Rand-Kar X-AIR HANUMAN 602T AP User manual

2008, october, 17
-User’s Manual
Section 1 to 7
-Maintenance Manual
Section 8
-Engine Manual
Annex
X-AIR
« HANUMAN »
X-AIR HANUMAN 602T AP (with Rotax 582 and parachute)
X-AIR HANUMAN 602T SP (with Rotax 582 without parachute)
X-AIR HANUMAN JABIRU AP (with Jabiru 2200 and parachute)
X-AIR HANUMAN JABIRU SP(with Jabiru 2200 without parachute)
X-AIR HANUMAN 912 AP (with Rotax 912 and parachute)
X-AIR HANUMAN 912 SP (with Rotax 912 without parachute)
X-AIR HANUMAN 912S AP (with Rotax 912S and parachute)
X-AIR HANUMAN 912S SP (with Rotax 912S without parachute)
RAND- KAR sa Canal de la Martinière 44320 Frossay - France Tél.: [phone] Fax : [phone]
Société au capital de 46 000 € siret : 384.220.695.00017 RM 44 A E 353 B FR 39.384.220.695
http///www.randkar.fr E-mail : [e-mail] support technique [e-mail]

2008, october, 17
SUMMARY
INTRODUCTION (Pages 5 to 9)
SECTION 1 : General points (Pages 11 to 15)
1-1 On-board documents
1-2 3 views drawings
1-3 Design features
1-3.1 Dimensions
1-3.2 Landing gear
1-3.3 ravel of control surfaces
1-3.4 Fuel tank
1-3.5 Wings
1-3.6 Fuselage
1-3.7 Empennage
1-3.8 Elevator
1-3.9 Direction
1-3.10 Seats
1-3.11 Controls
1-3.12 Diverse
1-4 Settings
SECTION 2 : Limitations (Pages 17 to 19)
2-1 Certification type
2-2 Pilot’s competence
2-3 Use conditions
2-4 Load factor
2-5 Weight and balance
2-6 Limited speeds
SECTION 3 : Powerplant (Pages 21 to 24)
3-1 Jabiru 2200
3-1.1 Manufacturer
3-1.2 echnical datas
3-1.3 Propeller
3-1.4 Noise pollution
3-2 Rotax 582
3-2.1 Manufacturer
3-2.2 echnical datas
3-2.3 Propeller
3-2.4 Noise pollution
3-3 Rotax 912
3-3.1 Manufacturer
3-3.2 echnical datas
3-3.3 Propeller
3-3.4 Noise pollution

2008, october, 17
SECTION 4 : Per ormances (Pages 25 to 27)
4-1 X-AIR Hanuman Jabiru
4-1.1 Service ceiling
4-1.2 ake off distance
4-1.3 Climb
4-1.4 Speeds
4-1.5 Engine off
4-1.6 Landing
4-2 X-AIR Hanuman 602 (Rotax 582)
4-2.1 Service ceiling
4-2.2 ake off distance
4-2.3 Climb
4-2.4 Speeds
4-2.5 Engine off
4-2.6 Landing
4-3 X-AIR Hanuman 912
4-3.1 Service ceiling
4-3.2 ake off distance
4-3.3 Climb
4-3.4 Speeds
4-3.5 Engine off
4-3.6 Landing
SECTION 5 : Standard procedure (Pages 29 to 35)
5-1 Pre-flight inspection
5-1.1 Cockpit
5-1.2 Engine
5-1.3 Airframe
5-2 Installation on board and starting engine
5-2.1 Engine cold
5-2.2 Engine hot
5-3 Check before take-off
5-4 ake-off
5-5 Climb
5-6 urns
5-7 Flight in turbulences
5-8 Stall
5-8.1 Engine off
5-8.2 Full throttle
5-9 Cruise
5-10 Descent, approach, landing
5-11 Crosswind
5-12 Engine stop
5-13 Parking
5-14 Performances

2008, october, 17
SECTION 6 : Emergency procedures (Pages 37 to 40)
6-1 Engine failure, emergency landing
6-1.1 before take-off
6-1.2 on take-off
6-1.3 In flight
6-2 Fire
6-2.1 Engine fire
6-2.2 Cabin fire
6-2.3 Electric cables fire
6-3 Regulator failure
6-4 Landing without elevator
6-5 Emergency landing with engine
6-6 Emergency landing on water
6-7 Emergency landing on trees
6-8 Flight in hard rain
6-9 Flight in icing conditions
6-10 spin
6-11 Use of parachute
SECTION 7 : Accessories and options (Pages 41 to 44)
7-1 using advices
7-1.1 Skis
7-1.2 Floats
7-1.3 Banner
7-1.4 Crop spraying
7-2 Repercussion of options mounting
7-2.1 Skis
7-2.2 Floats
7-2.3 Banner
7-2.4 Crop spraying
7-2.5 Balistic parachute
SECTION 8 : Maintenance (Pages 45 to 55)
8-1 aking down and transport
8-2 Airframe maintenance
8-3 Proppeller
8-4 Powerplant maintenance
8-4.1 Jabiru 2200
8-4.2 Rotax 912
8-4.3 Rotax 582
ANNEX : Engine manu acturer’s manual

2008, october, 17
INTRODUCTION
Dear fellow pilot,
Our congratulations and our thanks, for choosing our new X-AIR anuman Ultralight. We wish you
many pleasant hours of flight.
his maintenance and flight manual will help you achieve safe flying conditions.
Please read it attentively and follow all the instructions concerning assembly, preflight inspection, in-
flight operation and maintenance.
Feel free to contact your dealer for any additional information about your ultralight, and for any remark
you wish to make to improve the quality of this document, the service we can offer, or the general safety
of your flights.
his ultralight is an aircraft, and as such must be flight-tested by a certified instructor. All test flights to
be conducted in still air.
Never forget that you alone are responsible for the safe handling of your X-AIR anuman
Constant vigilance and attentiveness are essential.
Your own safety, the safety of your passenger and other fliers, as well as the future of ultralight flying are
at stake.
Many happy lights!

2008, october, 17
WARNING
Even in the best of conditions, ultralight flying may be hazardous. he user of this ultralight
acknowledges the existence of such hazards.
Before his first flight, the user must pledge to read this manual. He shall follow exactly the instructions
given.
He should be advised that the weight of any additional equipment increases the empty weight of the
aircraft and decreases its useful load accordingly -- since maximum weight cannot be exceeded.
he user pledges to carry out all the mandatory alterations specified in Rand Kar's regular newsletters.
Any alterations or repair other than those specified by the manufacturer, or carried out without the
manufacturer's agreement shall void the warranty.
he user must be a 3 axis licensed Ultralight pilot.
Rand Kar Sarl cannot be held responsible for any incidents or accidents caused by improper assembly, or
reckless use of the ultralight, particularly when flying in bad weather, performing aerobatics maneuvers,
or maneuvers exceeding the flight envelope of the aircraft.
at ............................................................................., Date ..............................................................
Signed
Name and adress : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Aircraft type : ................................................................................................................................
Serial N°: .....................................................................
Engine : ………………………………………………..
EngineN° : ………………………………
Gearbox : ……………………….Gearbox ratio : …………………
Propeller : ………………………………..
Instruments : …………………………..
Other equipements : ………………………

2008, october, 17
TO MAKE WARRANTY EFFICIENT, T IS FORM AVE TO BE RETURNED TO
RAND KAR sa Canal de la Martinière
F - 44320 FROSSAY - FRANCE
WARNING
Even in the best of conditions, ultralight flying may be hazardous. he user of this ultralight
acknowledges the existence of such hazards.
Before his first flight, the user must pledge to read this manual. He shall follow exactly the instructions
given.
He should be advised that the weight of any additional equipment increases the empty weight of the
aircraft and decreases its useful load accordingly -- since maximum weight cannot be exceeded.
he user pledges to carry out all the mandatory alterations specified in Rand Kar's regular newsletters.
Any alterations or repair other than those specified by the manufacturer, or carried out without the
manufacturer's agreement shall void the warranty.
he user must be a licensed Ultralight pilot.
Rand Kar Sarl cannot be held responsible for any incidents or accidents caused by improper assembly, or
reckless use of the ultralight, particularly when flying in bad weather, performing aerobatics maneuvers,
or maneuvers exceeding the flight envelope of the aircraft;
at ............................................................................., Date ..............................................................
Signed
Name and adress : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Aircraft type : X-AIR HANUMAN
Serial N°: .....................................................................
Engine : ………………………………………………..
EngineN° : ………………………………
Gearbox : ……………………….Gearbox ratio : …………………
Propeller : ………………………………..
Instruments : …………………………..
Other equipements : ………………………
his form to be filled and returned to:
RAND KAR sa Canal de la Martinière
F - 44320 FROSSAY - FRANCE
Form to be illed and returned to a ter weighing operation o empty inished aircra t:

2008, october, 17
C.of G calculation method.:
Aircraft must be horizontal
Weighing operation must be done with 3 similar weighing machines located each under every wheel of
the aircraft.
acceptable limit of C G = from 22 to 40,5 (cm)
Weight ( kg )
Front wheel A
Main gear : left wheel B
Main gear : right wheel C
O AL
150 x A
CG = ------------- = --------
(A+B+C)
Date:
Place:
ype of aircraft : X-AIR HANUMAN
Serial Number
Identification sheet:
Max. empty weight :
Owner : Signature :
Form to be illed and returned to a ter weighing operation o empty inished aircra t
to : RAND KAR sa Canal de la Martinière
F - 44320 FROSSAY - FRANCE
Property sheet

2008, october, 17
Owner N°1
Name and adress : ........................................................................................................
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Observations........................................................................................................
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Owner N°2
Name and adress : ........................................................................................................
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Observations........................................................................................................
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Buying date ……………………
Owner N°3
Name and adress : ........................................................................................................
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Observations........................................................................................................
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Buying date ……………………
Owner N°4
Name and adress : ........................................................................................................
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Observations........................................................................................................
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Buying date ……………………
Owner N°5
Name and adress : ........................................................................................................
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Observations........................................................................................................
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Buying date ……………………

2008, october, 17