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72-30 16) In this case, neither the operation nor the performance of the engine is affected. If the leaks are more serious, replace the cylinder. 100  
12-20 17) Clean the engine - refer to 12-20-03 201. 000  
07-10 18) Jack up the aircraft - refer to 07-10-00 201. 000  
08-10 19) Level the aircraft - refer to 08-10-00 201. 000  
52-40 20) Remove battery access door 243 (battery at the rear), visually inspect for cracks and security. 200  
52-40 21) Remove inspection doors 211L, 211R (if installed),
visually inspect for cracks and security. 200  
24-30 22) Disconnect battery - refer to 24-30-02 201. 000  
24-30 23) Remove the battery. Inspect the battery tray and the shims for condition, cracks and corrosion. 000  
 Install the battery - refer to 24-30-02 201.   
24-30 24) Check battery electrolyte level, condition of lugs and inspect for evidence of oxidation - refer to 24-30-02 201. 000  

AIAA
Validity : S / N 1 - 9999 05 20 05 (JA) Page 202
JUN 01
 

ATA "80A" MAJOR INSPECTION
PRELIMINARY STEPS AREA OTHER
INSPECTION PERFORMED
BY
52-40 25) Check the ground power receptacle door 216L (if
installed) for condition and correct locking, check the location and condition of the label on the door inside (if installed). 200  
24-40 26) Visually inspect the ground power receptacle (if installed) for corrosion and check cable security and connections. 200  
24-40 27) Connect an external power supply source to the ground power receptacle (if installed). Energize. 200  
52-40 28) Remove firewall-mounted inspection doors 212L (partial removal) and 212R (if installed), visually inspect for cracks and security. 200  
52-40 29) Remove and visually inspect inspection doors 235L, 235R. 200  
53-00 30) Remove junction fairings 217R and 217L, visually inspect for cracks and security. 200  
53-00 31) Remove cowlings under hull 218A and 218F, visually inspect for cracks and security. 200  
53-00 Post-MOD. 151 200  
 32) Remove and visually inspect fairings of retractable
footsteps 2111L and 2111R.   
52-40 All 200  
 33) Remove and check condition of inspection doors 213L, and (if installed) 214 and 213R.   
52-40 34) Remove and check condition of baggage compartment bottom door 242. 200  
53-00 35) Remove and visually inspect tail cone 222 for cracks and security. Check condition of tail cone electrical wiring (if installed) - refer to 53-20-00 201. 200  
　
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