AIAA
Validity : S / N 1 - 9999 05 20 05 Page 231
JUN 01
 

ATA "80A" MAJOR INSPECTION
STABILIZER INSPECTION (AREA 300) AREA OTHER
INSPECTION PERFORMED
BY
24-00 14) Visually inspect all cable connections in the vertical stabilizer. 300  
 Replace cables if damaged. Inspect cables for routing, clamp security, lugs and cleanliness.   
27-00 15) Check control surfaces for travel, efficiency and direction of flight controls : 000  
 - pitch - refer to 27-30-00 201,
- elevator trim tab - refer to 27-30-03 501, - rudder - refer to 27-20-00 201,
- rudder trim tab - refer to 27-20-04 201, - roll - refer to 27-10-00 201,
- wing flaps - refer to 27-50-00 501.   
20-00 16) Reinforce the anticorrosion protection - refer to 300  
 20-00-04 201 and lubricate - refer to 12-21-03 201.   

AIAA
Validity : S / N 1 - 9999 05-20-05 ,,A) Page 232
JUN 01
 

ATA "80A" MAJOR INSPECTION
FINAL STEPS AREA OTHER
INSPECTION PERFORMED
BY
 FINAL STEPS 000  
53-00 Post-MOD. 151 200  
 1) Install vertical stabilizer root front fairing 225.   
52-40 All 200  
 2) Install baggage compartment bottom door 242.   
52-40 3) Install landing gear hydraulic generator access door 238L. 200  
25-10 4) Install the sound-proofing panels and the cabin
upholstery panels. 200  
25-10 5) Tilt the instrument panel(s) back into position and install the covers forward of the instrument panel(s). 200  
52-40 6) Install inspection doors 235L, 235R. 200  
25-10 7) Install floor carpets and mats. 200  
25-10 8) Install the rear bench. 200  
25-10 9) Install the front seats and perform an operational test. 200  
 Check locking in all positions.   
24-40 10) Disconnect the external power supply source (if
installed). 200  
24-30 11) Connect the battery, lubricate the terminals - refer
to 24-30-02 201. 000  
52-40 12) Install battery access door 243 (battery at the rear). 200  
 Check that it is correctly locked.   
　
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