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

(5) Install the filler cap.
(6) Close the access panel in the cowling.
AIRCRAFT
DA 40 Series
AMM
Servicing
Doc # 6.02.01
Rev. 5 12-10-00 Page 7
20 Sep 2007
B. Change the Engine Oil in the TAE Engine
Detail Steps/Work Items Key Items/References
(1) Remove the engine cowlings. Refer to Section 71-11.
(2) Remove the engine oil drain plug. On the crankcase, lower left. Remove
the lock-wire.
(3) Drain the engine oil with the engine warm. Use a suitable container to catch the oil.
(4) Visually check the engine oil for coolant. No coolant allowed in oil.
(5) Install the engine oil drain plug.
S Tighten the drain plug.
S Lock the drain plug with lock-wire.
Use a new seal washer (TAE part no.
02-7250-03126R1).
CAUTION: USE ONLY THE CORRECT ENGINE OIL. REFER TO CHAPTER 2 OF
THE AIRPLANE FLIGHT MANUAL FOR THE CORRECT ENGINE OIL
SPECIFICATIONS. IF YOU DO NOT USE THE CORRECT ENGINE
OIL, THE ENGINE CAN BE DAMAGED.
(6) Fill the engine with new engine oil to the
maximum level.
(7) Do an engine run. Until the oil temperature is above 80 °C.
(8) Check oil level and refill as necessary. Refer to Paragraph A above.
(9) Check for leaks, specially at the drain plug.
(10) Install the engine cowlings. Refer to Section 71-11.
AIRCRAFT
Servicing DA 40 Series
AMM
Page 8
20 Sep 2007 12-10-00 Doc # 6.02.01
Rev. 5
5. Gearbox Oil (TAE Version only)
WARNING: ENGINE OPERATION WITH NO GEARBOX OIL (OR VERY LOW OIL
LEVEL) WILL CAUSE ENGINE MALFUNCTION OR FAILURE.
The gearbox oil quantity is 1 liter (1.06 US qts). The gearbox oil level can be checked through an oil
level window at the front side of the engine.
A. Replenish the Gearbox Oil System
CAUTION: IF THE GEARBOX OIL LEVEL IS LOW THE REASON MUST BE
DETERMINED AND THE PROBLEM MUST BE CORRECTED BY
AUTHORIZED PERSONNEL. REFER TO TAE SERVICE BULLETIN NO.
125-0003.
Detail Steps/Work Items Key Items/References
(1) Remove the engine top cowling. Refer to Section 71-11.
(2) Remove the gearbox oil filler plug. At the top of the gearbox. Remove the
lock-wire.
CAUTION: USE ONLY THE CORRECT GEARBOX OIL. REFER TO CHAPTER 2
OF THE AIRPLANE FLIGHT MANUAL FOR THE CORRECT
GEARBOX OIL SPECIFICATIONS. IF YOU DO NOT USE THE
CORRECT GEARBOX OIL, THE ENGINE CAN BE DAMAGED.
(3) Refill gearbox oil. Check level through oil level window.
(4) Install the gearbox oil filler plug:
S Tighten the plug.
S Lock the plug with lock-wire.
Use a new seal washer.
(5) Install the engine top cowling. Refer to Section 71-11.
AIRCRAFT
DA 40 Series
AMM
Servicing
Doc # 6.02.01
Rev. 5 12-10-00 Page 9
20 Sep 2007
B. Change the Gearbox Oil
Detail Steps/Work Items Key Items/References
(1) Remove the engine cowlings. Refer to Section 71-11.
(2) Remove the gearbox oil drain plug. At the bottom of the gearbox. Remove
the lock-wire.
(3) Drain the gearbox oil with the engine warm. Use a suitable container to catch the oil.
(4) Install the gearbox oil drain plug:
S Tighten the drain plug.
S Lock the drain plug with lock-wire.
Use a new seal washer (TAE part no.
02-0710-07191R1).
(5) Remove the gearbox oil filler plug. At the top of the gearbox. Remove the
lock-wire.
CAUTION: USE ONLY THE CORRECT GEARBOX OIL. REFER TO CHAPTER 2
OF THE AIRPLANE FLIGHT MANUAL FOR THE CORRECT
GEARBOX OIL SPECIFICATIONS. IF YOU DO NOT USE THE
CORRECT GEARBOX OIL, THE ENGINE CAN BE DAMAGED.
(6) Fill the engine with 1 liter (1.06 US qts) of new
gearbox oil.
Check level through oil level window.
(7) Install the gearbox oil filler plug:
S Tighten the plug.
S Lock the plug with lock-wire.
Use a new seal washer.
(8) Do an engine test run. Refer to Section 71-01, Paragraph 3.
(9) Check oil level through oil level window. Refill as
necessary.
Refer to steps (5) to (7) above.
(10) Check for leakage, specially at the drain plug and
filler plug.
(11) Install the engine cowlings. Refer to Section 71-11.
AIRCRAFT
Servicing DA 40 Series
AMM
Page 10
20 Sep 2007 12-10-00 Doc # 6.02.01
Rev. 5
6. Coolant (TAE Version only)
WARNING: ENGINE OPERATION WITH NO COOLANT (OR VERY LOW COOLANT
LEVEL) WILL CAUSE ENGINE MALFUNCTION OR FAILURE.
The coolant capacity is 6 liters (6.3 US qts). A coolant level sensor is installed in the coolant tank at
the top rear of the engine. It operates the WATER LEVEL caution light in the Auxiliary Engine Display
(AED). Refer to Section 75-01 for more details about the coolant system.
A. Replenish the Coolant System
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：鉆石40系列AMM 1(69)