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Type Certificate:
ASTM SLSA
Serial number: ________________
Build year: ___________________
Registration: __________________
Introduction
This manual contains information to be furnished to the pilot as required by the FAA in addition to further information
supplied by the manufacturer.
This manual must always be present on board the aircraft.
The aircraft is to be operated in compliance with information and limitations contained herein. All sections follow the
ASTM guidelines as finalized 14 December 2007.
P92 Eaglet
Flight Manual
FLIGHT MANUAL
US-LSA
P92 Eaglet
Manufacturer
COSTRUZIONI AERONAUTICHE TECNAM S.r.l.
Doc n° 27-13-100-00
1
Revision Date: 12-14-2007
Revision Number: 1.00
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Summary of Contents for Tecnam P92 Eaglet
- Page 1 P92 Eaglet Flight Manual FLIGHT MANUAL US-LSA P92 Eaglet Manufacturer COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Type Certificate: ASTM SLSA Serial number: ________________ Build year: ___________________ Registration: __________________ Introduction This manual contains information to be furnished to the pilot as required by the FAA in addition to further information supplied by the manufacturer.
- Page 2 P92 Eaglet Flight Manual Record of Revisions Any revisions to the present Manual, except actual weighing data, must be recorded in the following table. New or amended text in the revised pages will be indicated by a black vertical line in the left-hand margin; Revision Number, and date will be shown on the right-hand side of the amended page.
- Page 3 P92 Eaglet Flight Manual List of Effective Pages Page Date Page Date Page Date 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007 12-14-2007...
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Page 4: Table Of Contents
P92 Eaglet Flight Manual Table of Contents Unit Conversion Chart ..............................10 SECTION 1 GENERAL................................ 11 Introduction ................................11 Certification Basis ..............................11 Descriptive Data..............................13 1.3.1 Airframe................................13 Powerplant ................................13 1.4.1 Engine................................13 1.4.2 Propeller................................. 13 1.4.3 Oil System............................... 14 1.4.4... - Page 5 P92 Eaglet Flight Manual 1.9.6 Fuel Pressure ..............................22 1.9.7 O.A.T. Indicator.............................. 22 1.9.8 Stall Warning System............................22 1.9.9 Avionics ................................22 1.9.10 Exterior Lighting ............................22 1.10 Pitot and Static Pressure Systems .......................... 23 1.11 Landing Gear ................................. 24 1.11.1...
- Page 6 P92 Eaglet Flight Manual SECTION 4 PERFORMANCE ............................39 Introduction ................................... 39 Use of Performance Charts ............................ 39 Airspeed Indicator System Calibration ........................40 ICAO Chart ................................41 Stall Speeds................................42 Crosswind................................43 Takeoff Performance .............................. 44 Landing Distance ..............................45 Climb Performance ..............................
- Page 7 P92 Eaglet Flight Manual Checklist Procedures.............................. 56 6.2.1 Pre-Flight Inspection............................56 SECTION 7 GROUND HANDLING & SERVICE ......................62 Introduction ................................... 62 Aircraft Inspection Periods ............................ 62 Aircraft Alterations or Repairs..........................62 Ground Handling ..............................62 7.3.1 Towing ................................62 7.3.2...
- Page 8 P92 Eaglet Flight Manual Abbreviations & Terminology Airspeed Terminology KCAS Calibrated Airspeed is the indicated airspeed corrected for position and instrument error and expressed in knots. KIAS Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots.
- Page 9 P92 Eaglet Flight Manual Airplane Performance and Flight Planning Terminology Crosswind is the velocity of the crosswind component for which adequate control of the airplane Velocity during takeoff and landing is guaranteed Usable fuel is the fuel available for flight planning...
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Page 10: Unit Conversion Chart
P92 Eaglet Flight Manual Unit Conversion Chart Multiplying Yields Temperature Fahrenheit [°F] Celsius [°C] ⋅ − Celsius [°C] Fahrenheit [°F] ⋅ + Forces Kilograms [kg] 2.205 Pounds [lbs] Pounds [lbs] 0.4536 Kilograms [kg] Speed... -
Page 11: Section 1 General
1.1 Introduction The P92 Eaglet is an all metal, high wing, two-place, single-engine airplane equipped with tricycle landing gear. It is an ASTM compliant airplane designed to be flown by sport pilot rated pilots as well as higher rated pilots. - Page 12 P92 Eaglet Flight Manual THREE VIEW DRAWING Figure 1-1 General Views Wing Span 8.7m (28.5’) Length 6.5m (21,3’) Tail height 2.5m (8.2’) Propeller ground clearance 320mm (12.6”) Minimum ground steering radius 5.5m (18’) NOTE • Dimensions shown refer to aircraft weight of 600 kg (1320 lbs) and normal operating tire pressure Revision Date: 12-14-2007 Revision Number: 1.00...
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Page 13: Descriptive Data
P92 Eaglet Flight Manual 1.3 Descriptive Data 1.3.1 Airframe 1.3.1.1 Wing Wing span 8.7m (28.5’) Wing area 12 m (129 sq ft) Aspect ratio 6.31 Taper ratio 1.00 Dihedral 1.5º Wing chord 1.400 m (4.6’) 1.3.1.2 Fuselage Overall length 6.5m (21,3’) Overall width 1.143 m (45”) -
Page 14: Oil System
P92 Eaglet Flight Manual 1.4.3 Oil System Oil system Forced, with external oil reservoir See Rotax operator’s manual Oil Capacity Max. 3.0 liters (3.2 qt) – min. 2.0 liters (2.1 qt) 1.4.4 Cooling Cooling system: Combination air and liquid cooled system Coolant: See Rotax operator’s manual... -
Page 15: Standard Equipment
P92 Eaglet Flight Manual 1.6 Standard Equipment 1.6.1 Flight Instruments Airspeed Indicator, Altimeter, Vertical Speed Indicator, Compass 1.6.2 Engine instruments Tachometer, Oil Pressure, Fuel Pressure, Oil Temperature, Cylinder Head Temperature, Hour Meter, Left and Right Fuel Quantity, Volt Meter 1.6.3... -
Page 16: Airframe
P92 Eaglet Flight Manual 1.7 Airframe 1.7.1 Wing The wing is constructed of a central light alloy torque box; an aluminum leading edge with integrated fuel tank is attached to the front spar while flap and aileron are hinged to rear spar. Flaps are constructed of a center spar to which front and rear ribs are joined;... -
Page 17: Instrument Panel
1.7.9 Seats, Seatbelts, and Shoulder harnesses The P92 Eaglet usually comes with three point safety belts with waist and diagonal straps adjustable via a sliding metal buckle. Optional four point harnesses are available. Revision Date: 12-14-2007 Revision Number: 1.00... -
Page 18: Doors
P92 Eaglet Flight Manual Standard seats are aluminum with cushions. Seats are adjustable fore and aft by using the handle located under the seat on the outboard sides. Pushing the lever towards the center of the aircraft will release the locking pin allowing you to move the seat fore and aft. -
Page 19: Fuel System
P92 Eaglet Flight Manual 1.8.3 Fuel system The system is equipped with two aluminum fuel tanks integrated within the wing leading edge and accessible for inspection through dedicated covers. Capacity of individual tank is 45lt (11.9 gal) and total usable fuel is 86.8lt (22.9 gal). Each fuel tank is equipped with a cabin installed shutoff valve. - Page 20 P92 Eaglet Flight Manual Left fuel quantity indicator Right wing fuel tank vent Left wing fuel tank vent Right Fuel Tank Left Fuel Tank Right carb Figure 1-3 Fuel System Revision Date: 12-14-2007 Revision Number: 1.00 Doc n° 27-13-100-00...
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Page 21: Electrical System
P92 Eaglet Flight Manual 1.9 Electrical System The aircraft's electrical system consists of a 12 Volt DC circuit controlled by a Master switch located on the instrument panel. An integrated AC generator provides electricity and a 12 Volt battery placed in the fuselage or in the engine compartment. -
Page 22: Oil Temperature Gauge
P92 Eaglet Flight Manual 1.9.3 Oil temperature gauge Temperature reads in degrees Celsius. The oil temperature gauge has a green normal operating range, yellow caution ranges, and two red lines. 1.9.4 Cylinder head temperature The cylinder head temperature gauge normally reads the number three cylinder head temperature. It also indirectly reflects the coolant temperature. -
Page 23: Pitot And Static Pressure Systems
P92 Eaglet Flight Manual 1.9.10.3 Tail Strobe Light The strobe light is installed on top of the vertical stabilizer. Strobe light is activated by a switch and is protected by a fuse. Switch and fuse are positioned on the instrument panel. The signal reaches a strobe light trigger circuit box positioned in the tail cone just behind the baggage compartment. -
Page 24: Landing Gear
P92 Eaglet Flight Manual 1.11 Landing Gear The main landing gear consists of two special steel spring-leaf struts (1) positioned crossways to fuselage for elastic cushioning of landing loads. The two steel spring-leaf struts are attached to the fuselage underside via the main girder. -
Page 25: Brake System
P92 Eaglet Flight Manual 1.11.1 Brake System Figure 7-2 shows the brake system schematic diagram. The left and right wheel brakes are independent systems. The system has a reservoir (4) on the co-pilot’s brake pedals (1). The reservoir is directly connected to the brake master cylinders (3). Two flexible hoses connect the master cylinders on the co-pilot’s brake pedals to the master cylinders on the pilot’s brake pedals. -
Page 26: Section 2 Operating Limitations
P92 Eaglet Flight Manual SECTION 2 OPERATING LIMITATIONS 2 Introduction Section 3 includes operating limitations, instrument markings, and basic placards necessary for safe operation of the P92 Eaglet, its engine, standard systems and standard equipment. 2.1.1 Airspeed Limitations Airspeed limitations and their operational significance are shown below:... -
Page 27: Powerplant Limitations
P92 Eaglet Flight Manual 2.1.3 Powerplant Limitations The following table lists operating limitations for aircraft installed engine: Engine manufacturer: Bombardier Rotax GmbH. Engine model: 912 ULS or S2 Maximum power: (see table below) Max Power Max rpm. Time max. kW (hp) rpm prop.(engine) -
Page 28: Lubricant
P92 Eaglet Flight Manual 2.1.8 Lubricant Viscosity Use viscosity grade oil as specified in the following table: Warning Admissible pressure for cold start is 7 bar maximum for short periods Warning Use of Aviation Grade Oil with or without additives is not permitted 2.1.9... -
Page 29: Approved Fuel
P92 Eaglet Flight Manual 2.1.12 Approved Fuel Min. RON 95 (AKI 91 Premium USA) AVGAS 100LL (see Warning below) Warning Prolonged use of Aviation Fuel Avgas 100LL results in greater wear of valve seats and greater combustion deposits inside cylinders due to higher lead content. It is therefore suggested to avoid using this type of fuel unless strictly necessary. -
Page 30: Approved Maneuvers
P92 Eaglet Flight Manual 2.1.17 Approved Maneuvers This aircraft is intended for non-aerobatic operation only. Non-aerobatic operation includes: • Any maneuver pertaining to “normal” flight • Stalls (except whip stalls) • Lazy eights • Chandelles • Turns in which the angle of bank is not more than 60°... -
Page 31: Day Vfr
P92 Eaglet Flight Manual Flight into expected and/or known icing conditions is prohibited. NOTE Additional equipments may be asked to fulfill national or specific requirements. It’s a responsibility of the continued airworthiness manager to be compliant with these requirements. 2.1.21 Day VFR The airplane, in standard configuration, is approved only for day VFR operations under VMC: •... -
Page 32: Introduction
P92 Eaglet Flight Manual SECTION 3 WEIGHT & BALANCE 3 Introduction This section describes the procedure for establishing the basic empty weight and moment of the aircraft. Loading procedure information is also provided. 3.1 Aircraft weighing procedures 3.1.1 Preparation •... -
Page 33: Weighing Report
P92 Eaglet Flight Manual 3.2 Weighing report Model P92Eaglet____________S/N _____________ Date ________________ Horizontal Reference Datum: Propeller support flange w/o spacer. - Equipment list, date: _____ meters Nose wheel weight W Plumb bob distance LH wheel LH wheel weight Plumb bob distance RH wheel... -
Page 34: Distances From The Datum
P92 Eaglet Flight Manual 3.2.2 Distances from the datum The mean distances of the occupants, baggage and fuel from the datum are: Figure 3-4 Revision Date: 12-14-2007 Revision Number: 1.00 Doc n° 27-13-100-00... -
Page 35: Weight And Balance
P92 Eaglet Flight Manual 3.3 Weight and Balance In order to compute the weight and balance of this aircraft, we have provided the following loading charts. This will reduce the amount of math you need. To compute weight and balance use the formula: Weight * Arm = Moment. - Page 36 P92 Eaglet Flight Manual To computer weight and balance: 1. Get moments from loading charts 2. Obtain the empty weight and moment from the most recent weight and balance 3. Insert the weights and the moments for fuel, occupants and baggage from the previous chart 4.
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Page 37: Loading
3.4 Equipment List The following is a comprehensive list of TECNAM standard and optional supplied equipment for the P92 Eaglet. The list consists of the following groups: A. Engine and accessories B. - Page 38 P92 Eaglet Flight Manual Equipment list Date: Ref. Description & p/n Weight Datum m Electrical system Battery FIAMM 6H4P 12V 18Ah 6.00 0.71 Regulator, rectifier - p/n 945.345 0.20 0.82 Battery relay - p/n 111-226-5 0.30 2.59 Flaps actuator control - 2.20...
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Page 39: Section 4 Performance
P92 Eaglet Flight Manual SECTION 4 PERFORMANCE 4 Introduction This section provides all necessary data for accurate and comprehensive planning of flight activity from takeoff to landing. Data reported in graphs and/or tables were determined using: • “Flight test data” with conditions as prescribed by ASTM and bilateral agreements •... -
Page 40: Airspeed Indicator System Calibration
P92 Eaglet Flight Manual 4.2 Airspeed Indicator System Calibration Graph shows calibrated airspeed V as a function of indicated airspeed V IAS (kts) Fig. 4-1 Calibrated vs. Indicated Airspeed Revision Date: 12-14-2007 Revision Number: 1.00 Doc n° 27-13-100-00... -
Page 41: Icao Chart
P92 Eaglet Flight Manual 4.3 ICAO Chart Fig. 4-2 ICAO C HART Revision Date: 12-14-2007 Revision Number: 1.00 Doc n° 27-13-100-00... -
Page 42: Stall Speeds
P92 Eaglet Flight Manual 4.4 Stall Speeds Conditions: - Weight 600 kg (1320 lbs) - Throttle: idle - No ground effect NOTE Altitude loss during conventional stall recovery as demonstrated during test flights is approximately 100ft with banking under 30°. -
Page 43: Crosswind
P92 Eaglet Flight Manual 4.5 Crosswind Maximum demonstrated crosswind velocity is 15 knots Fig. 4-3 Crosswind chart Revision Date: 12-14-2007 Revision Number: 1.00 Doc n° 27-13-100-00... -
Page 44: Takeoff Performance
P92 Eaglet Flight Manual 4.6 Takeoff Performance TAKEOFF DISTANCE Conditions: Flaps: 15° Runway: dry, compact, grass Engine: full throttle Slope: 0° Wind: zero Vr = 48 KIAS = 49 KIAS ≥ 200 ft/min Vx flaps 15 = 56 KIAS Decrease distances by 10% for each 10 Knots of headwind. Increase distances by 20 % for each 10 Knots of tailwind For dry and paved runway operation decrease ground run by 6 %. -
Page 45: Landing Distance
P92 Eaglet Flight Manual 4.7 Landing Distance ONDITIONS Maximum weight = 600 kg (1320 lbs) Engine: throttle idle Brakes: maximum braking Runway: dry, compact grass Slope: 0° Wind: zero Conditions: ISA Flaps: 35° NOTE Decrease distances by 10% for each 10 Knots of headwind. Increase distances by 20 % for each 10 Knots of tailwind;... -
Page 46: Climb Performance
P92 Eaglet Flight Manual 4.8 Climb Performance CLIMB RATE IN CLEAN CONFIGURATION ONDITIONS • Flap: 0° • Engine: Full throttle • = 68 knots Fig. 5-5 C LIMB ⇒ Example: Given Find O.A.T. = 17°C Rate of climb = 654 ft/min... -
Page 47: Cruise
P92 Eaglet Flight Manual 4.9 Cruise Maximum takeoff weight = 600 kg (1320 lbs) Fuel tanks 2x45 liters (11.9 gal) (less the unusable fuel) OAT: +15°C Pressure altitude H Engine Speed Consumption Endurance (hrs) Range (N.m.) KTAS (gal/h) 4600 5000... -
Page 48: Balked Landing
P92 Eaglet Flight Manual 4.10 Balked Landing RATE OF CLIMB: BALKED LANDING ONDITIONS Maximum weight = 600 kg (1320 lb) Engine: full throttle Flaps: 35° 15 flaps = 48 KIAS NOTE During balked landing maneuver, flaps should be retracted immediately after applying full power. -
Page 49: Section 5 Emergency Procedures
P92 Eaglet Flight Manual SECTION 5 EMERGENCY PROCEDURES 5 Introduction Section 6 includes checklists and detailed procedures to be used in the event of emergencies. Emergencies caused by a malfunction of the aircraft or engine is extremely rare if appropriate maintenance and pre-flight inspections are carried out. -
Page 50: Engine Failures
P92 Eaglet Flight Manual 5.1 Engine Failures If an emergency arises, the basic guidelines described in this section should be considered and applied as necessary to correct the problem. 5.1.1 Engine Failures on Ground 5.1.1.1 ENGINE FAILURE DURING TAKEOFF RUN Throttle:.................. -
Page 51: Smoke And Fire
P92 Eaglet Flight Manual 5.1.2.4 LOW OIL PRESSURE Oil temperature:................. CHECK If the temperature tends to increase: If stable within the green arc: ............ LAND as soon as possible If increasing:................LAND as soon as possible and be alert for impending engine failure 5.1.2.5... -
Page 52: Cabin Fire During Flight
P92 Eaglet Flight Manual Fuel selector valves: ..............OFF Throttle:..................FULL IN until the engine stops running Cabin vents:................OPEN Ignition Switches:..............OFF Do not attempt an in-flight restart Procedure for a forced landing: ..........APPLY 5.2.4 Cabin Fire during Flight Cabin heat: ................ -
Page 53: Recovery From Unintentional Spin
P92 Eaglet Flight Manual Align the airplane on the opposite side of runway to the side with the defective tire to compensate for change in direction, which is to be expected during final rolling. Touchdown with the GOOD TIRE FIRST and hold aircraft with the flat tire off the ground as long as possible. -
Page 54: Electric Power System Malfunction
P92 Eaglet Flight Manual 5.6 Electric Power System Malfunction Electric power supply system malfunctions may be avoided by carrying out inspections as scheduled and prescribed in the Service Manual. Causes for malfunctions are hard to establish but, in any case, problems of this nature must be dealt with immediately. -
Page 55: Section 6 Normal Procedures
P92 Eaglet Flight Manual SECTION 6 NORMAL PROCEDURES 6 Introduction Section 6 contains checklists and the procedures for normal operation. 6.1 Removing and Reinstalling the Engine Cowling 6.1.1 Upper Cowling Parking brake: .........ON or chocks installed Fuel selector valves: ......OFF Ignition Switches:......OFF... -
Page 56: Checklist Procedures
P92 Eaglet Flight Manual 6.2 Checklist Procedures 6.2.1 Pre-Flight Inspection Before each flight, it is necessary to carry out a complete inspection of the aircraft starting with an external inspection followed by an internal inspection. 6.2.1.1 Cabin Inspection All required paperwork: ............ONBOARD Weight and balance: .............. - Page 57 P92 Eaglet Flight Manual 6.2.1.2 External Inspection It is best to follow to follow the external inspection in the station order outlined in fig. 6-1 so nothing is missed. Visual inspection is defined as follows: check for defects, cracks, detachments, excessive play, and unsafe or improper installation as well as for general condition.
- Page 58 P92 Eaglet Flight Manual M. Stall indicator micro switch : Check freedom of movement, turn on Master switch and check cabin acoustic warning signal is operative, turn off Master switch N. Right side fuel filler cap: CHECK visually for desired fuel level and secure O.
- Page 59 P92 Eaglet Flight Manual 6.2.1.4 STARTING ENGINE Brakes:..................SET Fuel selector valves: ..............BOTH ON Master switch: ................ON Throttle:..................IDLE Choke: ..................AS NEEDED Propeller area: ................CLEAR WARNING Check to insure no person or object is present in the area close to propeller Strobe light: ................
- Page 60 P92 Eaglet Flight Manual Carburetor Heat:................ CHECK Throttle:..................IDLE Fuel quantity indicators:............CHECK Fuel selector valves: ..............BOTH ON Flaps: ..................T/O (15°) Flight controls: ................CHECK Trim:..................CENTER Seat belts: .................. FASTENED Doors:..................CLOSED AND LOCKED Transponder (if installed): ............ALT 6.2.1.8...
- Page 61 P92 Eaglet Flight Manual 6.2.1.11 BALKED LANDING Throttle:..................FULL Airspeed: ................... 60 KIAS Flaps position: ................TO / 15 degrees Airspeed: ................... 65 KIAS Trim:..................ADJUST Above 300’ AGL: Flaps: ..................RETRACT Establish Vy clean:..............68 KIAS Trim:..................ADJUST After takeoff checklist:.............. COMPLETE 6.2.1.12...
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Page 62: Section 7 Ground Handling & Service
P92 Eaglet Flight Manual SECTION 7 GROUND HANDLING & SERVICE 7 Introduction This section contains factory-recommended procedures for proper ground handling and routine care and servicing. It also identifies certain inspection and maintenance requirements, which must be followed if the aircraft is to retain its new-plane performance and dependability. -
Page 63: Road Transport
P92 Eaglet Flight Manual 7.3.5 Road Transport It is recommended to secure tightly all aircraft components onto the cart to avoid damage during transport. Minimum cart size is 7x2.5 meters. It is suggested to place wings under the aircraft’s bottom, secured by specific clamps. Secondary components such as stabilator and struts shall be protected from accidental hits using plastic or other material. -
Page 64: Placards And Markings
P92 Eaglet Flight Manual Section 8 REQUIRED PLACARDS & MARKINGS 8 Placards and Markings The following limitation placards must be placed in plain view on the aircraft. Near the airspeed indicator a placard will state the following: Maneuvering speed V... - Page 65 Tecnam Aircraft, Inc. 1350 Churchill Way Marietta, GA 30062 www.tecnamaircraft.com Tecnam@bellsouth.net (770) 309-4155 Italian Address: COSTRUZIONI AERONAUTICHE TECNAM s.r.l. www.tecnam.com Casoria industrial plant 1a Traversa via G. Pascoli n°1 Via Maiorise 80026 Casoria (NA) – ITALY 81043 Capua (CE) - ITALY...
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