INTENTIONALLY BLANK
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R Example of How to Use the Decision Tree Figure 205/TASK 05-50-00-991-005- 12 (SHEET 1)
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May 01/03 CES
R Example of How to Use the Decision Tree Figure 205/TASK 05-50-00-991-005- 22 (SHEET 2)
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May 01/03 CES
R Example of How to Use the Decision Table Figure 206/TASK 05-50-00-991-006
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May 01/04 CES 4. Fault Isolation
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A. Corrective Actions Types
(1) Type 1
(a) The cause of vibrations is incorrect rigging of the elevator or/and excessive play at the elevator trailing edges:
- do the procedure: vibrations felt in the rear cabin (Ref. TASK 27-30-00-810-850).
(2) Type 2
(a) The cause of vibrations is the elevator servocontrol oscillations:
- do the procedure: vibrations felt along the cabin and in the cockpit (Ref. TASK 27-30-00-810-849).
(3) Type 3
(a) The cause of vibrations is excessive play at the aileron trailing edges:
- do the procedure: vibrations felt in the forward cabin and cockpit (Ref. TASK 27-10-00-810-835).
(4) Type 4
(a) The cause of vibrations is the aileron servocontrol oscillations:
- do the procedure: aileron oscillations (Ref. TASK 27-10-00-810-840).
(5) Type 5
(a) The cause of vibrations is excessive play at the rudder trailing edge:
- do the procedure: vibrations felt in the rear cabin and along the fuselage (Ref. TASK 27-20-00-810-802).
(6) Type 6
(a) The cause of vibrations is abnormal condition of the flap (1):
- do the procedure: flap vibration (Ref. TASK 27-54-00-810-801).
(7) Type 7
(a) Not applicable
(8) Type 8
(a) The cause of vibrations is excessive play in the NLG aft door gimbal joints:
- do the procedure: vibrations felt during climbs caused by abnormal clearance of the aft nose landing-gear doors (Ref. TASK 32-20-00-810-803).
(9) Type 9
(a) The cause of vibrations is the seal of belly fairing panels 191 and 192BT:
- do the procedure: vibration and/or noise felt in mid cabin (Ref. TASK 53-35-00-810-801).
(10) Type 10
(a) The cause of vibrations is the seals of belly fairing panels 191 and 192DT:
- do the procedure: vibration and/or noise felt in mid cabin (Ref. TASK 53-35-00-810-801).
(11) Type 11
(a) The cause of vibrations is the seals of belly fairing panels 191 and 192ET:
- do the procedure: vibration and/or noise felt in mid cabin (Ref. TASK 53-35-00-810-801).
(b) The cause of vibrations is the seal of belly fairing panels 191 and 192LB:
- do the procedure: vibration and/or noise felt in mid cabin (Ref. TASK 53-35-00-810-801).
(12) Type 12
(a) The cause of vibrations is the forward passenger/crew door cover plates:
- do the procedure: vibrations and noise in the forward passenger/crew door area (Ref. TASK 52-11-00-810-826).
(13) Type 13
(a) The cause of vibrations is the aft passenger/crew door cover plates:
- do the procedure: vibrations and noise in the aft passenger/crew door area (Ref. TASK 52-13-00-810-826).
(14) Type 14
(a) Not applicable
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May 01/03R CES
Hard/Overweight Landing
1. Possible Causes
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2. Job Set-up Information 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 时间限制/维护检查(5)
