TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飞机维护手册 05 时间限制维护检查 2(52)

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26-20 All 200  
 18) Check the expiry date of the fire extinguisher (if installed).   
 Visually inspect the fire extinguisher and its anchor points.   
 Check nozzle for obstruction - refer to 26-20-01 201.   
26-20 19) Replace the fire extinguisher (if installed). 200 10 years 
21-20 20) Visually inspect the air regulation box(es), the air outlets and the blower (if installed). 200  
21-40 21) Perform an operational test of the air regulation controls, check that in "fire shut-off" position the firewall-mounted box(es) are blanked - refer to 21-00-00 201. 200  
21-55 22) Visually inspect the vapor cycle cooling system (if
installed). 200  
21-55 23) Clean the suction filter and if necessary, the evaporator and the condenser of the vapor cycle cooling system (if installed) - refer to the latest issue of KEITH MM/IPC 200 NOTE 1 
 No. 20-0101 SM.   
21-55 24) Visually inspect the pipes and hoses of the vapor cycle cooling system (if installed) for routing and security. 000  
 Check condition of unions.   

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
ADAA
Validity : S / N 1 - 9999 05-20-06Page 205
(EA) JUN 01
 

ATA ANNUAL INSPECTION (Al)
COCKPIT AND FUSELAGE INSPECTION (AREA 200) AREA OTHER
INSPECTION PERFORMED
BY
24-30 25) Visually inspect (do not remove) the electrical power system (switch-breakers on panel, breakers on side panel, printed circuits on the firewall L.H. door) and (if installed) the Radio-Master-Switch forward of the circuit breaker panel. 200  
 Check fuses, markings, pins, lugs and attach fittings.   
27-50 26) Visually inspect the flap actuator and the supports for cracks. Using a mirror, inspect for cracks on frame C4 -refer to 27-50-01 201. 200 500 hrs 
32-30 27) Visually inspect the landing gear microswitches, electrical wiring and attach fittings - refer to 32-60-01 201,
32-30-07 201. 700 NOTE 1 
24-00 28) Visually inspect all cable connections under the floor, in the rear fuselage, under the instrument panel and on the front table. 200  
 Replace cables if damaged. Inspect cables for routing, clamp security, lugs and cleanliness.   
27-30 29) Remove the servo-actuator of the electrical pitch trim control (if installed). Check setting and inspect for
　
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