TECNAM P92-JS Model Guide
TECNAM P92-JS · Model Guide
Overview
The TECNAM P92-JS is a two-seat, single-engine light aircraft with a strut-braced rectangular high wing, fixed main landing gear and a steerable nosewheel. It is built by Costruzioni Aeronautiche Tecnam and certified by EASA under JAR-VLA. It is powered by a Rotax 912 S2 engine.
- Two seats, strut-braced high wing, fixed gear; EASA type certificate A.412 (SO/A-340), certified to JAR-VLA.
- Rotax 912 S2 engine: 98.6 hp for 5 minutes maximum, 92.5 hp continuous, with a fixed-pitch wooden Hoffmann propeller.
- The manual lists two weight options, 550 kg and 600 kg MTOW. Confirm which one a given aircraft is approved for.
- Standard tanks hold 70 liters (66.8 usable); optional 90-liter tanks give 86.8 usable.
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 m ·
- 2.5
- Length m ·
- 6.4
- Wing span m ·
- 8.7
- Wing area m2 ·
- 12
- Engine power max (hp) ·
- 98.6
- Engine displacement cc ·
- 1,352
- Engine power continuous (hp) ·
- 92.5
- Fuel total capacity liters ·
- 70
Weight & balance
- Max baggage weight kg ·
- 20
- Standard empty weight kg ·
- 325
- Max useful load option a kg ·
- 225
- Max useful load option b kg ·
- 275
- Max takeoff weight option a kg ·
- 550
- Max takeoff weight option b kg ·
- 600
What engine does the TECNAM P92-JS use?
The TECNAM P92-JS uses a Rotax 912 S2 engine. It makes 73.5 kW (98.6 hp) at 5800 rpm for a maximum of 5 minutes, and 69.0 kW (92.5 hp) at 5500 rpm continuous.
What fuel can the TECNAM P92-JS burn?
The TECNAM P92-JS manual lists EN 228 Premium, EN 228 Premium plus and AVGAS 100LL. Standard tanks hold 70 liters in total, of which 66.8 are usable. Optional tanks hold 90 liters, of which 86.8 are usable.
How much can the TECNAM P92-JS carry?
The TECNAM P92-JS has standard empty weight of 325 kg. Useful load is 225 kg at 550 kg MTOW or 275 kg at 600 kg MTOW. Baggage is limited to 20 kg.
What is the TECNAM P92-JS Model Guide?
The TECNAM P92-JS Model Guide is a model guide for the TECNAM P92-JS, dated 2026.
What year was the TECNAM P92-JS Model Guide published?
The TECNAM P92-JS Model Guide — the TECNAM P92-JS model guide on file — is dated 2026.
Most owners only have the POH. Here's the essential set for the TECNAM P92-JS.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P92-JSmanuals & documents
In this document
Weights and loading
The flight manual gives two maximum takeoff weights, 550 kg and 600 kg. Standard empty weight is 325 kg, so useful load is 225 kg or 275 kg respectively. Maximum baggage is 20 kg. Wing loading is 45.8 or 50 kg/m2, and power loading is 5.6 or 6.1 kg/hp.
Engine, propeller and fuel
The Rotax 912 S2 is a 4-cylinder, 1352 cc engine with liquid-cooled heads and air-cooled cylinders, twin carburettors and a reduction gear. It takes EN 228 Premium or Premium plus, or AVGAS 100LL. Oil capacity is 3.0 liters and coolant is 3 liters. The propeller is a 2-blade fixed-pitch wooden Hoffmann, 1740 mm in diameter.
Size and handling data
Wing span is 8.7 m, wing area 12 m2, overall length 6.4 m and height 2.5 m. Wheel track is 1.8 m and minimum ground steering radius is 5.5 m. Propeller ground clearance is 320 mm. Flaps travel from 0° to 38°. The manual lists a Cleveland wheel and brake kit with 5.00-5 main tires.
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
- Maximum power of 98.6 hp is limited to 5 minutes; continuous power is 92.5 hp.
- The propeller diameter is 1740 mm and no reduction is permitted.
- The flight manual must always be on board, and the aircraft must be operated within its limitations.
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 P92-JS Model Guide The TECNAM P92-JS is a two-seat, single-engine light aircraft with a strut-braced rectangular high wing, fixed main landing gear and a steerable nosewheel. It is built by Costruzioni Aeronautiche Tecnam and certified by EASA under JAR-VLA. It is powered by a Rotax 912 S2 engine. • Two seats, strut-braced high wing, fixed gear; EASA type certificate A.412 (SO/A-340), certified to JAR-VLA. • Rotax 912 S2 engine: 98.6 hp for 5 minutes maximum, 92.5 hp continuous, with a fixed-pitch wooden Hoffmann propeller. • The manual lists two weight options, 550 kg and 600 kg MTOW. Confirm which one a given aircraft is approved for. • Standard tanks hold 70 liters (66.8 usable); optional 90-liter tanks give 86.8 usable. Weights and loading The flight manual gives two maximum takeoff weights, 550 kg and 600 kg. Standard empty weight is 325 kg, so useful load is 225 kg or 275 kg respectively. Maximum baggage is 20 kg. Wing loading is 45.8 or 50 kg/m2, and power loading is 5.6 or 6.1 kg/hp. Engine, propeller and fuel The Rotax 912 S2 is a 4-cylinder, 1352 cc engine with liquid-cooled heads and air-cooled cylinders, twin carburettors and a reduction gear. It takes EN 228 Premium or Premium plus, or AVGAS 100LL. Oil capacity is 3.0 liters and coolant is 3 liters. The propeller is a 2-blade fixed-pitch wooden Hoffmann, 1740 mm in diameter. Size and handling data Wing span is 8.7 m, wing area 12 m2, overall length 6.4 m and height 2.5 m. Wheel track is 1.8 m and minimum ground steering radius is 5.5 m. Propeller ground clearance is 320 mm. Flaps travel from 0° to 38°. The manual lists a Cleveland wheel and brake kit with 5.00-5 main tires. Safety notes: • Maximum power of 98.6 hp is limited to 5 minutes; continuous power is 92.5 hp. • The propeller diameter is 1740 mm and no reduction is permitted. • The flight manual must always be on board, and the aircraft must be operated within its limitations.