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 : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Observations........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Owner N°2
Name and adress : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Observations........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Buying date ……………………
Owner N°3
Name and adress : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Observations........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Buying date ……………………
Owner N°4
Name and adress : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Observations........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Buying date ……………………
Owner N°5
Name and adress : ........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Observations........................................................................................................
..........................................................................................................................................................................
..........................................................................................................................................
Buying date ……………………

2008, october, 17

2008, october, 17
SECTION 1 : General points
1-1 Board documents
-he pilot will check before each flight the presence on board of all the necessary
documentation according the local regulations.

2008, october, 17
1-2 3 views drawings
Front view / Vue de Face
1740
2500
2
2
8
0
10050
2
°
Top view / Vue de dessus
Side view / Vue de coté
1500
6100

2008, october, 17
1-3 Design eatures
1-3.1 dimensions :
Wing span 10.05 m
Length 6.09 m
Heigth 2.40 m
Surface 13.92 m²
1-3.2 Landing gear
ricycle, brakes on main gear.
Wheel track width: 1.74 m
Wheel base : 1.50 m
Shock absorbers : Bungee
Alloyed aluminium wheels
yres 4 plys 3.50 x 8
1-3.3 Travel of control surfaces
Elevator : +30° -20°
Ailerons : +43 –20°
Rudder : +/-35°
Elevator trim : +/-35°
Flaps: 10°-20°-35°
1-3.4 Fuel tank
Behind the seats, capacity : l
Hanuman 58 AP and SP : 80 L
Hanuman Jabiru AP :80 L
Hanuman 912 AP: 80 L
Hanuman 912S AP: 80 L
Hanuman Jabiru SP: 60 L
Hanuman 912 SP: 60 L
Hanuman 912S SP: 60 L
1-3.5 Wings
profile NACA 23012
Wings set at : 4° at root
wist : 2°
Dihedral : 2°
Sweep angle 2°
Wing material
Leading edge aluminium ube 64,4x2 mm (Sleeved with 60 x 1,6 )
railing edge aluminium ube 50 x 2 mm (Sleeved with 45,3 x 1.5 )
Compression tubes aluminium ube 38 x 1,6 mm
ension cables 3 mm galva
Wing tip tube aluminium ube 25,4 x 1,6 mm
Wing struts streamlined aluminium Rajhamsa 73 x 28 mm
Battens 20 per wing diam.12,7 x 1,2 mm
Fabric Dacron polyester 170 gr / m²
Ailerons material
Leading edge aluminium ube 38 x 1,6 mm
railing edge aluminium ube 12.7 x 1,2 mm

2008, october, 17
Flaps material
Leading edge aluminium ube 38 x 1,6 mm
railing edge aluminium ube 12,7 x 1,2 mm
1-3.6 Fuselage
cone rectangular section
Material
Main upper and lower tubes aluminium ube 28,6 x 2 mm
Stiffeners aluminium ube 18,6 x 1,1 mm
aluminium ube 12,7 x 1,2 mm
1-3.7 Empennage
Flat profile
Material
Fabric :Dacron polyester 170 gr / m²
Horizontal empennage : Leading edge aluminium ube 25,4 x1,6 mm
railing edge aluminium ube 25,4 x1,6 mm
Vertical empennage : Leading edge aluminium ube 25,4 x1,6 mm
railing edge aluminium ube 25,4 x1,6 mm
1-3.8 Elevator
Flat profile
Material
Fabric :Dacron polyester 170 gr / m²
Leading edge aluminium ube 25,4 x1,6 mm
railing edge aluminium ube 25,4 x1,6 mm
1-3.9 Rudder
Flat profile
Material
Fabric :Dacron polyester 170 gr / m²
Leading edge aluminium ube 25,4 x1,6 mm
railing edge aluminium ube 25,4 x1,6 mm
1-3.10 Seats
Composite with foam
1-3.11 Controls
ype 3 axis
Rudder: action on rudder pedals linked to front wheel with rod end and to rudder with
cables
Handle stick Double between legs
Manette de gaz Double / left hand
Elevator control push pull tube
Aileron control 3 mm cables + push-pull tubes
Flaps control push-pull tubes
1-3.12 Diverse
Bolts: high quality 8.8 bichromated
3 mm stainless plates
powder coated painting

2008, october, 17
1-4 : Settings
he following elements can be subject to adjustment.
Elevator
o adjust the position of the stick relative to the pilot, the elevator control tube has three
holes drilled to allow length adjustment .
Choose the suitable hole and insert the bolt.
Add loctite.
ighten nut to close fit.
Ailerons
uning is achieved by turning the turnbuckles supplied and adjust rod ends.
his will alter the position of the ailerons, which are normally lined up with the wing lower
surface.
If the ailerons have a strong inverse slope (trailing edge higher), the aircraft will tend to
nose up.
If the slope is smaller (trailing edge lower), the aircraft will tend to nose down.
Flaps
Lined up with the wing lower surface.

2008, october, 17

2008, october, 17
SECTION 2 : Limitations
2-1 Certi ication
X-AIR anuman comes under Class 3 of the Ultralight Aircraft Certification of November, the
1rst, 1998, regulating flight authorization of Ultralights.
Certificates stipulated in sections R133-1 and following of the Code de L'Aviation Civile are not
required for ultralights, which are therefore exempted of any certification.
Each ultralight pilot must realize that he, and only he is responsible for the safe operation and
maintenance of his aircraft.
he X-AIR anuman can be used under such varied and diverse conditions that it is impossible
to give strict and all-inclusive instructions for its maintenance.
However, our present experience of the aircraft makes it possible to offer a realistic maintenance
program.
When in doubt, the owner should always seek advice from a competent professional.
Needless to say, we at RANDKAR welcome all your remarks; we will be pleased to answer all
your questions.
2-2 Required pilot competency
Student pilot license and orientation flight
hree-axis ultralight pilot license and further necessary training, as needed (an orientation flight is
mandatory in any case).
2-3 : Flight conditions
Day VFR, no icing conditions
2-4 Load actor
Max loads on controls
Rudder 1380 Newton
Elevator 480 Newton
Ailerons 1300 Newton
Flaps 960 Newton
On airframe
Limit : + 4 G (+6 ultimate)
- 2 G (-3 ultimate)
Warning : Load factor changes when turn
bank: 15° 30° 45° 60° 70°
load factor 1,04 1,15 1,41 2 3

2008, october, 17
2-5 Weight and balance
2-5.1 Empty weight
Basic empty weight (kg) Max. empty weight (kg)
X-air Hanuman Jabiru SP 276 284
X-air Hanuman Jabiru AP
289 306,5
X-air Hanuman 602 SP 263 281
X-air Hanuman 602 AP 276 303,5
X-air Hanuman 912 AP 296 306,5
X-air Hanuman 912 SP 280 284
X-air Hanuman 912S AP 296 305,5
X-air Hanuman 912S SP 284 284
2-5.2 Maximum weight at take-off
Like any aircraft, an ultralight has a maximum take off weight. his must never be
exceeded.
Maximum take off weights:
450 kg for the versions without parachute
472,5 kg for the versions with parachute
he builder will in no circumstances be held liable should these weight limitations be
exceeded whatever the origin or nature of the additional or accessory equipment carried on
the aircraft.
his manual includes all the information required for the use and maintenance of the
aircraft.
his manual is specific to the aircraft it describes, and must be read by all users, as stated
in Parts 1and 2 of June 17, 1986 ruling.
2-5.3 Balance
Calculation method of C. of G.:
Aircraft must be horizontal
Weighing operation must be made with three similar weighing machine located each under
each wheel of the plane
acceptable limit of C G = between 22 to 40,5mm forward from reference point
Reference point : axel of the base tube
Weight ( kg )
Front wheel A
Main gear : left wheel B
Main gear : right wheel C
150 x A
CG = ------------- = ………..
(A+B+C)

2008, october, 17
2-5.4 Changes made to the aircraft
Each owner is required to inform his local authority of any changes made to the aircraft's
characteristics as recorded in its type certificate (engine, propeller or any other part)
according to the local regulations
Added weight for options
OPTIONS Weight Kg lbs
Basic twin float set with fastenings and rudder 45 99,2
Amphibious twin float set with retract gear and fastenings 54 119
Hull with retract gear and sponsons 66 145,5
Snow skis with fastenings 9 19,84
Ballistic parachute with fastenings 12 26,45
Complete agri-spray set with fastenings 37 81,57
Microspray for agri-spraying 18 39,68
Total empty weight of X-AIR anuman is the sum of :
- Aircraft empty weight
- Weight of equipment ( instruments, intercom, radio ... )
- Weight of options
To obtain total loaded weight, you must add :
- Weight of crew ( pilot and passenger )
- Weight of fuel ( 0,72 kg, (1,59 lbs.) / liter )
- Weight of baggages
Total loaded weight must be less than, or equal to 450 kg (992 lbs. )
2-6 Limited speeds
-Maximum speed with flaps position 1 120 Km/h (65 kts)
position 2 110 Km/h (60 kts)
position 3 90 Km/h (48 kts)
- maximum crosswind speed 25 Km/h (13,5 kts)

2008, october, 17