曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Perform a magneto check again.
If the RPM drop still exceeds 175 RPM, then abort the mission for further investigations.
D. Check of "Alternate Air" (if installed)
"Alternate Air"   Pulled
Manifold pressure   Maintained
"Alternate Air"   Pushed
E. Engine check
Aircraft equipped with low noise level option
Full throttle (10 sec. maxi)   2500 RPM (+ 0 ; - 20)
Aircraft not equipped with low noise level option
Full throttle (10 sec. maxi)   2575 RPM (+ 0 ; - 20)
All
Idle   750 RPM (+ 100 ; + 0)
Mixture   Mixture control to IDLE CUT-OFF
Idle increase of 20 to 40 RPM
ABM
Validity : S / N 1 - 9999 05-30-02Page 208
(CA) JUN 011
 
F. Air conditioning (if installed)
Circuit breaker   Engaged
Air outlets   Open
Power   > 1200 RPM
Air conditioning switch   "AIR COND"
Wait for 2 to 3 minutes. Check cool air at air outlets.
Air conditioning switch   OFF
Power   700 RPM
6. ENGINE SHUT-DOWN / SECURING AIRCRAFT
Parking brake   Set
Anti-collision lights (if installed)   OFF
Throttle   REDUCED
WARNING : THE TEST HEREAFTER MUST BE IMPERATIVELY CARRIED OUT WITH ENGINE POWER LOWER THAN 1000 RPM ; THE FAILURE TO OBSERVE THIS RULE MAY LEAD TO EXHAUST SYSTEM DAMAGE.
Magneto cut-off test (*)   OFF, then BOTH
Propeller   FULL FORWARD
Throttle   1800 RPM for 15 sec., then 1200 RPM
Mixture   IDLE CUT-OFF
AFTER ENGINE STOPS :
Magneto selector   OFF
Alternator switch-breaker   OFF
Fuel selector   from LEFT to OFF
- Fuel selector warning light   Check ON
Oil pressure warning light   Illuminated
Main switch  OFF
Fuel selector   OFF
Control lock   Installed
Chocks / Tie-downs   Installed
(*) Depending on the kind of operation, it is not necessary to perform this test more than once a day, but just before securing the aircraft.
ABM
Validity : S / N 1 - 9999 05 30 02Page 209
(CA) JUN 01
 
PAGE INTENTIONALLY LEFT BLANK
ABAA
Validity : S / N 1 - 9999 05-30-02Page 210
(CA) JUN 011
 
AIRCRAFT S/N : F : 1/8
Pilot
Date
 
Time
0 - PREFLIGHT INSPECTION Outside and inside checks
Refer to Section 4 of the PILOT'S OPERATING HANDBOOK

L R
Fuel gage level  
ALT 1
Altimeters QFE (hPa)  
ALT 2
Manifold pressure (in.Hg)  

QFU QNH
hPa QFE
hPa OAT
°C Vw
    

1 - ENGINE START
Fuel flow check  
Start - oil pressure  
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飛機維護手冊 05 時間限制維護檢查 2(80)