TECNAM P2008 JC Model Guide
TECNAM P2008 JC · Model Guide
Overview
TECNAM P2008 JC is a single-engine, two-seat light aeroplane with a strut-braced high wing and fixed landing gear. It has a Rotax 912 S2 engine. It is EASA type certified (TC A.583, 27 September 2013) under CS-VLA, Normal category. All figures below come from the Aircraft Flight Manual (AFM), because no registry performance data was supplied.
- Two seats, strut-braced high wing, fixed gear. The Rotax 912 S2 makes 98.6 hp for 5 minutes and 92.5 hp continuous.
- Standard MTOW is 630 kg (1388 lb). The MTV-34 propeller supplement (S9) shows 650 kg (1433 lb).
- AFM speed limits: VNE 145 KIAS, VNO 113 KIAS, VA 99 KIAS, VFE 71 KIAS.
- No range, cruise speed or ceiling data was supplied. Confirm these in AFM Section 5 for the specific aircraft.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 47 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Height (ft) ·
- 8.8
- Length (ft) ·
- 22.9
- Max power (hp) ·
- 98.6
- Wing span (ft) ·
- 29.5
- Continuous power (hp) ·
- 92.5
- Max takeoff weight (lb) ·
- 1,388
V-speeds
- VA_KTS ·
- 99
- VFE_KTS ·
- 71
- VNE_KTS ·
- 145
- VNO_KTS ·
- 113
Weight & balance
- Max takeoff weight (lb) ·
- 1,388
- Max takeoff weight s9 (lb) ·
- 1,433
How many seats does the TECNAM P2008 JC have?
The TECNAM P2008 JC is a single-engine two-seat aircraft with a strut-braced high wing and fixed landing gear, according to the AFM foreword.
What engine does the TECNAM P2008 JC use?
The TECNAM P2008 JC uses a Rotax 912 S2 of 1352 cc. It is rated 98.6 hp at 5800 rpm for 5 minutes maximum and 92.5 hp at 5500 rpm continuous.
What is the maximum takeoff weight of the TECNAM P2008 JC?
The standard AFM gives 630 kg (1388 lb) for the TECNAM P2008 JC. The S9 supplement for the MTV-34 propeller lists 650 kg (1433 lb).
What is the TECNAM P2008 JC Model Guide?
The TECNAM P2008 JC Model Guide is a model guide for the TECNAM P2008 JC, dated 2026.
What year was the TECNAM P2008 JC Model Guide published?
The TECNAM P2008 JC Model Guide — the TECNAM P2008 JC model guide on file — is dated 2026.
Common. More common than 92% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the TECNAM P2008 JC.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Powerplant and propeller
The engine is a Bombardier-Rotax 912 S2: 4 cylinders, horizontally opposed, 1352 cc, liquid-cooled heads, ram-air cooled cylinders, with an integrated reduction gearbox. Maximum power is 73.5 kW (98.6 hp) at 5800 rpm for 5 minutes, and 69.0 kW (92.5 hp) at 5500 rpm continuous. The standard propeller is a GT 2-blade fixed-pitch wood propeller, 1730 mm. The S9 supplement lists a 3-blade MT Propeller, 1700 mm.
Size and weights
Wing span is 9.00 m (29.5 ft), overall length 6.93 m (22.9 ft) and height 2.67 m (8.8 ft). Wing area is 12.16 m2. Standard MTOW is 630 kg (1388 lb), giving a wing loading of 51 kg/m2. With the S9 supplement, MTOW is 650 kg (1433 lb) and wing loading is 53.5 kg/m2. Check which weight applies to the airframe you are considering.
What to check when buying
Confirm the AFM edition and revision match the aircraft. One manual provided is Edition 2, Revision 6 (19 February 2020). Check which supplements are fitted (Section 9 lists them) and whether the propeller and MTOW match. Recent revisions amended the equipment list and added new brake pumps (Rev 5) and a pitot heating check (Rev 2). Verify those items on the aircraft.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Do not exceed VNE (145 KIAS) in any operation. Exceed VNO (113 KIAS) only in smooth air and with caution.
- Do not make full or abrupt control movements above VA (99 KIAS); the aircraft may be overstressed.
- The AFM must be carried in the aeroplane at all times, and the owner is responsible for keeping it current.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
TECNAM P2008 JC Model Guide TECNAM P2008 JC is a single-engine, two-seat light aeroplane with a strut-braced high wing and fixed landing gear. It has a Rotax 912 S2 engine. It is EASA type certified (TC A.583, 27 September 2013) under CS-VLA, Normal category. All figures below come from the Aircraft Flight Manual (AFM), because no registry performance data was supplied. • Two seats, strut-braced high wing, fixed gear. The Rotax 912 S2 makes 98.6 hp for 5 minutes and 92.5 hp continuous. • Standard MTOW is 630 kg (1388 lb). The MTV-34 propeller supplement (S9) shows 650 kg (1433 lb). • AFM speed limits: VNE 145 KIAS, VNO 113 KIAS, VA 99 KIAS, VFE 71 KIAS. • No range, cruise speed or ceiling data was supplied. Confirm these in AFM Section 5 for the specific aircraft. Powerplant and propeller The engine is a Bombardier-Rotax 912 S2: 4 cylinders, horizontally opposed, 1352 cc, liquid-cooled heads, ram-air cooled cylinders, with an integrated reduction gearbox. Maximum power is 73.5 kW (98.6 hp) at 5800 rpm for 5 minutes, and 69.0 kW (92.5 hp) at 5500 rpm continuous. The standard propeller is a GT 2-blade fixed-pitch wood propeller, 1730 mm. The S9 supplement lists a 3-blade MT Propeller, 1700 mm. Size and weights Wing span is 9.00 m (29.5 ft), overall length 6.93 m (22.9 ft) and height 2.67 m (8.8 ft). Wing area is 12.16 m2. Standard MTOW is 630 kg (1388 lb), giving a wing loading of 51 kg/m2. With the S9 supplement, MTOW is 650 kg (1433 lb) and wing loading is 53.5 kg/m2. Check which weight applies to the airframe you are considering. What to check when buying Confirm the AFM edition and revision match the aircraft. One manual provided is Edition 2, Revision 6 (19 February 2020). Check which supplements are fitted (Section 9 lists them) and whether the propeller and MTOW match. Recent revisions amended the equipment list and added new brake pumps (Rev 5) and a pitot heating check (Rev 2). Verify those items on the aircraft. Safety notes: • Do not exceed VNE (145 KIAS) in any operation. Exceed VNO (113 KIAS) only in smooth air and with caution. • Do not make full or abrupt control movements above VA (99 KIAS); the aircraft may be overstressed. • The AFM must be carried in the aeroplane at all times, and the owner is responsible for keeping it current.