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NOTE : The Airworthiness Authorities shall be given prior notice of any test flight to allow them to be present if required.
A. Major test flight - refer to 05-30-03
A major test flight shall be performed :
- after each major inspection,
- after a significant repair following an incident,
- after aircraft disassembly and assembly.
B. Minor test flight
A minor test flight is limited to aircraft component(s) modified and shall be performed :
- when the origin of a defect has not been detected or when the correct operation of a system has not been confirmed during ground tests,
- after wing or control surface replacement,
- after engine or propeller replacement,
- after modification of radionavigation or radiocommunication system, particularly after new antenna installation.
AAAA
Validity : S / N 1 - 9999 05-30-00Page 1
(BA) JUN 01
 
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WA
Validity : S / N 1 - 9999 05-30-00Page 2
(BA) JUN 01
 
MAINTENANCE RUN-UP
1. PRELIMINARY INSPECTION (Figure 201) NOTE : Place the aircraft into the wind.
1) Cabin (1)
Pilot door OPEN
Control lock  REMOVED
Magneto selector   OFF
Landing gear lever  DOWN
Mixture   IDLE CUT-OFF
Engine controls   Check deflections
Engine control friction   Checked
Oxygen (if installed)   Check pressure
Fire extinguisher (if installed)   Check pressure
Fuel selector   OPEN (L.H.)
Proceed with the external inspection moving clockwise around the aircraft.
2) L.H. wing (2)
Wing  Free from frost, snow, ice
Pitot   Cover removed, clean, unobstructed
Tie-down  REMOVED
Fuel tank   Check level
Fuel tank cap  SECURED
Fuel tank draining   Fuel free from water and sediment
Fuel tank drain   Check CLOSED
3) L.H. main landing gear (3)
Chocks   INSTALLED
Shock-absorber  Normal position
Door   Check play and cleanliness
M icroswitches   Clean
Landing gear well   No foreign body
4) Forward fuselage (4)
Windshield and window panels   Clean
Engine cowling attachment   Check
Oil   Check level and absence of leak
Propeller   Clean, good condition
Propeller cone   Check (no slack)
Air intakes   Clean
Oil pump breather   Unobstructed
Exhaust pipe   Check
Fuel filter draining   Fuel free from water and sediment
Fuel filter drain   Check CLOSED
ABAA
Validity : S / N 1 - 9999 05 30-01Page 201
(CA) JUN 01
 
5) Nose landing gear (5)
Towing fork   REMOVE
Shock-absorber  Normal position
　
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本文鏈接地址：TB 20 MAINTENANCE MANUAL 05 TIME LIMITS MAINTENANCE CHECKS TB20飛機(jī)維護(hù)手冊(cè) 05 時(shí)間限制維護(hù)檢查 2(73)