Type Certificate Data Sheet No. IA192
TECNAM P-2002 Sierra RG · Pilot's Operating Handbook
Overview
This document is the Type Certificate Data Sheet (TCDS) for the Tecnam P2002 Sierra RG, issued by the Civil Aviation Authority of Israel. It outlines the conditions and limitations under which the aircraft meets airworthiness requirements, including specifications for the engine, fuel, weights, and operational limits.
- Model: P2002 Sierra, Ultra-Light Category.
- Engine: ROTAX 912ULS2 (100 HP).
- Maximum Take-Off Weight: 454 KG.
- Fuel Capacity: 100 liters.
- Stalling speed (flaps down): 40 mph.
- Maximum flaps extended speed: 81 mph.
- Center of Gravity Range: 1693 mm to 1728 mm behind Datum.
- Number of seats: Two.
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 ·
- 2006
- File size ·
- 139 KB
- Publisher ·
- tecnam.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Oil capacity liters ·
- 2.5
- Fuel capacity liters ·
- 100
- Max baggage weight kg ·
- 20
- Max landing weight kg ·
- 454
- Max take off weight kg ·
- 454
- Max pilot passenger weight kg ·
- 172
Performance
- Va mph ·
- 100
- Vfe mph ·
- 81
- Vmo mph ·
- 100
- Vne mph ·
- 178
- Vs1 mph ·
- 46
- Vso mph ·
- 40
V-speeds
- VA_MPH ·
- 100
- VFE_MPH ·
- 81
- VMO_MPH ·
- 100
- VNE_MPH ·
- 178
- VS1_MPH ·
- 46
- VSO_MPH ·
- 40
Weight & balance
- Cg rear limit mm ·
- 1728
- Cg forward limit mm ·
- 1693
What is the Type Certificate Data Sheet No. IA192?
The Type Certificate Data Sheet No. IA192 is a pilot's operating handbook for the TECNAM P-2002 Sierra RG, dated 2006.
Where does the Type Certificate Data Sheet No. IA192 come from?
This copy of the Type Certificate Data Sheet No. IA192 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 No. IA192 published?
The Type Certificate Data Sheet No. IA192 — the TECNAM P-2002 Sierra RG pilot's operating handbook on file — is dated 2006.
Most owners only have the POH. Here's the essential set for the TECNAM P-2002 Sierra RG.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P-2002 Sierra RGmanuals & documents
In this document
Engine Specifications
The aircraft is powered by a ROTAX 912ULS2 engine with specific RPM limits and temperature requirements.
Airspeed Limits
The document specifies various airspeed limits including Vne (178 mph), Vmo (100 mph), and stalling speeds.
Weight and Balance
Maximum take-off and landing weight is 454 KG, with specific limits for pilot, passenger, and baggage.
Center of Gravity
The forward limit is 1693 mm and the rear limit is 1728 mm behind the datum.
Required Equipment
Basic required equipment must be installed for certification as per applicable airworthiness regulations.
Operating Limitations
Aircraft must be operated according to the limitations specified in the CAAI approved AFM.
Safety notes
- Current weight and balance report must be provided at the time of original certification.
- The airplane must be loaded to keep the C.G. within specified limits.
- Major structural repairs must be done at CAAI certificated repair stations.
- Placards must be installed in the cockpit as specified.
Full document text
TCDS IA192 Rev. 0 State of Israel Ministry of Transport Civil Aviation Authority Number: IA192 Revision: 0 Make: Costruzioni AeronauticheTecnam s.r.l. Via Tasso, 478 80127 Napoli, Italy Model: P2002 Sierra 23 March, 2006 TYPE CERTIFICATE DATA SHEET NO. IA192 This Data Sheet which is part of Type Certificate No. IA192 prescribes conditions and limitations under which the aircraft for which the Type Certificate was issued meets the airworthiness requirements of the Aviation Regulations (Certification Procedures for Aircraft and Parts thereof) – 1977 - הטיס תקנות - תשל "ז Type Certificate Holder: Costruzioni AeronauticheTecnam s.r.l. Via Tasso, 478 80127 Napoli, Italy Model: P2002 Sierra I. Model P2002 Sierra, Ultra-Light Category, Approved by CAAI February 2, 2006 Engine 1 ROTAX 912ULS2 (100 HP) per Limitations Section of CAAI approved Airplane Flight Manual (AFM). Fuel Gasoline, minimum 95 octane rating per Limitations Section of CAAI approved AFM. Oil Use SAE specification oil, see also Engine Manual. Engine limits (RPM) - Maximum (Limited for 5 minutes) 5800 - Maximum continuous 5500 Cylinder Head Temperature - Maximum 150ºC - Minimum for Flight 60º Oil Temperature - Maximum 140ºC - Minimum for Flight 50ºC Oil Pressure - Maximum 7.0 bar - Minimum 0.8 bar - Normal Operating Temperature 2.0-5.0 bar Propeller Tonini GT-2/173/VRR-SRTC FW 01 Two wood Blades, fixed pitch (See Propeller Manual). Levelling means Seat support trusses (See AFM, Section 6). Airspeed Limits (Mph) - Vne (never exceed speed) 178 - Vmo (Maximum operational speed in level flight ) 100 - Va (Maneuvering speed) 100 - Vso (Stalling speed flaps down) 40 - Vs1 (Stalling speed flaps up) 46 - Vfe (Maximum flaps extended speed) 81 Page 1 2 3 Rev. 0 0 0 TCDS IA192 Rev. 0 IA192 Rev.0 page 2 of 3 Controls Surfaces Travel: Ailerons 20˚ Up (+ 2˚) 15˚ Dn ( + 2˚) Elevator 15˚ TEU (+ 1˚) 3˚ TE˚D (+ 1˚) Trim Tab 2˚ ; 9˚ deg. (+ 1˚) Rudder Left 30˚ Right 30˚ (+ 2˚) Flaps 0˚ ; 40˚ (+ 2˚) Center of Gravity Range: Fwd Limit: 1693 mm behind Datum; (26.0% of MAC) Rear Limit: 1728 mm behind Datum. (32.5% of MAC) Datum Propeller support flange without spacer Maximum Weights - Maximum Take-Off 454 KG (See Notes 2, 4, 5) - Maximum Landing 454 KG - Maximum Pilot and Passenger 172 KG Maximum Baggage 20 KG, 2.26 m aft the datum Minimum Crew One pilot Number of seats Two Wheels and Tyres Nose Wheel Tyre Size 4.00-6; Main Wheel Tyre Size 5.00-5 Fuel Capacity (liters) Total Fuel: 100 Oil Capacity (liters) 2.5 (2 litres minimum) Cooling System Per Limitations Section of CAAI approved AFM Manufacturer Serial Model P2002 Sierra S/N 141 and Subsequent Numbers eligible Certification Basis BCAR CAP 482 Section S, Rev. 3 . /129 2002 components defined by Drawing List the consists of Sierra 2002 P The Model Type Design Data Import Israeli Airworthiness Certificate may be issued on the basis of a Tecnam Statement of Requirements Conformity containing the following statement: “The airplane covered by this certificate has been examined, tested and found to conform to the type design approved under CAAI Type Certificate No. IA192 and to be in condition for safe operation”. Equipment The basic required equipment as prescribed in the applicable airworthiness regulation (see certification basis) must be installed in the aircraft for certification. The Required Equipment for the kinds of approved operations are listed in the Tecnam P2002 Sierra AFM, dated December 28, 2005. Service P2002 Sierra Technical Information (Service Bulletins), issued by Tecnam and approved by Information CAAI. Available documents for P2002 Sierra: - AFM 2002/127, CAAI approved February 2, 2006 - Maintenance Manual 2002/128 dated December 28, 2005. TCDS IA192 Rev. 0 IA192 Rev.0 page 3 of 3 Other Operating Aircraft shall be operated according to Operating Limitations of the CAAI approved AFM. Limitations NOTES: NOTE 1: (a) Current weight and balance report including list of equipment included in certified empty weight and loading instructions must be provided for each aircraft at the time of original certification. (b) The airplane must be loaded so that the C.G. is within the specified limits at all times. NOTE 2: All required placards listed in the limitation section of the CAAI approved AFM must be installed in the appropriate locations in the airplane. NOTE 3: Information essential to the proper servicing and maintenance of the aircraft is contained in the manufacturer’s Maintenance Manual marked Tecnam. Mandatory replacement times, structural inspection intervals and related structural inspection procedures are presented in the approved section of the Maintenance Manual. NOTE 4: Major structural repairs must be accomplished at CAAI certificated repair stations in accordance with Tecnam repair methods approved by CAAI. NOTE 5: Placards must be posted in the cockpit, as follows: 1. Maximum Takeoff Weight: 454 Kg. 2. Minimum Fuel Capacity for Take Off: 15 liters END