Page 1 Airplane Flight Manual XA42 S/N: Manufacturer: XtremeAir GmbH _________________ Harzstraße 2 Registration: Am Flughafen Cochstedt ___________________ 39444 Hecklingen Document Number: Germany AFM-XA42-0040-002-A.01 This Manual includes the material required to be furnished to the pilot by EASA regulations and additional informations provided by the manufacturer and constitutes the EASA approved Flight Manual.
Page 3 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Intentionally left blank Page Page date: 24.01.2011...
Page 5 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 LOG OF REVISIONS Issue Date Approved A.01 27.01.2011 Page date: Page 24.01.2011...
Page 7 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 LOG OF EFFECTIVE PAGES Issue Cover and l A.01 II and III A.01 lV and V A.01 VI and VII A.01 Vlll and Chapter 01, Page 1 A.01 Chapter 01, Page 2 and Chapter 01, Page 3 A.01...
Page 8: Table Of Contents
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 TABLE OF CONTENTS LOG OF REVISIONS ......................II LOG OF EFFECTIVE PAGES ....................III TABEL OF CONTENTS ......................IV INTRODUCTION ........................ VI NOTES ..........................VI WARNINGS; CAUTIONS AND NOTES ................VII GENERAL ......................1-01 DESCRIPTION ......................1-01 SPECIICATION OF CATEGORY ..................
Page 9 CENTER OF GRAVITY CALCULATION (SAMPLE) ............2-06 LOADING WEIGHTS AND MOMENTS ................. 3-06 WEIGHTS AND MOMENTS LIMITS ................4-06 EUIPMENT LIST XA42 S/N:101 .................. 5-06 DESCRIPTION AND OPERATION OF AIRCRAFT AND SYSTEMS ....... 1-07 AIRCRAFT ........................ 1-07 FUSELAGE ....................... 1-07 WING ........................
Page 10: Introduction
Amendments, which affect the airworthiness of the aircraft will be announced in the mandatory Service Bulletins issued by the manufacturer XtremeAir GmbH coming along with the "Airworthiness Directive" (AD) publication issued by the EASA. The owner is responsible for incorporating prescribed...
Page 11: Warnings; Cautions And Notes
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 WARNINGS, CAUTIONS AND NOTES The following definitions apply to Warnings, Cautions, and Notes: WARNING Operating procedures, techniques, etc., which could result in personal injury or loss of life if not carefully followed. CAUTION Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed.
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Page 15: General
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 GENERAL DESCRIPTION The XA42 is a two-seat, high performance acrobatic tailwheel airplane. The structure is manufactured from carbon/honeycomb sandwich. SPECIFICATION OF CATEGORY The aircraft is certified in the Utility and Acrobatic category according to EASA CS-23.
Page 17: Technical Data
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 TECHNICAL DATA 1.4.1 3 VIEW DRAWING All dimensions in millimeters Page date: Page 24.01.2011 Chapter 01...
Page 19 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 1.4.2 MAIN DATA Length overall 6670 mm Height overall (ground attitude) 2542 mm Span 7500 mm Wheel base 4425 mm Wheel track 2000 mm 1.4.3 WING Wing plan form Trapezoid Wing span 7500 mm Wing area 11.25 m²...
Page 20: Engine
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 1.4.7 VERTICAL TAIL (INCLUDING RUDDER) Plan form: Trapezoid Height: 1100 mm Area: 1.54 m² Airfoil: DU86-MOD1 1.4.8 RUDDER Height: 1400 mm Area: 0.82 m² Deflection: ± 30 ° ENGINE Manufacturer: Lycoming Engines, Williamsport, PA 17701, USA...
Page 21: Oil
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Maximum sump capacity: 15.15 l / 16 US qt Minimum sump capacity: 8.52 l / 9 US qt Average Ambient Air Temp. Mil-L6082 grades Mil-22851 ashless dispersant grades All temperatures SAE 15W50 or 20W50 > 27°C (80°F)
Page 23 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Secondary Terminology Feet per minute Feet (1 ft = 304.8 mm) Inch (1 in = 25.4 mm) Meter Liter US gal US (liquid) gallon (1 US gal = 3.79 Liter) US quartt US (liquid) quart (1 US qt = 0.946 Liter)
Page 25: Conversion Table
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 1.13 CONERVERSION TABLE km/h km/h 1000 1230 1500 1640 2000 2051 2500 2461 3000 2871 3500 1067 1000 3281 4000 1219 1125 3691 4500 1372 1250 4101 5000 1524 1375 4511 5500 1676 1500 4921...
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Page 29: Limitations
NOTE In case of an XA42 is equipped with specific options additional information required for safe operation will be contained in chapter 9. Instrument markings and placards are provided for the acrobatic category only; for utility category refer to corresponding limitations.
Page 30 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 WARNING For acrobatic flights the wing tanks must be empty. Total fuel capacity - Acro: 65 l / 17.1 US gal Usable fuel capacity - Acro: 64 l / 16.9 US gal 2.4.2 ENGINE LIMITATIONS •...
Page 31: Propeller
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 PROPELLER MT-Propeller MTV-9-B-C/C203-20d, 3-blade hydraulic constant speed RPM limits Max. takeoff: Acrobatic 2700 rpm Utility 2670 rpm Max. continuous: 2500 rpm WEIGHT LIMITS Maximum empty weight • Utility: 670 kg / 1477 lbs • Acro:...
Page 32: Acrobatic Maneuvers
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 ACROBATIC MANEUVERS 2.8.1 UTILITY FLIGHT All acrobatic maneuvers are prohibited except the following: • Stall • Chandelle • Lazy eight • Steep turns 2.8.2 ACROBATIC FLIGHT The airplane is certified in the acrobatic category and capable of unlimited acrobatics.
Page 33: Load Factors
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Recommended entry speeds (IAS) Maneuvers Symbol Remarks Min. kts / km/h Max. kts / km/h Snap roll 80 / 148 174 / 322 Tail slide 100 / 185 225 / 417 Spin Inverted spin Knife edge >...
Page 35: Flight Crew Limits
The structure is qualified up to 72 °C / 161 °F. Flying with structural temperature above 72 °C / 161 °F is prohibited. To avoid high temperatures, paint colours have to comply with XtremeAir´s color specification for composite structure. 2.14 MAXIMUM OPERATING ALTITUDE The certified maximum operating altitude is 15.000 ft / 4572 m MSL.
Page 37 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 2.17.2 OPERATING PLACARDS Callsign placard on the instrument panel (example only): On right cockpit wall: Near eyeball air vents On right cockpit wall: Below compass: Steer Steer DATE VHF ON/OFF AIRPATH On right cockpit wall...
Page 38 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 On right cockpit wall: For aircraft with Airspeed indicators in knots On baggage compartment: Near fuselage and Wing tank drains: On oil inspection flap For aircraft with Airspeed indicators in km/h Near smoke refill connector...
Page 39 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 2.17.3 INSTRUMENT MARKINGS Airspeed indicator green arc 54 kts / 99 km/h to 185 kts / 342 km/h yellow arc 185 kts / 342 km/h to 225 kts / 417 km/h red line 225 kts / 417 km/h...
Page 41: Kinds Of Operation Equipment List
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 2.18 KINDS OF OPERATION EQUIPMENT LIST The aircraft may be operated under VFR day conditions when the appropriate equipment is installed and operable. If icing conditions occur flying is prohibited. To meet certification standards, the following equipment and systems must be installed and operable:...
Page 42 For airplanes that are registered in the United States, the FAR Part 91 “General Operating and Flight Rules” prescribes each occupant to wear an approved parachute when performing acrobatic maneuvers. XtremeAir GmbH highly recommends wearing an approved parachute during all flights. Page EASA approved...
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Page 45: Emergency Procedures
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 EMERGENCY PROCEDURES INTRODUCTION 3.1.1 GENERAL This section contains the checklist and procedures coping with emergencies that may occur. This checklist must be followed in emergencies to ensure maximum safety for the crew and/or aircraft. The knowledge of these procedures will enable the aircrew to better cope with an emergency. The steps should be performed in the listed sequence.
Page 47: Air Speeds For Emergency Operation
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 AIR SPEEDS FOR EMERGENCY OPERATION Stall speed 54 KIAS / 100 km/h Engine failure after takeoff 80 KIAS / 150 km/h Best recommended gliding speed (glide angle 1:7) • Utility - 999 kg 80 KIAS / 150 km/h •...
Page 49 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 (3.3.3 continued) Engine restart in flight: Propeller control Fine pitch PUSH Electric fuel pump Mixture PUSH FULL RICH Throttle 5 (mm) open ADJUST Starter (only if propeller is stopped!) ENGAGE 3.3.4 OIL SYSTEM MALFUNCTION Low oil pressure:...
Page 51: Forced Landings
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 3.3.6 ENGINE MALFUNCTIONS High cylinder head temperature: Mixture PUSH FULL RICH Power REDUCE Flight with reduced power CONTINUE Sudden loss of power: Mixture PUSH FULL RICH Electric fuel pump Fuel capacity of tank selected CHECK...
Page 52: Fires
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Final and landing: Approach speed 80 KIAS / 150 km/h Glide angle with speed CONTROL After touchdown APPLY BRAKES 3.4.2 PRECAUTIONARY LANDING WITH ENGINE POWER Proceed like short field landing; additionally in short final MASTER SWITCH OFF.
Page 53: Unitentional Spin
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 UNINTENTIONAL SPIN Standard procedure for spin recovery: Throttle IDLE Elevator and aileron NEUTRAL Rudder against direction of rotation APPLY After rotation stops: Rudder NEUTRAL Aircraft RECOVER FROM DIVE BAIL-OUT Speed REDUCE below 100 kts Mixture...
Page 54: Lightning Strike
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 3.11 LIGHTNING STRIKE In case the aircraft gets struck by a lightning: Engine / Propeller Vibration REDUCE RPM if necessary Airspeed REDUCE TO 110 kts Load factors AVOID higher loads than + 1,2 / 0,8G...
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Page 57: Normal Procedures
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 NORMAL PROCEDURES GENERAL 4.1.1 AIRSPEEDS FOR NORMAL OPERATION Operation IAS kts IAS km/h Climb out after take-off Cruise climb 90 to 160 160 to 300 Best climb rate (V Best angle of climb (V Normal approach Approach for short field landing 4.1.2...
Page 58: Checklist Procedures
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 CHECKLIST PROCEDURES A) Cockpit, Canopy AFM and legal documents CHECK ON BOARD Ignition, Master switch Clear of foreign objects CHECK Baggage compartment CHECK Front seat harness SECURED Controls free movement CHECK Throttle free movement CHECK...
Page 59 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Tyre wear CHECK G) Right rear fuselage Fuselage skin for damage CHECK Static port clean? CHECK H) Right wing trailing edge Spade and spade arm CHECK Aileron linkage CHECK Wing trailing edge and skin for damage...
Page 60 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Ignition cables and spark plugs CHECK Wiring CHECK Engine actuator cables to freedom of movement CHECK Oil and fuel system for leaks CHECK Cowling CLOSE M) Propeller Blades to damage CHECK Hub to damage and oil leaks...
Page 61: Starting Procedures
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 STARTING PROCEDURES Startup: Canopy CLOSED and LOCKED Straps ATTACH and TIGHTEN Fuel selector switch to ACRO tank SWITCH Avionic switch OFF CHECK Master switch Propeller control PUSH FINE PITCH Mixture PUSH FULL RICH Throttle FULL OPEN Electric fuel pump ON 3 sec.
Page 63: Takeoff Procedures
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 TAKEOFF PROCEDURES 4.6.1 BEFORE TAKEOFF Run-up: Canopy closed and locked CHECK Straps TIGHTEN Fuel selector to fuselage tank CHECK Fuel capacity CHECK Electric fuel pump Engine instrument readouts in the GREEN CHECK Mixture PUSH FULL RICH...
Page 65: Climb
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 CLIMB Takeoff power: Acrobatic: RPM max. 2700 rpm ADJUST Utility : RPM max. 2670 rpm ADJUST Manifold pressure AS REQUIRED Airspeeds: Normal climb 120 kts / 220 km/h Best rate of climb 90 kts / 167 km/h...
Page 67: Shutdown
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 4.9.3 GO AROUND Throttle FULL OPEN Airspeed 80 kts / 150 km/h 4.9.4 NORMAL LANDING Approach speed 80 kts / 150 km/h Three point attitude TOUCHDOWN Elevator pulled DECELERATE 4.9.5 LANDING IN CROSSWIND Approach speed...
Page 69: After Leaving The Aircraft
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 4.11 AFTER LEAVING THE AIRCRAFT 4.11.1 SHORT TIME PARKING Nose in the wind TURN Wheels with chocks SECURE 4.11.2 LONG TIME PARKING Fuel selector switch Wheels with chocks SECURE Aircraft at tie down points TIE DOWN...
Page 71 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 4.12.2 MANEUVERS Utility category: Stall: Level and accelerated stalls up to MTOW, Airspeed and G-limits in the Utility category are to be respected. Chandelle: Airspeed and G-limits in the Utility category must be respected. Lazy eight: Airspeed and G-limits in the Utility category must be respected.
Page 73 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 4.12.3 SPIN Spin entry: Airspeed REDUCE At reaching stall speed: Rudder to desired direction of spin APPLY Aileron NEUTRAL Elevator PULL The aircraft falls in a stable spin. The loss of altitude for 6 turns of standard spin (rudder deflected, aileron neutral, elevator pulled, power off) is about 2300 ft.
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Page 77: Performance
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 PERFORMANCE GENERAL Performance data charts on the following pages are presented to facilitate the planning of flights in detail and with reasonable accuracy under various conditions. The data in the charts have been computed from actual flight tests with the aircraft and engine in good condition and using average piloting techniques.
Page 79: Isa Conversion
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 ISA CONVERSION ISA Conversion of pressure altitude and outside air temperature are shown in the following figure. Page date: Page 24.01.2011 Chapter 05...
Page 81: Airspeed Calibration
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 AIRSPEED CALIBRATION Indicated airspeed assumes zero instrument error. STALL SPEED Below 60 kts IAS the control’s sensibility decreases and the stall is announced by a slight shudder 6 kts before stalling. While executing power-on stalls the aircraft starts to wiggle around the pitch and roll axis. Deck angle is around 70°...
Page 82: Take-Off Performance
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 TAKE-OFF PERFORMANCE The mentioned take-off distances are valid for a hard surface runway, clean aircraft and no wind. For other conditions, use following factors: 10 kts headwind distances are reduced by 15 % Wind: 20 kts headwind...
Page 83 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 5.5.2 TAKE-OFF DISTANCES FOR ACROBATIC CATEGORY TAKE-OFF WEIGHT 850 kg Conditions: Lift-off speed 70 KIAS / 130 km/h Speed over 50 ft obstacle V 80 KIAS / 150 km/h Power setting full throttle, 2700 rpm...
Page 85: Rate Of Climb Performance
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 RATE OF CLIMB PERFORMANCE Speed for best rate of climb 90 kts / 167 km/h Speed for best angle of climb 78 kts / 145 km/h Climb rate in ft/min for best rate of climb...
Page 87: Landing Performance
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 LANDING PERFORMANCE The mentioned landing distances are valid for a hard surface runway, clean aircraft and no wind. For other conditions, use following factors: 10 kts headwind distances are reduced by 15 % Wind: 20 kts headwind...
Page 89 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 850 kg Landing weight Pressure altitude Distance Temperature °C ISA +10 ISA +20 ISA +30 Landing run 0 / SL over 50 ft obstacle Landing run 1000 over 50 ft obstacle Landing run 2000 over 50 ft obstacle...
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Page 91: Weight & Balance
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 WEIGHT & BALANCE AND EQUIPMENT LIST GENERAL This section describes the procedure for establishing the basic weight and moment of the aircraft. Sample forms are provided for reference. Procedures for calculating the weight and movement for various operations are also provided.
Page 93: Center Of Gravity Calculation (Sample)
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 6.2.1 OWNERS WEIGHT AND BALANCE RECORD Enter all weight change data from aircraft log book in the table below. XA42 S/N: Weight change Operational empty weight Added (+), Removed (-) Description of Date modification Weight...
Page 95: Loading Weights And Moments
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 LOADING WEIGHTS AND MOMENTS The maximum number of occupants is 2. Pilot (rear seat) Copilot (front seat) Weight Occupant + Parachute Arm = 1,73 m / 68.1 in Arm = 0,86 m / 33.86 in...
Page 96: Weights And Moments Limits
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 WEIGHTS AND MOMENTS LIMITS Example: At 900kg (1984 lbs) and 56700 kgcm (49203 in lbs) CG Location is 63 cm (24,8 in) aft of Reference Datum. UTILITY FLIGHT Maximum takeoff Forward CG Rear CG weight...
Page 97 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 EQUIPMENT LIST XA42 S/N: ____ Part or P/N Weight Required (R) Item Manufacturer (kg) Optional (O) Engine Lycoming Engines AEIO-580-B1A 202.30 -0.61 Magneto LH Slick 6350 2.00 -0.15 Magneto RH Slick 6393 2.30 -0.15 Slick Start...
Page 99 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Part or P/N Weight Required (R) Item Manufacturer (kg) Optional (O) Ampere Shunt Westach 237-30 0.09 +1.15 Tachometer Noris Automation NIR2-060-FG-476 0.15 +1.15 RPM Sensor 420815-1 0.05 -0.18 Magnetic Compass front Airpath C-2300 0.25 +1.15...
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Page 103: Description And Operation Of Aircraft And Systems
AIRCRAFT The XA42 is designed and manufactured by XtremeAir GmbH, Harzstraße 2, Am Flughafen Cochstedt, 39444 Hecklingen, Germany, in accordance with the EASA CS-23, categories utility and acrobatic, to fulfill normal operations and acrobatic flying up to the Unlimited aerobatic level.
Page 104: Empennage
FLIGHT CONTROL SYSTEM 7.5.1 PRIMARY CONTROL SYSTEM The XA42 is standard equipped with conventional control stick and adjustable rudder pedals. The primary control surfaces are operated through direct mechanical linkages. 7.5.2 LONGITUDINAL FLIGHT CONTROL SYSTEM The elevator is actuated via a conventional control stick.
Page 105: Instrumentation
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 INSTRUMENTATION 7.6.1 INSTRUMENT PANEL For instrumentation of the instrument panel refer to the following figure. The table below shows whether the instruments are standard or optional equipment. Fig. 7.6.1 cockpit 10 30 18 19b 20 & 21...
Page 107 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Instrument Position Standard Optional Air speed indicator Magnetic direction indicator Altimeter Tachometer Oil temperature / oil pressure EGT scanner Manifold pressure Fuel pressure Volt-Ampere meter G-Meter Clock Prop Mixture Radio Transponder Fuel capacity indicator Fuel Selector Valve...
Page 108: Landing Gear
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 Fig. 7.6.3 Instrument Panel front Instrument Position Standard Optional Air speed indicator Magnetic direction indicator Altimeter Throttle PTT button LANDING GEAR Landing gear is a taildragger configuration made out of spring steel. Tail wheel is a swivel-mounted solid rubber wheel.
Page 109: Canopy
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 CANOPY The canopy is one single part that is hinged on the right hand side via 3 integral hinges equipped with brass bushings to the fuselage and locked on the left hand side of the aircraft. The lock is redundant as there are three bolts moving in opposite directions.
Page 110 Airplane Flight Manual XA42 7.10.2 OIL SYSTEM The oil is cooled by a two oil coolers mounted on the left and right hand side in the engine compartment. The oil level is determined by a dipstick. A thermostatic valve is fitted upstream of the oil cooler.
Page 111: 7.11 Fuel System
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 7.11 FUEL SYSTEM 7.11.1 GENERAL The fuel system consists of two separate wing tanks and one acro tank. For utility flights all the tanks may be used. During acrobatic flights the wing tanks must be empty. The total volume of all three tanks is 275 L / 72.5 US gal.
Page 113: 7.12 Electrical System
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 7.11.2 FUEL SELECTOR VALVE FUEL SELECTOR VALVE The fuel selector can be operated from the rear cockpit (pilot). There is no access from the front The fuel selector can be operated from the rear cockpit (pilot). There is no access from the front The fuel selector can be operated from the rear cockpit (pilot).
Page 115: 7.14 Baggage Compartment
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 7.14 BAGGAGE COMPARTMENT The baggage compartment is located behind the seat and may carry up to 10 kg / 22 lbs of secured baggage. WARNING The baggage compartment must be empty during acrobatic flying! Before loading the baggage compartment, check CG limits are not exceeded according to weight &...
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Page 119: Introduction
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 HANDLING, SERVICE & MAINTENANCE INTRODUCTION a) The airplane owner should establish contact with the dealer or certified service station for service and information. b) All correspondence regarding the airplane must include its serial number (see type placard).
Page 121: Cleaning And Protection
Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 GROUND HANDLING a) Due to its low weight and the free swiveling tail wheel two persons can easily move the airplane by hand. The best spot to push is the leading edge of the wings; the best spot to pull is the propeller close to the root of the blades.
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Page 125 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 SUPPLEMENTS LOG OF EFFECTIVE PAGES Issue Chapter 09, Page I and Chapter 09, Page 1.1 A.01 Chapter09, Page 2.1 and Chapter 09, Page 2.2 A.01 TABLE OF CONTENT Supplement Title Installed EMERGENCY LOCATION TRANSMITTER TRANSPONDER TRT 800 H...
Page 126 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 EMERGENCY LOCATION TRANSMITTER 9.1.1 GENERAL Emergency Location Transmitter (ELT) intalled is the Kannad 406 AF-COMPACT. This supplement is a permanent part of the handbook and must be used as long as ELT is installed. ELT is self powered by the ELT battery (replacement every 6 years).
Page 127 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 AFM-XA42-0040-002-A.01 TRANSPONDER TRT 800H 9.2.1 GENERAL This supplement contains information for efficient use of the aircraft’s transponder. The Funkwerk Avionics TRT 800H is installed. These informations must be used with the complete manual. This supplement is a permanent part of the manual and must be used as long as the transponder TRT 800H is installed.
Page 128 Airplane Flight Manual XA42 AFM-XA42-0040-002-A.01 - certified to EUROCAE ED-73B and CS-ETSO-2C1 1 2a - maximum flight level 35000 ft, maximum velocity 250 knots - Display information contains code, reply symbol, mode of operation and pressure altitude - temperature compensated high precision piezo-resistive pressure sensor...

XtremeAIR XA42 Flight Manual

1 General

2 Limitations

3 Emergency Procedures

4 Normal Procedures

5 Performance

6 Weight & Balance

7 Description and Operation of Aircraft and Systems

8 Handling, Servicing and Maintenance

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