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时间:2011-03-14 13:13来源:蓝天飞行翻译 作者:admin
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Temporary information is normally incorporated into the manual at the next formal revision. When the condition remains temporary after a bulletin incorporation, the temporary paragraphs are identified by a heading referencing the originating bulletin. When the temporary condition no longer exists, the bulletin is cancelled and the original manual content is restored.
Bulletin status is defined as follows:
.  
In Effect (IE) – the bulletin contains pertinent information not otherwise
covered in the FCOM. The bulletin is active and should be retained in the
manual.


.  
Incorporated (INC) – the bulletin operating information has been
incorporated into the FCOM. The bulletin is active and should be retained
in the manual.


.  
Cancelled (CANC) – the bulletin is no longer active and should be
removed from the FCOM. Previously cancelled bulletins are no longer
listed in the Bulletin Record.

 

The record below should be accomplished by the person revising the material.
Number  Subject  Ref. No. (CS3-)  Date  Status 
ELF–9  Emergency Deployment if Escape Slides  06–16–95  IE 
ELF–10  Intermittent/Inoperative EGT Indicators  06–16–95  IE 
ELF–11  Flight Management Computer Navigation Anomaly  06–16–95  IE 

Preface -Bulletin Record 737 Operations Manual

Number  Subject  Ref. No. (CS3-)  Date  Status 
ELF–12  Standby Horizon Indicator Display  06–16–95  IE 
ELF–14  Nonselected MCP Setting Changes  06–16–95  IE 
ELF–15  Auxiliary Power Unit (APU) Starting  06–16–95  IE 
ELF–16  BLEED TRIP OFF Light Illumination During A No Engine Bleed Takeoff  06–16–95  IE 
ELF–17 R1  Runaway Stabilizer Procedure  09–20–95  IE 
ELF–22  Control Wheel Microphone/Interphone Switch Anomaly  03–12–99  IE 
ELF–25  Maneuvering Speeds for 737-100/200/300/400/500  12–03–99  IE 
ILF–28  Trailing Edge Flaps - Outboard Flap Carriage Spindle Fractures  11–17–03  IE 
ILF–29  FMC Arc Leg Sequencing Anomaly  05–12–04  IE 

Copyright . The Boeing Company. See title page for details.
0.6.2  December 3, 2004

Flight Crew Operations Manual Bulletin
for
 

The Boeing Company Seattle, Washington 98124-2207

737
Number: ELF-9 Date: June 16, 1995 Document Effectivity: 
Subject:  Emergency Deployment of Escape Slides 
Reason:  This bulletin provides information contained in Red Bulletin 737-300 85-7R1, dated April 15, 1992, which advised flight crews of possible jamming of cabin doors when deploying emergency escape slides. 

Information in this Flight Crew Operations Manual (FCOM) bulletin is recommended by The Boeing Company, but may not be FAA approved at the time of writing. In the event of conflict with the FAA approved Airplane Flight Manual (AFM), the AFM shall supersede. The Boeing Company regards the information or procedures described herein as having a direct or indirect bearing on the safe operation of this model airplane.
THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT
Background Information
It was reported that during a 737 emergency evacuation the right hand forward service door was opened with considerable force and speed. The escape slide compartment cover opened prematurely and the escape slide partially came out of the compartment onto the airplane floor. This initially prevented further opening of the door. The compartment cover was then pushed back toward the closed position, which permitted opening of the door. As the door was opened the escape slide was pushed out. The escape slide was then deployed and inflated normally.
Checks were accomplished on comparable but not identical configurations and revealed that in some instances the use of considerable force and speed during the initial door opening sequence could duplicate the reported condition. Doors and escape slides operated properly when excessive force and speed were not exerted.
System modifications were evaluated and Service Bulletin 737-25A1182 was issued to correct this condition. Until such modifications are incorporated, flight crew personnel are advise to open all doors smoothly during an emergency evacuation, avoiding excessive force or speed during the initial door opening sequence.
Page 1 of 2
Flight Crew Operations Manual Bulletin No. ELF-9,dated June 16, 1995 (continued)
 
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