Tecnam P2002-JF Flight Manual
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Tecnam P2002-JF Flight Manual

Tecnam P2002-JF Flight Manual

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FLIGHT MANUAL

M
:
ANUFACTURER
COSTRUZIONI AERONAUTICHE
P2002-JF
A
:
IRCRAFT MODEL
EASA T
C
YPE
ERTIFICATE
S
: ...............................................................
ERIAL NUMBER
B
: ....................................................................
UILD YEAR
R
EGISTRATION MARKINGS
This manual contains information to be furnished to the pilot as required by
EASA in addition to further information supplied by the manufacturer.
This manual must always present on board the aircraft
The aircraft is to be operated in compliance with information and
limitations contained herein.
Sections2, 3, 4, 5 and 9 (supp.1) are approved by EASA n°EASA.AC.01372
dated 3/8/2005
st
th
1
Edition – 29
March 2004
F
M
LIGHT
ANUAL
Doc. n° 2002/28
st
th
1
edition, March 29
2004
st
rd
1
revision, August 3
2005
P2002-JF
TECNAM
N
. A .006
O
: ....................................................
P2002-JF
I n t r o d u c t i o n
S.r.l.
i-1

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Summary of Contents for Tecnam P2002-JF

  • Page 1: Flight Manual

    P2002-JF LIGHT ANUAL I n t r o d u c t i o n FLIGHT MANUAL Doc. n° 2002/28 edition, March 29 2004 revision, August 3 2005 P2002-JF TECNAM S.r.l. ANUFACTURER COSTRUZIONI AERONAUTICHE P2002-JF IRCRAFT MODEL EASA T . A .006 ERTIFICATE : ………………………………………………………...
  • Page 2 P2002-JF LIGHT ANUAL I n t r o d u c t i o n RECORD of REVISIONS Any revisions to the present Manual, except actual weighing data, must be recorded in the following table and, in case of approved sections, endorsed by the responsible airworthiness authority.
  • Page 3 P2002-JF LIGHT ANUAL I n t r o d u c t i o n LIST OF EFFECTIVE PAGES Sect. Page Date Sect. Page Date 3 August 2005 29 March 2004 “ “ “ “ 29 March 2004 “ “...
  • Page 4 P2002-JF LIGHT ANUAL I n t r o d u c t i o n Sect. Page Date Sect. Page Date 29 March 2004 29 March 2004 “ “ “ “ “ “ “ “ “ “ “ “ “...
  • Page 5 P2002-JF LIGHT ANUAL 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* Performances Section 5** Weight & Balance / Equipment List...
  • Page 6 P2002-JF LIGHT ANUAL I n t r o d u c t i o n INTENTIONALLY LEFT BLANK Edition – 29 March 2004...

  • Page 7: Table Of Contents

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l SECTION 1 GENERAL TABLE OF CONTENTS INTRODUCTION ..................2 CERTIFICATION BASIS ................2 WARNINGS - CAUTIONS - NOTES ............2 THREE-VIEW DRAWING................3 DESCRIPTIVE DATA.................

  • Page 8: Introduction

    S E C T I O N 1 G e n e r a l INTRODUCTION The P2002-JF is a twin seat, single engine aircraft with a tapered, low wing. fixed main landing gear and steerable nosewheel. This Flight Manual has been prepared to provide pilots and instructors with information for the safe and efficient operation of this very light aeroplane.

  • Page 9: Three-View Drawing

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l THREE-VIEW DRAWING 8.6 m 6.61 m 2.43 m NOTE Dimensions shown refer to aircraft weight of 580 kg and • normal operating tire pressure.

  • Page 10: Descriptive Data

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l DESCRIPTIVE DATA WING Wing span: 8.6 m Wing surface 11.5 m Wing loading 50.4 kg/m Aspect ratio Taper ratio Dihedral 5° FUSELAGE Overall length 6.61 m...

  • Page 11: Engine

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l ENGINE Manufacturer: Bombardier-Rotax GmbH Model 912 S2 Certification basis FAR 33 Amendment 15 Austrian T.C. No. TW 9-ACG dated 27 November 1998...

  • Page 12: Fuel

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l FUEL • Min. RON 95 Fuel grade: • EN 228 Premium • EN 228 Premium plus • AVGAS 100LL (see Section 2 page 11)

  • Page 13: Maximum Weights

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l MAXIMUM WEIGHTS Maximum take-off weight: 580 kg Maximum landing weight: 580 kg Maximum baggage weight 20 kg STANDARD WEIGHTS Standard Empty Weight...

  • Page 14: Abbreviations And Terminology

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS Calibrated Airspeed is the indicated airspeed corrected for position and instrument error and expressed in knots.

  • Page 15: March 2004

    P2002-JF LIGHT ANUAL S E C T I O N 1 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 decreased by 2°C for each 1000 ft of altitude.

  • Page 16: March

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l WEIGHT AND BALANCE TERMINOLOGY Datum “Reference datum” is an imaginary vertical plane from which all horizontal distances are measured for balance purposes.

  • Page 17: Unit Conversion Chart

    P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l UNIT CONVERSION CHART ULTIPLYING YIELDS EMPERATURE Fahrenheit [°F] Celsius [°C] ⋅ −   Celsius [°C] Fahrenheit [°F]   + ⋅...
  • Page 18 P2002-JF LIGHT ANUAL S E C T I O N 1 G e n e r a l INTENTIONALLY LEFT BLANK 1-12 Edition – 29 March 2004...
  • Page 19 P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations SECTION 2 LIMITATIONS TABLE OF CONTENTS INTRODUCTION....................2 AIRSPEED LIMITATIONS ..................2 AIRSPEED INDICATOR MARKINGS..............3 POWERPLANT LIMITATIONS ................4 LUBRICANT......................5 COOLANT....................... 6 PROPELLER ......................6 POWERPLANT INSTRUMENT MARKINGS ............

  • Page 20: Introduction

    ANUAL L imitations INTRODUCTION Section 2 includes operating limitations, instrument markings, and basic placards necessary for safe operation of the P2002-JF, its engine and standard systems and equipment. AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown below: SPEED...

  • Page 21: Airspeed Indicator Markings

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations AIRSPEED INDICATOR MARKINGS Airspeed indicator markings and their colour code are explained in the following table. Refer to section 9 of this Flight Manual for operational limitations for aircraft fitted with optional equipment.

  • Page 22: Powerplant Limitations

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations POWERPLANT LIMITATIONS The following table lists operating limitations for aircraft installed engine: : Bombardier Rotax GmbH. NGINE MANUFACTURER : 912 S2 NGINE MODEL : (see table below)

  • Page 23: Lubricant

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations WARNING Admissible pressure for cold start is 7 bar maximum for short periods. FUEL PRESSURE: 2.2 psi (0.15 bar) 5.8 psi (0.40 bar) LUBRICANT VISCOSITY Use viscosity grade oil as specified in the following table:...

  • Page 24: Coolant

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations COOLANT Coolant type and specifications are detailed into the “Rotax Operator’s Manual” and in its related documents. PROPELLER : Hoffmann Propeller GmbH ANUFACTURER : HO17GHM A 174 177 C...

  • Page 25: Powerplant Instrument Markings

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations POWERPLANT INSTRUMENT MARKINGS Powerplant instrument markings and their colour code significance are shown below: RED LINE GREEN ARC YELLOW ARC RED LINE Minimum limit Normal Caution Maximum...

  • Page 26: Weights

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations WEIGHTS Maximum takeoff weight: 580 kg Maximum landing weight: 580 kg Maximum zero fuel weight. 580 kg Maximum baggage weight: 20 kg (2.26m aft from datum) CENTER OF GRAVITY RANGE...

  • Page 27: Approved Maneuvers

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations APPROVED MANEUVERS This aircraft is certified in normal category under EASA CS-VLA. CS-VLA applies to aeroplanes intended for non-aerobatic operation only. Non aerobatic operation includes: Any manoeuvre pertaining to “normal” flight •...

  • Page 28: Flight Crew

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations FLIGHT CREW Minimum crew for flight is one pilot seated on the left side. KINDS OF OPERATION The airplane, in standard configuration, is approved only for day VFR operation with terrain visual contact.

  • Page 29: Fuel

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations FUEL : 50 liters each WO TANKS : 100 liters OTAL FUEL CAPACITY : 99 litres SABLE FUEL Q : 0.5 litres each (1.0 litres total) NUSABLE FUEL Q Compensate uneven fuel tank levels by acting on the fuel selector valve located into the cabin.

  • Page 30: Limitation Placards

    P2002-JF S E C T I O N 2 LIGHT ANUAL L imitations LIMITATION PLACARDS The following limitation placards must be placed in plain view on the aircraft. Near the airspeed indicator a placard will state the following: =96 K...
  • Page 31 P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS INTRODUCTION....................2 ENGINE FAILURES....................2 IN-FLIGHT ENGINE RESTART................

  • Page 32: Introduction

    P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s INTRODUCTION Section 3 includes checklists and detailed procedures to be used in the event of emergencies.
  • Page 33 P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF Speed: check Find a suitable place on the ground to land safely. The landing should be planned straight ahead with only small changes in directions not exceeding 45°...
  • Page 34 P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s LOW FUEL PRESSURE If the fuel pressure indicator falls below the 2.2 psi (0.15 bar) limit, it is necessary...

  • Page 35: In-Flight Engine Restart

    P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s IN-FLIGHT ENGINE RESTART Altitude: preferably below 4000 ft Carburettors heating: ON...

  • Page 36: Glide

    P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s ENGINE FIRE IN-FLIGHT Cabin heating: OFF Fuel selector valve: OFF Electric fuel pump: OFF...

  • Page 37: Landing Emergency

    P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s LANDING EMERGENCY FORCED LANDING WITHOUT ENGINE POWER Procedure to glide: apply (suggested airspeed 68 KIAS) Locate most suitable terrain for emergency landing, possibly upwind.

  • Page 38: Recovery From Unintentional Spin

    P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s LANDING WITH A FLAT MAIN TIRE 1. Pre-landing checklist: complete 2. Flaps: land 3.
  • Page 39 P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s CARBURETTOR ICE AT TAKEOFF At takeoff, given the unlikely possibility of ice formation at full throttle, carburettor heat is normally OFF.
  • Page 40 P2002-JF S E C T I O N LIGHT ANUAL E m e r g e n c y P r o c e d u r e s TRIM SYSTEM FAILURE LOCKED CONTROL In case the trim control should not respond, act as follows:...
  • Page 41 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS INTRODUCTION....................2 RIGGING AND DERIGGING ENGINE COWLING..........2 PRE-FLIGHT INSPECTIONS................. 3 CHECKLISTS......................7 Edition – 29 March 2004...

  • Page 42: Introduction

    P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures INTRODUCTION Section 4 contains checklists and the procedures for the conduct of normal operation. RIGGING AND DERIGGING ENGINE COWLING UPPER COWLING: Parking brake: ON Fuel selector valve: OFF III.

  • Page 43: Pre-Flight Inspections

    P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures LOWER COWLING After disassembling upper cowling, move the propeller to a horizontal position. Using a standard screwdriver, press and rotate 90° the two Cam-locks positioned on lower cowling by the firewall.
  • Page 44 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures EXTERNAL INSPECTION To carry out the external inspection it will be necessary to follow the checklist below with the station order outlined in fig. 4-1. WARNING Visual inspection is defined as follows: check for defects, cracks, detachments, excessive play, unsafe or improper installation as well as for general condition.
  • Page 45 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures WARNING Fuel level indicated by the fuel quantity indicators (on the instrument panel) is only indicative. For flight safety, pilot should verify actual fuel quantity embarked before takeoff.
  • Page 46 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures R Propeller and spinner condition: check for nicks and security. S Open engine cowling and perform the following checklist: Check no foreign objects are present. Check the cooling circuit for losses, check coolant level into the expansion tank, insure radiator honeycomb is unobstructed.

  • Page 47: Checklists

    P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures CHECKLISTS BEFORE STARTING ENGINE (after preflight inspection) Flight controls: operate until their stop checking for movement smoothness II. Parking brake: engage III. Throttle: adjust friction IV. Generator switch: ON, generator light ON, check the ammeter.
  • Page 48 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures CAUTION Master Avionic switch (if installed) must be set OFF during the engine’s start-up to prevent avionic equipments damages. STARTING ENGINE Circuit Breakers: check IN Generator & Master switches: ON III.
  • Page 49 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures BEFORE TAXIING Radio and Avionics: ON Altimeter: set III. Direction indicator: set in accordance with the magnetic compass IV. Parking brake: OFF and taxi TAXIING I. Brakes: check II.
  • Page 50 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures TAKEOFF AND CLIMB Call TWR for takeoff Check for clear final and wind on runway III. Parking brake: OFF Carburetor heat: OFF Taxi to line-up Check magnetic compass and direction indicator Full throttle (approx.
  • Page 51 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures NOTE Compensate unpredicted asymmetrical fuel consumption between left and right fuel tanks operating the fuel selector valve. Switch on the electric fuel pump prior to swap the fuel feeding from one tank to...
  • Page 52 P2002-JF S E C T I O N 4 LIGHT ANUAL Normal Procedures ENGINE SHUT DOWN Keep engine running at 1200 rpm for about one minute in order to reduce latent heat. Electric fuel pump: OFF III. Turn off all electrical utilities (with the exception of the Strobe Light)
  • Page 53 P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s SECTION 5 PERFORMANCES TABLE OF CONTENTS INTRODUCTION...................... 2 USE OF PERFORMANCE CHARTS................ 2 AIRSPEED INDICATOR SYSTEM CALIBRATION..........3 STALL SPEED (A ) ................

  • Page 54: Introduction

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s INTRODUCTION This section provides all necessary data for accurate and comprehensive planning of flight activity from takeoff to landing.

  • Page 55: Airspeed Indicator System Calibration

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s AIRSPEED INDICATOR SYSTEM CALIBRATION (Approved data) Graph shows calibrated airspeed V as a function of indicated airspeed V IAS (kts) Fig.
  • Page 56 P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s Fig.5-2. ICAO C HART ⇒ Example: Given Find Temperature = 20°C Ts = 12° Pressure Altitude = 1600 ft issue –...

  • Page 57: Stall Speed (Approved Data )

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s STALL SPEED (Approved data) : - Weight 580 kg ONDITIONS - Throttle: idle - No ground effect...

  • Page 58: Crosswind

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s CROSSWIND Maximum demonstrated crosswind velocity is 22 kts ⇒ Example: Given Find Wind direction = 30° Headwind = 17.5 Kts...

  • Page 59: Takeoff Performances (Approved Data )

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s TAKEOFF PERFORMANCES (Approved data) TAKEOFF DISTANCE ONDITIONS - Flaps: 15° - Runway: dry, compact, grass - Engine throttle: full throttle - Slope: 0°;...
  • Page 60 P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s NOTE 1. Decrease distances by 10% for each 10Kts of ahead wind. Increase distances by 20% for each 10 Kts of tailwind.

  • Page 61: Climb Performances

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s CLIMB PERFORMANCES CLIMB RATE IN CLEAN CONFIGURATION ONDITIONS - Flap: 0° - Engine: Full throttle = 65 KIAS - R/C residual: 100 ft/min.

  • Page 62: Cruise

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s CRUISE ONDITIONS - ISA - Wind: zero - MTOW = 580 kg TAS (KTS) 2224 RP M...

  • Page 63: Balked Landing

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s BALKED LANDING RATE OF CLIMB: BALKED LANDING ONDITIONS - Maximum weight = 580 kg - Engine: full throttle - Flaps: LAND (40°)

  • Page 64: Landing Distance (Approved Data )

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s LANDING DISTANCE (Approved data) LANDING DISTANCE AND GROUND ROLL ONDITIONS - Weight: 480 kg; Flap: 40° - Runway: dry, compact, grass - Engine: idle - Slope: 0°;...
  • Page 65 P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s OAT: ISA +10°C Hp (ft) Total Distance (m) Ground Run (m) 2000 4000 6000 OAT: ISA +20°C...

  • Page 66: Consequences From Rain And Insect

    P2002-JF S E C T I O N 5 LIGHT ANUAL P e r f o r m a n c e s CONSEQUENCES FROM RAIN AND INSECT Flight test have demonstrated that neither rain nor insect impact build-up on leading edge have caused substantial variations to aircraft’s flight qualities.
  • Page 67 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance SECTION 6 WEIGHT & BALANCE TABLE OF CONTENTS INTRODUCTION....................2 AIRCRAFT WEIGHING PROCEDURES .............. 2 WEIGHT AND BALANCE..................6 LOADING........................ 9 EQUIPMENT LIST ....................9 Edition – 29...

  • Page 68: Introduction

    P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance 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...
  • Page 69 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance MAC 1370 15 mm inboard from rib n°7 1337 from the propeller's flange (without sapacer) Reference line W2 * A - W1 * B W1 + W2...
  • Page 70 S E C T I O N 6 LIGHT ANUAL Weight & Balance EIGHING EPORT Model P2002-JF S/N:________ Weighing n°____ Date:_________ Datum: Propeller support flange without spacer. 1337 Datum Reference line W2 * A - W1 * B W1 + W2...
  • Page 71 S E C T I O N 6 LIGHT ANUAL Weight & Balance EIGHING EPORT Model P2002-JF S/N:________ Weighing n°____ Date:_________ Datum: Propeller support flange without spacer. 1337 Datum Reference line W2 * A - W1 * B W1 + W2...

  • Page 72: Weight And Balance

    P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance WEIGHT AND BALANCE To determine the aircraft's CG location and to verify that the CG lies within the predetermined CG travel range, it would be helpful to use the chart in the following page.
  • Page 73 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance MTOW Moment (empty) - Kg m Edition – 29 March 2004...
  • Page 74 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance Fig 6-3 C.G. RANGE CHART Fig 6-4 L OAD POSITION WITH RESPECT TO ATUM Edition – 29 March 2004...

  • Page 75: Loading

    Fig 6-5 C ABIN IMENSIONS EQUIPMENT LIST The following is a comprehensive list of all TECNAM supplied equipment for the P2002-JF. The list consists of the following groups: A - Engine and accessories B - Landing gear C - Electrical system...
  • Page 76 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance EQUIPMENT LIST & kg D ESCRIPTION EIGHT ATUM & NGINE ACCESSORIES Engine Rotax 912S2 - p/n 309.120.133 61.0 0.32 Prop. HOFFMANN -0.13 p/n HO17GHM A 174 177C Exhaust and manifolds - p/n 973670 4.50...
  • Page 77 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance A/C S/N EQUIPMENT LIST & EIGHT ESCRIPTION ATUM LECTRICAL SYSTEM Battery FIAMM 6H4P 12V 18Ah 6.00 2.59 Regulator, rectifier - p/n 945.345 0.20 0.82 Battery relay - p/n 111-226-5 0.30...
  • Page 78 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance EQUIPMENT LIST & EIGHT ESCRIPTION ATUM Vacuum Instr.Ind. Varga Enterprise 0.10 1.35 10-01100 Prop. RPM Ind. Aircraft Mitchell. D1-112- 1.10 1.35 5041 Fuel Quantity Ind. Road GmbH XID4000800 0.56...
  • Page 79 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance EQUIPMENT LIST & EIGHT ESCRIPTION ATUM VOR/ILS Antenna. Command Industries 0.26 5.80 CI 138C ELT Antenna Kit Model E-01 0.21 2.70 Fire Extinguisher Enterprises Ltd 2.20 2.32...
  • Page 80 P2002-JF S E C T I O N 6 LIGHT ANUAL Weight & Balance INTENTIONALLY LEFT BLANK 6-14 Edition – 29 March 2004...
  • Page 81 P2002-JF S E C T I O N 7 LIGHT MANUAL Systems SECTION 7 AIRCRAFT & SYSTEMS DESCRIPTION TABLE OF CONTENTS INTRODUCTION....................2 AIRFRAME ......................2 FLIGHT CONTROLS....................3 INSTRUMENT PANEL ..................4 SEATS AND SAFETY HARNESS................. 5 CANOPY ......................... 5 BAGGAGE COMPARTMENT................

  • Page 82: Introduction

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems INTRODUCTION This section provides description and operation of the aircraft and its systems. AIRFRAME The wing is constructed of a central light alloy torque box; an aluminium leading edge with integrated fuel tank is attached to the front spar while flap and aileron are hinged to rear spar.

  • Page 83: Flight Controls

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems USELAGE The front part of the fuselage is made of a mixed structure: a truss structure with special steel members for cabin survival cell, and a light-alloy semi-monocoque structure for the cabin's bottom section.

  • Page 84: Instrument Panel

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems INSTRUMENT PANEL The conventional type instrument panel allows placement of a broad range of equipment. Instruments marked with an asterisk (*) are optional. Fig. 7-2. INSTRUMENT PANEL ARBURETTOR Carburettor heat control knob is located just to the left of the centre throttle control;...

  • Page 85: Seats And Safety Harness

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems HROTTLE RICTION It is possible to adjust the engine's throttle friction lock by appropriately tightening the friction lock knob located on the instrument panel near the center throttle control.

  • Page 86: Powerplant

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems POWERPLANT ENGINE Manufacturer Bombardier-Rotax GmbH Model ROTAX 912 S2 Type 4 stroke, horizontally-opposed 4 cylinder, mixed air and water cooled, twin electronic ignition, forced lubrication. Maximum rating 98.6hp (73.5kW) @ 5800 rpm/min (2388 rpm/min. prop).
  • Page 87 P2002-JF S E C T I O N 7 LIGHT MANUAL Systems LH FUEL QUANTITY INDICATOR RH FUEL QUANTITY INDICATOR LH FUEL QUANTITY SENSOR RH FUEL QUANTITY SENSOR FUEL VENT FUEL VENT LH FUEL TANK RH FUEL TANK SUMP SUMP...

  • Page 88: Electrical System

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems ELECTRICAL SYSTEM The aircraft's electrical system consists of a 12 Volt DC circuit controlled by the Master Switch located on the instrument panel. Electricity is provided by an alternator and by a buffer battery.
  • Page 89 P2002-JF S E C T I O N 7 LIGHT MANUAL Systems ENERATOR LIGHT Generator light (red coloured) illuminates either: • for a generator failure. • for a failure of the regulator/rectifier, with consequent overvoltage sensor shut off. OLTMETER AND MMETER The voltmeter indicates voltage on bus bar.

  • Page 90: Pitot And Static Pressure Systems

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems Follow this procedure to start the engine using the external power source. 1. Magnetos, Master switch, Generator switch: OFF 2. Open the receptacle door and insert the external power source’s plug into the socket 3.

  • Page 91: Brakes

    P2002-JF S E C T I O N 7 LIGHT MANUAL Systems BRAKES The aircraft's braking system is a single system acting on both wheels of main landing gear through disk brakes, the same circuit acts as parking brake via an intercept valve (2).
  • Page 92 P2002-JF S E C T I O N 7 LIGHT MANUAL Systems INTENTIONALLY LEFT BLANK 7-12 Edition – 29 March 2004...
  • Page 93 P2002-JF LIGHT ANUAL S E C T I O N 8 Ground Handling & Service SECTION 8 GROUND HANDLING & SERVICE TABLE OF CONTENTS INTRODUCTION...................... 2 AIRCRAFT INSPECTION PERIODS............... 2 AIRCRAFT ALTERATIONS OR REPAIRS ............2 GROUND HANDLING..................... 2 CLEANING AND CARE................... 3 Edition –...

  • Page 94: Introduction

    P2002-JF LIGHT ANUAL S E C T I O N 8 Ground Handling & Service 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 95: Cleaning And Care

    P2002-JF LIGHT ANUAL S E C T I O N 8 Ground Handling & Service JACKING Given the light empty weight of the aircraft, lifting one of the main wheels can easily be accomplished even without the use of hydraulic jacks. For an acceptable procedure please refer to the Maintenance Manual.
  • Page 96 P2002-JF LIGHT ANUAL S E C T I O N 8 Ground Handling & Service LEFT INTENTIONALLY BLANK Edition – 29 March 2004...
  • Page 97 P2002-JF LIGHT ANUAL S E C T I O N 9 SUPPLEMENTS SECTION 9 SUPPLEMENTS TABLE OF CONTENTS N° 1: GARMIN GNS 430 GPS/VHF COMM/NAV (5 UPPLEMENT PAGES INTRODUCTION....................2 1.1 GENERAL ....................2 1.2 LIMITATIONS ..................3 1.3 EMERGENCY PROCEDURES ..............4 1.4 NORMAL OPERATION ................

  • Page 98: Introduction

    P2002-JF LIGHT ANUAL S E C T I O N 9 SUPPLEMENTS ° 1 UPPLEMENT N GARMIN GNS 430 GPS/VHF COMM/NAV INTRODUCTION This section contains supplementary information for safe and efficient operation of the aircraft if equipped with a Garmin GNS 430 system.

  • Page 99: 1.2 Limitations

    P2002-JF LIGHT ANUAL S E C T I O N 9 SUPPLEMENTS 1.2 LIMITATIONS 1. The “Pilot’s guide and Reference” p/n 190-00140-00 rev. F dated July 2000 or later versions, must be available for proper use of the instrument. 2. Only VFR use is permitted.

  • Page 100: 1.3 Emergency Procedures

    P2002-JF LIGHT ANUAL S E C T I O N 9 SUPPLEMENTS 1.3 EMERGENCY PROCEDURES If the information provided by the Garmin GNS430 is not available or manifestly wrong, it is necessary to use other navigation instruments. 2. If the message “WARN” appears in the lower left portion of the display, the receiver cannot be considered useful as a navigation aid.

  • Page 101: 1.5 Performance

    P2002-JF LIGHT ANUAL S E C T I O N 9 SUPPLEMENTS 1.5 PERFORMANCE No variations. 1.6 WEIGHT AND BALANCE See section 6 of the present manual. 1.7 SYSTEMS See “GNS 430 Pilot’s Guide” p/n 190-00140-00 rev. F dated July 2000 or later versions, for a complete description of the system.
  • Page 102 P2002-JF LIGHT ANUAL S E C T I O N 9 SUPPLEMENTS LEFT INTENTIONALLY BLANK Edition – 29 March 2004...

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