Tecnam ECHO CLASSIC JABIRU P92 Flight Manual
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Tecnam ECHO CLASSIC JABIRU P92 Flight Manual

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FLIGHT MANUAL
P92 E
M
:
ANUFACTURER
COSTRUZIONI AERONAUTICHE
P92 E
A
:
IRCRAFT TYPE
S
:...............................................................
ERIAL NUMBER
M
ANUFACTURING DATE
The Flight Manual must always be kept on board the aircraft. The aircraft
described herein is to be operated in accordance with procedures and limitations
described in this Flight Manual.
st
th
1
edition,5
July 2011
F
LIGHT MANUAL
C
CHO
LASSIC
C
J
CHO
LASSIC
ABIRU
:.....................................................................
P92 Classic Jabiru
I N T R O D U C T I O N
J
ABIRU
TECNAM
S.r.l.
i-1

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Summary of Contents for Tecnam ECHO CLASSIC JABIRU P92

  • Page 1 P92 Classic Jabiru LIGHT MANUAL I N T R O D U C T I O N FLIGHT MANUAL P92 E LASSIC ABIRU TECNAM S.r.l. ANUFACTURER COSTRUZIONI AERONAUTICHE P92 E LASSIC ABIRU IRCRAFT TYPE :............... ERIAL NUMBER :..............ANUFACTURING DATE The Flight Manual must always be kept on board the aircraft.
  • Page 2 P92 Classic Jabiru LIGHT MANUAL I N T R O D U C T I O N RECORD OF REVISIONS All revisions to the current Manual, except for actual weighing data, must be recorded in the following table. New text or amendments to revised pages shall be clearly marked by a vertical black line on the left hand margin, with revision N°...
  • Page 3 P92 Classic Jabiru LIGHT MANUAL I N T R O D U C T I O N List of Effective Page Section Page Date Section Page Date July 2011 July 2011 “ “ “ “ “ “ “ July 2011 “...
  • Page 4 P92 Classic Jabiru LIGHT MANUAL I N T R O D U C T I O N Section Page Date Section Page Date July 2011 “ “ “ “ “ July 2011 “ “ “ “ edition,5 July 2011...
  • Page 5 P92 Classic Jabiru LIGHT MANUAL I N T R O D U C T I O N TABLE OF CONTENTS General Section 1 Limitations Section 2 Emergency procedures Section 3 Normal procedures Section 4 Performance Section 5 Weight and balance Section 6 Systems description Section 7...

  • Page 6: Table Of Contents

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L SECTION 1 GENERAL TABLE OF CONTENTS INTRODUCTION ...................... 2 WARNINGS - CAUTIONS - NOTES ................ 2 THREE VIEW DRAWING ..................3 DESCRIPTIVE DATA ....................4 CONTROL SURFACES TRAVEL LIMITS .............. 4 ........................

  • Page 7: Introduction

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L INTRODUCTION The P92 E is a twin seat single engine aircraft with a LASSIC ABIRU strut-braced rectangular high wing, fixed main landing gear and steerable nose wheel. This Flight Manual has been prepared to provide pilots and instructors with information for the safe and efficient operation of this aircraft.

  • Page 8: Three View Drawing

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L THREE VIEW DRAWING  Dimensions shown refer to aircraft weight of 473 kg and normal operat- ing tire pressure.  Propeller clearance 360mm  Propeller clearance with deflated front tire and compressed shock absor- ber 142mm ...

  • Page 9: Descriptive Data

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L DESCRIPTIVE DATA WING Wing span: 8.5 m Wing chord 1.4 m Wing surface 11.9 m Wing loading 39.7 kg/m Aspect ratio Taper ratio Dihedral 1.5° FUSELAGE Overall length 6.4 m Overall width 1.1 m...

  • Page 10: Engine

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L ENGINE Manuc: JABIRU AIRCRAFT Pty Ltd Model 2200 Aero Engine Engine Type: 4 cylinder horizontally-opposed twins with overall displacement of 2200 c.c., ram-air cooled heads and cylinders single carburetter, direct drive. Com- pression ratio 9.5:1.

  • Page 11: Oil

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L Oil system: Pumped with integral sump Oil: AeroShell W100 or 15W50 or equivalent Oil capacity: 2.3 litres COOLING Cooling system: Mixed air and liquid pressurized closed circuit system Coolant: Coolant type and specifications are detailed into the Jabiru manuals (see sec.

  • Page 12: Abbreviations And Terminology

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L ABBREVIATIONS AND TERMINOLOGY AIRSPEED TERMINOLOGY AND SYMBOLS Calibrated Airspeed is indicated airspeed corrected for position and instrument error. Indicated Airspeed: is the speed shown on the on-board airspeed in- dicator.
  • Page 13 P92 Classic Jabiru LIGHT MANUAL G E N E R A L METEOROLOGICAL TERMINOLOGY Outside Air Temperature is the free air static temperature expressed in degrees Celsius (°C). Standard Temperature is 15°C at sea level pressure altitude and de- creased by 2°C for each 1000 ft of altitude. Pressure Altitude is the altitude read from an altimeter when the baro- metric subscale has been set to 1013 mb.
  • Page 14 P92 Classic Jabiru LIGHT MANUAL G E N E R A L WEIGHT AND BALANCE TERMINOLOGY Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. is the horizontal distance from the reference datum to the center of gravity (C.

  • Page 15: Unit Conversion Factors

    P92 Classic Jabiru LIGHT MANUAL G E N E R A L UNIT CONVERSION FACTORS  ULTIPLYING YIELDS EMPERATURE Fahrenheit [°F] Celsius [°C]       Celsius [°C] Fahrenheit [°F]       ORCES 2.205 Kilograms [kg]...
  • Page 16 P92 Classic Jabiru LIGHT MANUAL L I M I T A T I O N S SECTION 2 LIMITATIONS TABLE OF CONTENTS INTRODUCTION ...................... 2 AIRSPEED LIMITATIONS..................2 AIRSPEED INDICATOR MARKINGS ..............3 POWERPLANT LIMITATIONS ................4 PROPELLER ......................4 POWERPLANT INSTRUMENT MARKINGS ............

  • Page 17: Introduction

    P92 Classic Jabiru LIGHT MANUAL L I M I T A T I O N S INTRODUCTION Section 2 includes operating limitations, instrument markings, and basic placards necessary for safe operation of the P92 E , its engine, standard systems and LASSIC ABIRU standard equipment.

  • Page 18: Airspeed Indicator Markings

    P92 Classic Jabiru LIGHT MANUAL L I M I T A T I O N S AIRSPEED INDICATOR MARKINGS For all model MARKING IAS km/h SIGNIFICANCE 72 – 110 White arc Flap Operating Range (lower limit is 1.1VSO, at maxi- mum weight and upper limit is maximum speed permiss- ible with flaps extended at 38°) 110 –...

  • Page 19: Powerplant Limitations

    P92 Classic Jabiru LIGHT MANUAL L I M I T A T I O N S POWERPLANT LIMITATIONS The following table lists operating limitations for aircraft installed engine: : Jabiru Aircraft Pty Ltd. NGINE MANUFACTURER : Jabiru 2200 NGINE MODEL AXIMUM POWER Max Power (HP) Max RPM...

  • Page 20: Powerplant Instrument Markings

    P92 Classic Jabiru LIGHT MANUAL L I M I T A T I O N S POWERPLANT INSTRUMENT MARKINGS Powerplant instrument markings and their color code significance are shown below: RED LINE GREEN ARC YELLOW ARC RED LINE Minimum Normal Caution Maximum limit INSTRUMENT...

  • Page 21: Weight Limits

    P92 Classic Jabiru LIGHT MANUAL L I M I T A T I O N S WEIGHT LIMITS Maximum takeoff weight: 473 kg CENTER OF GRAVITY LIMITS Forward limit 20% aft of datum Aft limit 33% aft of datum Datum Leading edge of wing Aircraft Level Datum Cabin floor...
  • Page 22 P92 Classic Jabiru LIGHT MANUAL EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS INTRODUCTION ....................2 ENGINE FAILURE ....................2 FORCED LANDING ....................3 SMOKE AND FIRE ....................3 RECOVERY FROM UNINTENTIONAL SPIN............4 edition,5 July 2011...

  • Page 23: Introduction

    P92 Classic Jabiru LIGHT MANUAL EMERGENCY PROCEDURES INTRODUCTION Section 3 includes checklists and detailed procedures to be used in the event of emer- gencies. Emergencies caused by a malfunction of the aircraft or engine are extremely rare if appropriate maintenance and pre-flight inspections are carried out. In case of emergency, suggestions presented in this section should be considered and applied as necessary to correct the problem.

  • Page 24: Forced Landing

    P92 Classic Jabiru LIGHT MANUAL EMERGENCY PROCEDURES FORCED LANDING EMERGENCY LANDING WITHOUT ENGINE POWER Set glide speed to optimal value of 110 Km/h Select terrain area most suitable for emergency landing, possibly upwind Fuel shutoff valves: OFF Fuel pump: OFF Magnetos: OFF Tighten safety belts, release door safety lock and unlatch doors Flaps: as needed...

  • Page 25: Recovery From Unintentional Spin

    P92 Classic Jabiru LIGHT MANUAL EMERGENCY PROCEDURES NOTE DO NOT USE WATER to put out fire and do not open engine cowling until absolutely certain fire is extinguished. In case an appropriate fire extinguisher is not handy, still keeping engine cowling closed, it is possi- ble to use a woolen blanket, sand or dirt to try smothering the fire.
  • Page 26 P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS INTRODUCTION ....................... 2 RIGGING AND DERIGGING ENGINE COWLING ..........2 PREFLIGHT INSPECTION ..................3 CHECKLISTS ......................6 edition,5 July 2011...

  • Page 27: Introduction

    P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES INTRODUCTION Section 4 contains checklists and amplified procedures for the conduct of normal opera- tion. RIGGING AND DERIGGING ENGINE COWLING UPPER COWLING: Parking brake ON. Fuel shutoff valves OFF. III. Master switch OFF, Magnetos OFF. IV.

  • Page 28: Preflight Inspection

    P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES PREFLIGHT INSPECTION Before each flight, it is necessary to carry out a complete inspection of the aircraft as hereby detailed. CABIN INSPECTION A Weight and balance: check if within limits B Safety belts used to lock controls: free C Flight controls: activate flight controls to insure unhindered movement of control rods and surfaces.
  • Page 29 P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES G Check integrity of left side main landing gear, tire inflation (1.4 bar), condition and alignment; check fuselage skin condition. H Horizontal tail and tab: check integrity and unhindered movement. Vertical tail and rudder: check integrity and unhindered movement. L Check integrity of right side main landing gear, tire pressure (1.4 bar), condition and alignment;...
  • Page 30 P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES U Close engine cowling. Z Remove tow bar and chocks NOTE Avoid blowing inside left strut mounted pitot as this may damage instruments. FIG. 4-1 edition,5 July 2011...

  • Page 31: Checklists

    P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES CHECKLISTS BEFORE STARTING ENGINE (after preflight inspection) I. Flight planning, fuel consumption, refueling. II. Aircraft loading and related inspections (see section 6) III. Seat and safety belts adjustment IV. Doors secured V. Parking brake ON. STARTING ENGINE Master switch ON.
  • Page 32 P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES HOLDING Parking brake ON. Turn on navigation lights, strobe light, and landing light (optional equip- ment) III. Check engine parameters. Jabiru 80° - 100° Oil temperature 120°-160° Cylinder heads temperature 2.2 – 5.2 Oil pressure Check ammeter to insure alternator is charging.
  • Page 33 P92 Classic Jabiru LIGHT MANUAL NORMAL PROCEDURES CRUISE Reach cruising altitude Set power and engine rpm's for cruise. III. Check engine parameters Jabiru 80° - 100° Oil temperature 120°-160° Cylinder heads temperature 2.2 – 5.2 Oil pressure IV. Carburetor heat as needed, see paragraph on carb heat in Section 3. NOTE Compensate unpredicted asymmetrical fuel consumption between left and right fuel tanks by shutting off appropriate fuel tap located inside...
  • Page 34 P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E SECTION 5 PERFORMANCE TABLE OF CONTENTS INTRODUCTION ................2 AIRSPEED CALIBRATION............... 3 STALL SPEEDS ................. 3 CROSSWIND ..................4 TAKEOFF PERFORMANCE ............5 LANDING ..................6 CLIMB PERFORMANCE ..............

  • Page 35: Introduction

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E 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: ...

  • Page 36: Airspeed Calibration

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E AIRSPEED CALIBRATION The difference between indicated airspeed and calibrated airspeed is within JAR-VLA limits of  3% for all speeds above 1.3 Vs. STALL SPEEDS CONDITIONS: - weight 473 kg - engine idle - no ground effect...

  • Page 37: Crosswind

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E CROSSWIND Maximum demonstrated crosswind velocity is 15 Kts  Example: Given Find Wind direction = 30° Headwind = 17.5 Kts Wind velocity = 20 Kts Crosswind = 10 Kts Fig.

  • Page 38: Takeoff Performance

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E TAKE-OFF PERFORMANCE TAKEOFF DISTANCE ONDITIONS - ISA - Flaps: 15° - Engine: full throttle - Slope: 0° Wind: zero - Runway: dry, compact, grass PESO (Kg) Fig.

  • Page 39: Landing

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E LANDING ONDITIONS - Flaps: 38° Runway: dry, compact, grass - Engine: throttle idle - Slope: 0° Wind: zero Distance over a 15 m obstacle Ground roll DISTANCE WEIGHT (Kg)

  • Page 40: Climb Performance

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E CLIMB PERFORMANCE CLIMB RATE IN CLEAN CONFIGURATION ONDITIONS - ISA - Flaps: 0° - Weight 450 kg - Engine: full throttle P92 Echo P92 Echo/100 1000 1500 2000...

  • Page 41: Cruise

    P92 Classic Jabiru LIGHT MANUAL P E R F O R M A N C E CRUISE ONDITIONS Altitude: 0 Wind: 0 GIRI CAS km/h Consumo orario [lt/h] 2800 3000 CONSEQUENCES FROM RAIN AND INSECT Flight tests have demonstrated that neither rain nor insect impact build-up on leading edge has caused substantial variations on aircraft's flight qualities.
  • Page 42 P92 Classic Jabiru LIGHT MANUAL W E I G H T & B A L A N C E SECTION 6 WEIGHT & BALANCE TABLE OF CONTENTS INTRODUCTION ....................... 2 AIRCRAFT WEIGHING PROCEDURES ..............2 WEIGHING REPORT ....................3 C. G. TRAVEL ......................4 edition,5 July 2011...

  • Page 43: Introduction

    P92 Classic Jabiru LIGHT MANUAL W E I G H T & B A L A N C E INTRODUCTION This section describes the procedure for establishing the basic empty weight and moment of the aircraft. Loading procedure information is also provided. AIRCRAFT WEIGHING PROCEDURES REPARATION Carry out weighing procedure inside closed hangar...

  • Page 44: Weighing Report

    P92 Classic Jabiru LIGHT MANUAL W E I G H T & B A L A N C E WEIGHING REPORT Model P92 C s/n:____ Weighing n°____ Date:_________ LASSIC Datum: Propeller support flange without spacer meters Nose wheel weight W Plumb bob distance from LS wheel LS wheel weight Plumb bob distance from RS wheel...

  • Page 45: C. G. Travel

    P92 Classic Jabiru LIGHT MANUAL W E I G H T & B A L A N C E C. G. TRAVEL Maximum admissible C.G. travel exceeds actual operational limits. Moreover, oc- cupants and fuel impact only marginally on CG travel. When on flat terrain, exceeding CG travel aft limit will cause aircraft tail to lower.
  • Page 46 P92 Classic Jabiru LIGHT MANUAL SYSTEMS SECTION 7 AIRPLANE AND SYSTEM DESCRIPTIONS TABLE OF CONTENTS INTRODUCTION ....................2 AIRFRAME ......................2 FLIGHT CONTROLS ....................2 INSTRUMENT PANEL .................... 3 SEATS AND SAFETY HARNESS ................4 DOORS ........................4 BAGGAGE COMPARTMENT ................. 5 ENGINE ........................

  • Page 47: Introduction

    P92 Classic Jabiru LIGHT MANUAL SYSTEMS INTRODUCTION This section provides description and operation of the aircraft and its systems. AIRFRAME The wing is made up of a central light alloy torque box; a composite leading edge is attached to the front spar and geometrically similar flap and aileron are hinged to rear.

  • Page 48: Instrument Panel

    P92 Classic Jabiru LIGHT MANUAL SYSTEMS Flaps are extended via an electric servo actuator controlled by a switch on the dashboard. Flaps act in continuous mode, an mechanical indicator shows surface position. The electric circuit is protected by a breaker positioned on the right side of the dashboard.

  • Page 49: Seats And Safety Harness

    P92 Classic Jabiru LIGHT MANUAL SYSTEMS HROTTLE RICTION It is possible to adjust the engine's throttle friction by tightening appropriately the friction lock located on the dashboard near center throttle control. SEATS AND SAFETY HARNESS Aircraft features three point fitting safety belts with waist and diagonal straps ad- justable via a sliding metal buckle.

  • Page 50: Baggage Compartment

    P92 Classic Jabiru LIGHT MANUAL SYSTEMS BAGGAGE COMPARTMENT The baggage compartment is located behind the pilots' seats. Baggage shall be uniformly distributed on utility shelf. ENGINE Manuc: JABIRU AIRCRAFT Pty Ltd Model 2200 Aero Engine Engine Type: 4 cylinder horizontally-opposed twins with overall displacement of 2200 c.c., ram-air cooled heads and cylinders single carburetter, direct drive.

  • Page 51: Airspeed Indicator System

    P92 Classic Jabiru LIGHT MANUAL SYSTEMS IL AND CYLINDER HEADS TEMP OIL PRESSURE These instruments are connected in series with their respective sensors. Tempera- ture instruments are protected by the same breaker; oil pressure indicator and a second breaker protects other instruments. UEL LEVEL GAUGE Each fuel level gauge is connected with their respective floating located in each fuel tank.
  • Page 52 P92 Classic Jabiru LIGHT MANUAL GROUND HANDLING AND SERVICE SECTION 8 GROUND HANDLING AND SERVICE TABLE OF CONTENTS INTRODUCTION ....................2 AIRPLANE INSPECTION PERIODS ..............2 AIRPLANE REPAIR OR MODIFICATIONS ............2 GROUND HANDLING .................... 2 CLEANING AND CARE ..................5 edition,5 July 2011...
  • Page 53 P92 Classic Jabiru LIGHT MANUAL GROUND HANDLING AND SERVICE INTRODUCTION This section contains factory-recommended procedures for proper ground han- dling and routine care and servicing. It also identifies certain inspection and main- tenance requirements which must be followed if the aircraft is to retain its new- plane performance and dependability.
  • Page 54 P92 Classic Jabiru LIGHT MANUAL GROUND HANDLING AND SERVICE Tie-down ropes shall be fastened to the wing strut attachments and anchoring shall be provided by ramp tie-downs. Nose gear fork can be used for front tie- down location. Flight controls shall be secured to avoid possible weathervaning to end travel damage of moving surfaces.
  • Page 55 P92 Classic Jabiru LIGHT MANUAL GROUND HANDLING AND SERVICE GROUND ANCHORAGE (OPTIONAL) The airplane should be moored for immovability, security and protection. FAA Advisory Circular AC 20-35C, Tiedown Sense, contains additional information regarding preparation for severe weather, tiedown, and related information. The following procedures should be used for the proper mooring of the airplane: Head the airplane into the wind if possible.
  • Page 56 P92 Classic Jabiru LIGHT MANUAL GROUND HANDLING AND SERVICE CLEANING AND CARE To clean painted surfaces, use a mild detergent such as shampoo normally used for car finish; use a soft cloth for drying The plastic windshield and windows should never be dusted when dry; use luke- warm soapy water and dry using chamois only.

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