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Flight Manual

             

ASK 21 Mi

           Flight Manual

 

 

(2) Oxygen

 

       
For reasons of space, due to the incorporation of the power-plant and 
the fuselage tank, only one oxygen bottle can be accommodated in the 
ASK 21 Mi, in the baggage compartment. The oxygen bottle fixtures are 
only supplied as optional extra and are not provided as standard equip-
ment. 
After fitting the oxygen bottle the pilot must make sure that it is securely 
seated and that the pin at the front mounting fixture is secured. 

Note:

 

Fitting of an oxygen system changes the empty 
mass (weight) C.G. position! 

 

Warning:

 

Fuel can ignite itself through pure oxygen. 

 
 

(3) Emergency Location Transmitter 

 
The least vulnerable location in case of accident is the area between the 
two drag spar pins at either side of the fuselage. 
 
Therefore, the emergency location transmitter (ELT) should be fitted, in 
an appropriate mounting, in the compartment behind the spar tunnel 
(e.g. to the left fuselage wall. Control linkage elements and the access 
to or ventilation of electric components on the floor must in no case be 
impaired.  
 
Depending on the model of the ELT further possible mounting positions 
are the fuselage wall above the opening to the wing leading edge bag-
gage compartment, or - in an appropriate mounting - the cross tube at 
the rear instrument panel carrier. 
 
Since the center fuselage section contains carbon fibre layers - and car-
bon screens the aerial radiation - the ELT aerial must be fixed in the 
canopy area. Yet the aerial must not be fitted direct to the canopy as it 
would be separated from the unit in case of a canopy jettisoning 
 

 
Issue:   

01.12.2007   mh / mg / mm 

Revision: 

7.29

 

Summary of Contents for ASK 21 Mi

Page 1: ...n the two drag spar pins at either side of the fuselage Therefore the emergency location transmitter ELT should be fitted in an appropriate mounting in the compartment behind the spar tunnel e g to th...

Page 2: ...Flight Manual ASK 21 Mi Flight Manual Fig 7 8 1 Fuel System Issue 01 12 2007 mh mg mm Revision 7 30 TN 4 09 09 09 M M nch...

Page 3: ...Tankgeber Fuel indicator 6001 04P 6001 04P 6001 04P 6001 04P Einspritzventil Injection valve Druckregler Pressure regulator Kraftstofffilter Fuel filter Kraftstoffpumpen Fuel pumps Drainerventil Drain...

Page 4: ......

Page 5: ...rve the torque moments 3 Examine the elastic tensioning cords of the engine compartment doors Replace if damaged 4 With the propeller retracted the drive belt allows access to the guide pulleys 36 che...

Page 6: ...more time than retracting replace the gas strut This must be tested with a sufficiently charged engine battery 15 Examine the rubber elements of the power plant suspension mounting for cracks and othe...

Page 7: ...emission 7 3 4 After 150 hours 1 Inspect the engine in accordance with the Engine Manual 2 Dismount the exhaust silencer and remove the fairing Inspect the silencer visually for damages Inspect the c...

Page 8: ...ompartment wherever access is possible with the power plant installed 4 Check the fuel level indicator hose at the fuselage tank every year for leaks and for condition 7 3 6 After 3 Years 1 Inspection...

Page 9: ...O O O O O Check engine compartment door hinges for firm seat or cracks O O O O O O Check propeller stop block for function If required replace O O O O O O Check retighten the 4 lateral set screws at...

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