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

_______________
 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
　
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