IKARUS FOX C 22 ROTAX 462 GC
ROTAX 462
Engine Clock: 100 Hours at 20160815
Air-frame Clock: Same as above
Propeller make and model: 3 bade fiber
Radio: iCom IC-A23 & Headset included.Hangered: Bundu Airfield @ R750pm
(would be happy to move to Rosslyn Microlighters or open for discussion)
Always been hangered.
ATF: Current - Expiry 20170817
FOR SALE
100% R 90,000.00
or 50% between R30,000 and R50,000 (Terms and Conditions apply)
or 33% between R20,000 and R40,000 (Terms and Conditions apply)
Christopher Riley
083-2694525
chris@notebook.co.za
Sunday 14 August 2016
Saturday 13 August 2016
Thursday 11 August 2016
ZU-CLY Manual
(also see http://www.comco-ikarus.de/Website-Management/UserData/ModuleContents/722/165%20-%20165%20-%2022C_2001_05.pdf)
Handbook of operating limitations and information for Microlight
Handbook of operating limitations and information for Microlight
Zu-CLY
WARNING: this manual is specifically for
the Fox C-22, ZU-CLY
Therefore procedures and limits may not
be applicable to other aircraft.
Appendix
Description page
Description 1
Specifications 2
Operating
procedures 3
Operating
limits 4
Service
hints 5
Equipment
list 6
DESCRIPTION
This Fox C-22 is a strut-braced high
wing airplane powered with a Rotax 462 two-cylinder, 2-stroke, water-cooled engine.
The engine is equipped with a starter and generator for 12-volt operation. The
12-volt storage battery supplies current for starting and identification
lights. The battery is located in the nose of the aircraft
A single control stick is situated between the seats, with
the throttle situated on the outer front sides of both seats. The flap handle
is situated in the roof between the two seats. The hydraulic brakes, situated
on the control stick, control both wheels simultaneously. The wide tread landing
gear with rubber cord shock absorbers and the steerable nose wheel provide
stability and easy manoeuvring on the ground.
The instrument panel
contains the flight instrument, engine instruments, and hand held radio
bracket. The intercom system is located on the floor at the panel base.
The two 25 litre fuel tanks are situated behind each seat.
There are no fuel cocks in the system. Fuel pressure is supplied via a
mechanical fuel pump situated to the
left, rear of the engine. An auxiliary electric fuel pump is also fitted.
FOX C-22 SPECIFICATIONS
H.P.
and RPM 55
@ -6800
Gross
weight 450
kg
Empty
weight 248
kg
Wing
span 9.6
m
Overall
length 5.41
m
Propeller
diameter 72”
Take-off
run (minimum) 55m
Rate
of climb-sea level ft./min. 1000
Cruising
range (miles) 183
Nautical Miles
Service
ceiling 12000
Fuel
consumption Lt./hr - cruising 15
Fuel
capacity, litres 50
Fuel
octane rating unleaded/leaded
Tyre
pressure 1
bar
operating procedures
STARTING:
1.
APPLY CHOKE IF THE
ENGINE IS COLD. (MANUAL CHOKE ON THE
CARB.
2.
SET THE THROTTLE TO
IDLE POSITION.
3.
TURN “MASTER SWITCH”
ON.
4.
MOVE THE MAGNETO
SWITCH TO “ON” POSITION
5.
ENSURE PROP AREA IS
CLEAR OF PEOPLE; ACTIVATE THE STARTER BY TURNING THE KEY FURTHER TO THE RIGHT.
6.
ONCE STARTED OPEN THE
THROTTLE UPTO 1800 rpm.
7.
LET THE ENGINE RUN
FOR A FEW 45 SECONDS, SWITCH THE ENGINE OFF & RELEASE THE CHOKE.
PRE-TAKE
OFF CHECKS:
1.
ENSURE THAT FLIGHT
CONTROLS ARE FULLY OPERATIVE.
2.
CHECK THAT HARNESSES
ARE SECURE.
3.
CHECK THE IGNITION
CIRCUITS (MAGS) AT 4000 rpm. DROP MUST NOT EXCEED 300 rpm
AFTER
TAKE-OFF CHECKS:
1.
CLIMBING WITH THE
ENGINE RUNNING AT MAX. Rpm (6800) IS PERMISSIBLE FOR 5 MINUTES.
2.
OBSERVE COOLANT
TEMPERATURES.
3. LIMITS
MUST NOT BE EXCEEDED. 70°C
ENGINE
OPERATING PROCEDURES:
1. FOR
DETAILED INSTRUCTIONS ON THE ENGINE OPERATING PROCEDURES AND SERVICE INTERVALS
REFER TO THE ROTAX OPERATIONS MANUAL FOR ROTAX 462 UL
FUEL
SYSTEM:
1.
BOTH TANKS FEED
SIMULTANEOUSLY. THERE IS NO FUEL GAUGE FITTED.
COOLANT
1.
COOLANT IS CHECKED BY
REMOVING THE RADIATOR CAP AND OBSERVING THE LEVEL.
2.
USE 50% ANTIFREEZE CONCENTRATE WITH ADDITIVES
AGAINST CORROSION AND 50% WATER.
OPERATING
LIMITATIONS
AIRSPEED:
1. MAXIMUM SPEED (VNE) 66 Knots (RED LINE)
2. CAUTION SPEED - LIMITED OPERATION. 55 Knots TO
66 Knots. (YELLOW ARC ON INDICATOR.)
3. NORMAL OPERATING SPEEDS - 25 Knots TO 55 Knots
(GREEN ARC ON INDICATOR.)
4. ROTATE SPEED 25
Knots
5. BEST CLIMB SPEED 43 Knots
6. APPROACH SPEED: WITH
POWERED 38 Knots
UN-POWERED 43 Knots
7. STALL SPEED MAX WEIGHT POWER 28 Knots
UN-POWERED 30 Knots
8. MANOEUVRING SPEED – MAX 43 Knots
9. MAX CROSS WIND LANDING 13 knots
10.BEST GLIDE 38
Knots
TACHOMETER:
1. MAXIMUM RPM - 6800
(RED LINE ON INSTRUMENT.)
2. CAUTION RPM - LIMITED OPERATION. 6400 Rpm -
6800 Rpm. (YELLOW ARC ON INSTRUMENT.)
3. NORMAL OPERATING RPM – 2000 Rpm TO 6200 rpm
(GREEN ARC)
OIL
TEMPERATURE:
1.
MAXIMUM COOLANT TEMPERATURE - 80’C
(RED
LINE ON GAUGE.)
2.
NORMAL OPERATING TEMPERATURE- 60’- 80’C
1. (GREEN
ARC ON GAUGE.)
WEIGHT:
1.
MAXIMUM CERTIFICATE
WEIGHT - 450 Kg
MANOEUVRES:
NO ACROBATIC MANOEUVRES PERMISSIBLE.
Service
hints
BATTERY:
THE 12 VOLT BATTERY IS LOCATED AFT OF
THE FIREWALL ON THE PASSENGER SIDE, ACCESSIBLE BY REMOVING THE FIREWALL BACK
COWLING.
WINDSHIELD
AND WINDOWS:
USE ONLY GOOD QUALITY SOAP, CLEAN WATER
AND CLEAN WATER AND CLEAN SOFT CLOTHS TO CLEAN THESE AREAS. THE USE OF PATENTED
CLEANERS IS NOT RECOMMENDED BECAUSE OF THEIR POSSIBLE SOLVENT ACTION ON THE
MATERIAL USED IN THE CONSTRUCTION OF THESE PARTS,
EQUIPMENT
LIST:
ALTIMETER
REV COUNTER
COMPASS
AIR SPEED INDICATOR
VERTICAL SPEED INDICATOR
COOLANT TEMPERATURE GAUGE
FLIGHT DURATION METER
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