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时间:2011-03-20 21:14来源:蓝天飞行翻译 作者:admin
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 Subtask 23-61-42-420-061
 K. Installation of the Static Discharger Retainers Zone 534 (634) (Wing-Tip) (Ref. Fig. 404/TASK 23-61-42-991-005)
 (1) Put the static discharger retainer (2) in position with the filling piece (4), and install it with the (2 off) rivets (1) and the (4 off) rivets (3).
 (a) Use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to remove the unwanted sealant from around the applicable static discharger retainer.
 Subtask 23-61-42-420-062
 L. Installation of the Static Discharger Retainers Zone 534 (634) (Wing-Tip Fence) (Ref. Fig. 405/TASK 23-61-42-991-006)
 (1)
 Put the static discharger retainer (16) in position and install it with the (5 off) rivets (14) and the (1 off) rivet (15).

 (2)
 Put the static discharger retainer (13) in position and install it with the (4 off) rivets (12) and the (2 off) rivets (11) .

 (3)
 Put the static discharger retainer (10) in position and install it with the (4 off) rivets (9) and the (2 off) rivets (8).

 (4)
 Put the static discharger retainer (7) in position and install it with the (2 off) rivets (6), the (2 off) rivets (5), and the (2 off) rivets (4).

 (5)
 Use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to remove the unwanted sealant from around the applicable static discharger retainer.


 Subtask 23-61-42-760-050
 M. Test
 (1) Make sure that the bonding resistance is correct (Ref. TASK 23-61-00-200-001).
 1EFF : ALL 1 23-61-42Page 422 1 1 Feb 01/01 1 1 1CES 1 Subtask 23-61-42-420-052


 N. Continue the Installation of the Static Discharger Retainer
 (1)
 If necessary, paint the applicable static discharger retainer the same as the adjacent structure.

 (2)
 Do not paint the interfaces of the applicable static discharger retainer.


 5. Close-up
________ Subtask 23-61-42-410-050
 A. Close Access
 (1) Install the static discharger (Ref. TASK 23-61-41-400-001). Subtask 23-61-42-865-052
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 5CC1, 5CC2, 14CC1, 14CC2, 19CE1, 19CE2, 19CE3, 15CE1, 15CE2, 16CE1, 16CE2.
 Subtask 23-61-42-942-050
 C. Removal of Equipment
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the safety barriers.

 (3)
 Remove the access platform(s).

 (4)
 Remove the warning notice(s).

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 1EFF : ALL 1 23-61-42Page 423 1 1 Nov 01/00R 1 1 1CES 1


 COCKPIT VOICE RECORDER - DESCRIPTION AND OPERATION
__________________________________________________
 1. General
_______

R **ON A/C 001-049, 062-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 The Solid State Cockpit Voice Recorder (SSCVR) is designed to record crew conversations and communications into memory block unit in flight and on ground, when at least one engine is running or up to five minutes after the last engine is shut down irrespective of which engine is shut down first. The system can also operate in manual mode on the ground. The recorder is a four-track system and all tracks are recorded simultaneously. The SSCVR provides storage for 2 hours of consecutive recording for each of the four audio input channels. When the memory block unit is fully recorded, the system progressively erases recordings made in the previous 2 hours and simultaneously records new information; thus only information recorded in the last 2 hours of operation is retained. The recorded information can be intentionally erased when the aircraft is on the ground with the parking brake on, locked and electrically powered. Bulk erasure is also possible during manual operation of the system.
 **ON A/C 051-061,
 The Solid State Cockpit Voice Recorder (SSCVR) is designed to record crew conversations and communications into Crash Survivable Memory Unit (CSMU) in flight and on ground, when at least one engine is running or up to five minutes after the last engine is shut down irrespective of which engine is shut down first. The system can also operate in manual mode on the ground. The recorder is a four-track system and all tracks are recorded simultaneously. The SSCVR provides storage for 30 minutes of consecutive recording for each of the four audio input channels. When the CSMU is fully recorded, the system progressively erases recordings made in the previous 30 minutes and simultaneously records new information; thus only information recorded in the last 30 minutes of operation is retained. The recorded information can be intentionally erased when the aircraft is on the ground with the parking brake on, locked and electrically powered. Bulk erasure is also possible during manual operation of the system.
 
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