P92 Echo Classic De Luxe
TECNAM P-92 Echo S · Checklist
Overview
The Tecnam P-92 Echo S checklist provides essential specifications, performance data, and operational guidelines for this advanced ultra-light aircraft. It covers design features, construction details, and standard equipment, ensuring pilots have the necessary information for safe operation.
- Designed MTOW is 600 kg (1320 lb)
- Max speed at sea level is 230 km/h (124 kts)
- Cruising speed at 75% power is 205 km/h (110 kts)
- Stalling speed with flaps is 64 km/h (34.5 kts)
- Service ceiling is 4500 m (15000 ft)
- Fuel tank capacity is 45 liters (11.9 gallons) each
- Baggage allowance is 20 kg (44 lb)
- The aircraft features dual flight controls and adjustable seats
Document
Source
Originally published by tecnamair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 5.6 MB
- Publisher ·
- tecnamair.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Wing span m ·
- 9.4
- Wing area m2 ·
- 13.4
- Width cabin m ·
- 1.1
- Designed mtow kg ·
- 600
- Height overall m ·
- 2.5
- Length overall m ·
- 6.5
- Baggage allowance kg ·
- 20
Performance
- Max range km ·
- 750
- Max speed kmh ·
- 230
- Service ceiling m ·
- 4500
- Cruising speed kmh ·
- 205
- Rate of climb msec ·
- 6.2
- Stalling speed kmh ·
- 64
V-speeds
- VNE_KIAS ·
- 140
Weight & balance
- Limit loads g ·
- +4 / -2
- Ultimate loads g ·
- +6 / -3
- Max takeoff weight kg ·
- 600
What is the P92 Echo Classic De Luxe?
The P92 Echo Classic De Luxe is a checklist for the TECNAM P-92 Echo S.
Where does the P92 Echo Classic De Luxe come from?
This copy of the P92 Echo Classic De Luxe was originally published by tecnamair.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the TECNAM P-92 Echo S.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P-92 Echo Smanuals & documents
In this document
Specifications
The document outlines the designed MTOW, limit and ultimate loads, baggage allowance, dimensions, and wing area.
Performance
Details include max speed, cruising speed, rate of climb, stalling speed, service ceiling, and max range.
Construction
Describes the aircraft's monocoque tail cone, aluminum wing structure, fuel tank safety features, and visibility enhancements.
Interior
Highlights adjustable seats, luggage area, dual control systems, and instrument panel design.
Landing Gear
Covers the robust design of the landing gear, maintenance-free features, and shock absorber systems.
Engine and Propeller
Details the engine options, maintenance accessibility, fuel system, and propeller specifications.
Safety notes
- Ensure fuel quality meets specified standards.
- Check weight and balance before flight.
- Monitor stalling speed during maneuvers.
- Maintain awareness of service ceiling limitations.
- Inspect landing gear for damage before use.
Full document text
P92 Echo Classic De Luxe advanced ultra light SpecificationS DeSiGn WeiGHt & LoaDinG kG Lb Designed MTOW 600 1320 Limit Loads +4 / -2 g Ultimate Loads +6 / –3 g Baggage Allowance 20 44 DimenSion m in Wing Span 9,4 30,8 Lenght Over-All 6,5 21,3 Height Over-All 2,5 8,2 Width Cabin 1,1 3,6 Wing Area 13,4 m² 144 sqft Transv. Dihedral 1,5° Tailplane Span 2,9 9,5 Wheel Track 1,8 5,9 Wheel Tyres Air trAc 5.00-5 (mAin geAr) enGine anD propeLLer rotAx 100 HP rotAx 80 HP Power Max. @ 580M0 Rinpumte (Sm) Ax. 5 73.5 kW (98.5 HP) 59.6 kW (80 HP) Reduction 2,4286:1 2,273:1 Propeller gt tonini Fuel Auto fuel: min. ron 95 (Aki 91 Premium usA)/AvgAs: 100ll Tanks 45 x 2 litres 11,8 x 2 gAl performance 100 HP 80 HP Max Speed S/L 230 km/H 124 kts 219 km/H 117 kts Cruising Speed 75% 5250 Rpm 205 km/H 110 kts 190 km/H 102 kts Vne - Never Exceed Speed 260 km/H 140 kts Rate Of Climb 6,2 m/sec 1220 ft/min 6 km/H 1180 ft/min Stalling Speed (with Flap) 64 km/H 34,5 kts Service Celling 4500 m 15000 ft 4000 km/H 13000 ft Max Range (without Reserve) 65% 750 km 466 n.m. 720 km/H 447 n.m. Take Off Run & Landing Run 100 m 328 ft 110 km/H 360 ft fueL Fuel Tank Capacity 45x2 lt 11,9x2 gAl P92 Echo Classic De Luxe The P92 Echo Classic is a two-seat, single strut braced high wing aircraft. The P92 Echo Classic was designed and manufactured according to the international airworthiness standards. This has been accomplished by one of the most renowned European Designers in the general aviation field, with the aid of modern planning instruments. The P92’s performance and flying qualities are so superior that it compares to aircraft certified under FAR/CS 23. aDvantaGeS • Superior performance and flight characteristics • 205 km/h (100 kts) cruise speed • Stable and responsive • Ideal for flight schools • High level of comfort that makes it ideal for long routes • Excellent visibility advanced ultra light conStruction • The Tecnam line employs a monocoque tail cone section with the forward fuselage using sheet aluminium over steel tubing. • The wing is an all aluminium conventional structure with a single strut. • The fuel tanks hold 11.9 gal/45l each, located in the wing leading edge separated from the fuselage for safety. • A wide rear window together with large side windows complete the extraordinary visibility allowing 360° of vision in the cockpit. • The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column. • The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height. • The large flaps are deployed electrically. • The low stall speed and the general slow flying characteristics of the aircraft allow it to operate with ease on short runways. interior • Seats are adjustable and increase in height as they are moved forward. • The luggage area allowing for 44 pounds/20 kg of weight is located behind the seats with easy access in flight. • All Tecnam aircraft have dual control sticks, throttles and rudder pedals. • The trim tab and the flaps are electrically activated with a position indicator on the instrument panel. • The fresh air vents are conveniently located in the doors. • The aircraft has dual rudder pedals with a steerable nose wheel. • The wide instrument panel is designed to accommodate a full variety of instrumentation. LanDinG Gear • The main landing gear legs are made of spring steel, directly connected to the main structure. The landing gear is robust enough for rough strips and require no maintenance. • The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance. • The main landing gear wheels and brakes are conventional aircraft size (5.00x5) • The brake lever control and the parking brake are located forward between the seats. enGine anD propeLLer • The top and bottom engine cowls are quickly and easily removed making any maintenance procedure faster to accomplish. The top cowl has a large opening for easy access to the engine compartment for effective pre-flight inspections. • The engine’s mount is steel-tubing with shock mounts. It also supports the nosewheel that is not anchored directly to the cabin’s structure. • Two power plant options are available: Rotax 912UL 80HP four-cylinder, four-stroke engine and Rotax 912 ULS 100HP four-cylinder, four-stroke engine. Both engines come with an integrated 1:2.4286 reduction gear. • A fixed pitch wood and composite propeller comes as standard. • The quick drain gascolator is installed in the engine compartment with easy outside access. • The fuel system uses a mechanical engine driven pump along is with an electrical back-up pump. • The battery is located in the rear of the fuselage with easy access through a hinged door. advanced ultra light ZaragoZa plant COSTRUZIONI AERONAUTICHE TECNAM S.R.L. Costruzioni Aeronautiche Tecnam operates in three facilities. The Casoria facility is located adjacent to the Napoli Capodichino Airport and covers an area of 10.8000 sq ft with 43.100 sq ft of enclosed facilities. The Capua facility is located adjacent to the “Oreste Salomone” Airport, covers an area of 12.9000 sq ft with 43.100 sq ft of enclosed facilities. Capua has already a new area of 38.7000 sq ft with 64.600 sq ft of enclosed facilities. This extension will double the production capacity of the Capua plant. Modern reinforced concrete buildings are used for manufacturing processes, design activities and office administration. And finally the TECNAM Spain facility located in Villanueva del Gallego, Zaragoza - Spain covers an area of 16.404 sq ft with 65.661 sq ft of enclosed facilities with a runway adjacent of 3.937 length/ft. advanced ultra light VIa MaIorISE 081043 CapUa (CE) ItalY tEl.+39 0823 620134 FaX +39 0823 622899 WWW.tECnaM.CoM InFo@tECnaM.CoM CaSorIa plant CapUa plant StanDarD equipment
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fLiGHt inStrumentS anD inDicatorS Magnetic Compass Airspeed Ind., Kts Altimeter (In) Vertical Speed Bank Indicator Flaps Indicator Pitot System Static System Stabilator Trim Position Indicator enGine inStrumentS Tachometer Hour Recorder Oil Press. Oil Temp. Head Temp. Lh + Rh Fuel Qty fLiGHt controLS Hydraulic Brakes Parking Brake Electrical Flaps Dual Flight Controls Steerable Nose Wheel Stabilator Trim (Between The Seats) Engine Controls: - Throttle, Two - Choke Flight Trim Controls: - Stabilator With Indicator Fuel Control Selector With On/Off Panel Switches: - Starter Engine Lh And Rh Ignition Switches eLectricaL SyStem 12 Volt 18A Amp. Battery 12 Volt Alternators - 20 Amp. Switches: - Landing Light 12 Volt Socket Circuit Fuses Panel fueL SyStem Two Integral Fuel Tanks With 90 Litres Total Capacity Engine Driven Fuel Pump Fuel Quick Drain interior Pilot And Copilot Seats: - Adjustable Fore And Aft - Arm Rest Seat Belts & Shoulder Harness, All Seats Wall To Wall Carpeting Map & Storage Pockets Luggage Compartments exterior Rear Window Tie Down Rings Main Wheels, 5,00 X 5 Nose Wheel, 4,00 X 6 Wheel Pants cabin confort SyStem Ventilator Adjustable, 2 Place poWerpLant anD propeLLer Engines: 1 Rotax 912ULS2 80/100 Hp, 4 Cylinders Liquid/Air Cooled, Integrated Reduction Gear Dual Ignition System Throttle Control Lh/Rh Tubular Steel Engine Mount Propeller Gt Propeller, 2 Blade Fix Propeller Spinner Air Filter; Oil Filter Oil And Water Coolers proDuct Support/DocumentS Manufacturers Full Two Year Limited Warranty Pilots Operation Handbook Maintenance Manual