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25-10 2) Tilt the instrument panel(s) back into position and install the covers forward of the instrument panel(s). 200  
24-40 3) Disconnect the external power supply source (if
installed). 200  
24-30 4) Connect the battery, lubricate the terminals - refer
to 24-30-02 201. 000  
52-40 5) Install battery access door 243 (battery at the rear). 200  
 Check that it is correctly locked.   
52-40 6) Install inspection door 211 R (front battery option). 200  
52-40 7) Install inspection door 214 (if installed). 200  
53-00 Post-MOD. 151 200  
 8) Install retractable footsteps fairings 2111L and 2111R.   
53-00 All 200  
 9) Install cowlings under hull 218A and 218F.   
71-10 10) Install lower engine cowling 131 and upper engine
cowling 121 - refer to 71-10-01 201. 100  
53-00 11) Install rear tail cone 222 - refer to 53-20-00 201. 200  
 12) Check that all cowlings, access doors and fairings are correctly installed. 000  
07-10 13) Lower the aircraft onto ground - refer to 07-10-00 201. 000  
08-10 14) Weigh the aircraft for weight and balance computations - refer to 08-20-00 201. 000 5 years 
 15) Perform a test run-up. Record the parameters (at engine shutdown) - refer to 05-30-02 201. 000  
34-20 16) Perform a compensation of the compass(es) - refer to 34-23-00 201. 200 3 years 
71-10 17) After the test run-up, remove upper engine cowling 121 and lower engine cowling 131, and check for leaks (oil, fuel, air, exhaust gases). 000  
 If everything is normal, reinstall the engine cowlings and
check that they are correctly locked - refer to   
 71-10-01 201.   
 18) Record this inspection in the aircraft maintenance files 000  
 (airframe and engine log books).   

AIM
Validity : S / N 1 - 9999 05-20-04 (JA) Page 218
JUN 01
 
"80A" MAJOR INSPECTION

Registration number Model and Serial number Aircraft operating hours

ATA "80A" MAJOR INSPECTION
PRELIMINARY STEPS AREA OTHER
INSPECTION PERFORMED
BY
 PRELIMINARY STEPS 000  
 1) Record anomalies into log book or equivalent document for corrective action. 000  
 2) Check aircraft compliance with airworthiness directives, service bulletins and service letters - refer to 05-00-021. 000  
　
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