS) Maximum Landing Gear Extended Speed VLE: 122 KIAS (119 KCAS) 11. Reserved TCDS A.185 P2006T Page 6 of 9 Issue 04, 21 November 2013 12. Operations Capability: Day/Night-VFR, IFR Flight into expected or actual icing conditions is prohibited See Note 1 13. Maximum Weights: Take-off 1180 kg (2600 lb) Zero Fuel 1145 kg (2524 lb) Landing 1180 kg (2600 lb) The following values apply when EASA Major Change Approval n. 10037759 “Increment of the maximum take-off weight (1230 Kg)” as per C.A. Tecnam MOD2006/015 is installed: Take-off 1230 kg (2712 lb) Zero Fuel 1195 kg (2635 lb) Landing 1230 kg (2712 lb) 14. Centre of Gravity Range: Forward limit 0.221 m (16.5 % MAC) behind Datum Rear limit: 0.415 m (31.0 % MAC) behind Datum 15. Datum: Wing leading edge (MAC = 1.339m) 16. Reserved 17. Levelling Means: Seat support trusses (see AFM, 2006/044, Sect.6 for the procedure) 18. Minimum Flight Crew: 1 (Pilot) 19. Maximum Passenger Seating Capacity: 3 20. Reserved 21. Baggage/Cargo Compartments: Max. allowable Load 80 kg Location 1.215 m aft the datum 22. Wheels and Tyres: Nose Wheel Tyre Size 5.00-5 Main Wheel Tyre Size 6.00-6
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TCDS A.185 P2006T Page 7 of 9 Issue 04, 21 November 2013 A.IV. Operating and Service Instructions 1. Flight Manual: C.A. Tecnam Aircraft P2006T report “Aircraft Flight Manual” No. 2006/044 1st ed. Rev 0 dated May 25th 2009 and any EASA approved edition and revision. 2. Airworthiness Limitations: C.A. Tecnam Aircraft P2006T report “Airworthiness Limitation and instruction for continued airworthiness" No. 2006/032 1st ed. Rev 2 dated May 25th 2009 and any EASA approved edition and revision. 3. Airplane Maintenance Manual (AMM): C.A. Tecnam Aircraft P2006T report "Aircraft Maintenance Manual” No. 2006/045 current issue 4. Illustrated Parts Catalogue: C.A. Tecnam Aircraft P2006T report “Airplane Illustrated Parts Catalogue” No. 2006/046 current issue 5. Service Information and Service Bulletins: Refer to Service Bulletin No. SB 000 - CS “Service Bulletins record”, current issue TCDS A.185 P2006T Page 8 of 9 Issue 04, 21 November 2013 A.V. Notes: 1. Airplane has been certified to operate VFR Day, VFR Night and IFR Night. Basic aircraft equipment configuration allows VFR Day operation. Additional equipment configuration are available at customer choice (see “Aircraft Flight Manual” Sect.6 for further information). 2. When major change, “Tecnam MOD2006/002” (Easa approval 10029633), is installed for Optional Equipment Garmin G950, the corresponding major modification to CRI A-01 must be considered together with special condition detailed in CRI B-52 “Human factor in Integrated Avionic Systems”. TCDS A.185 P2006T Page 9 of 9 Issue 04, 21 November 2013 ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record TC Holder Period Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA effective III. Change Record Issue Date Changes Issue 01 5 June 2009 Initial issue Issue 02 30 March 2012 Update to include changes MOD2006/002” (Easa approval 10029633) and MOD2006/015” (Easa approval 10037759) Issue 03 20 December 2012 Update to include changes MOD2006/033” (Easa approval 10041602) Issue 04 08 November 2013 Amend fuel specification