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STABILIZERS - Horizontal Stabilizer - Joint Inspection - FAA Final Rule

#41

Postby four engine jock » Wed May 24, 2017 8:03 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0278-01B] Multi Operator Message
MESSAGE DATE: 23 May 2017 1657 US PACIFIC TIME / 23 May 2017 2357 GMT

This message is sent to 737-100/-200 Customers, Airlines For America, International Air Transport Association, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Engineering, Regulatory

SERVICE REQUEST ID: 4-3777310937
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: 27-Jun-2017 23:59
PRODUCT TYPE: Airplane
PRODUCT LINE: 737
PRODUCT: 737-100/-200
ATA: 5510-00



SUBJECT: Information - STABILIZERS - Horizontal Stabilizer - Joint Inspection - FAA Final Rule

REFERENCES:
/A/ AD 2017-11-01
/B/ 2015-NM-199-AD; SR# 4-3248906869; dated 26-Aug-2016 /C/ SB 737-55A1033; Rev 02, dated 07-Aug-2015



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SUMMARY:
Please be advised of the following notice from the FAA:

The FAA is adopting a new airworthiness directive (AD) for certain Boeing 737-100, -200, and -200C series airplanes. This AD is intended to complete certain mandated programs to support the airplane reaching its limit of validity (LOV) of the engineering data that support the established structural maintenance program. This AD requires various repetitive inspections for cracking of certain lugs on the rear spar and horizontal stabilizer, related investigative and corrective actions if necessary, and replacement of the center section rear spar upper chord as applicable. We are issuing this AD to address the unsafe condition on these products.

This AD is effective June 27, 2017.

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DESCRIPTION:
Applicability:
This AD applies to Boeing 737-100, -200, and -200C series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-55A1033, Revision 2, dated August 7, 2015.

DESIRED ACTION:
==============
The complete text of the subject AD was noted in the Federal Register and will be accessible via the following World Wide Web address:

http://rgl.faa.gov/Regulatory_and_Guida ... t?OpenPage

Enter the AD number from ref /A/ (excluding "AD") in the search box and use your left mouse button to select "Go".


Craig Richesin, Boeing Communication System Manager

Courtney Makela - Director
Engineering Integration
Customer Support
The Boeing Company

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four engine jock
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ED CARTER ANNOUNCED AS FLEET CHIEF FOR ALL OUT-OF-PRODUCTION MODELS

#42

Postby four engine jock » Thu Jun 01, 2017 8:43 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0293-01B] Multi Operator Message
MESSAGE DATE: 31 May 2017 1601 US PACIFIC TIME / 31 May 2017 2301 GMT

This message is sent to all Customers, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Maintenance, Engineering, Flight Operations, Management

SERVICE REQUEST ID: 4-3787231625
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: No Action Required
PRODUCT TYPE: Airplane
PRODUCT LINE: ALL
PRODUCT: ALL
ATA: 0000-00



SUBJECT: Information - ED CARTER ANNOUNCED AS FLEET CHIEF FOR ALL OUT-OF-PRODUCTION MODELS


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DESCRIPTION:

In order to better leverage synergies across the Out-of-Production fleets, Boeing has combined the support for all Out-of-Production models under one Fleet Chief. Effective immediately, Ed Carter will have the Fleet Chief responsibility for all Out-of-Production model airplanes. This will include the 707, 727, 737CL, 757, DC-9, MD-10, MD-90, 717, DC-10, MD-10, and MD-11. Support for all series of the 747 will remain under Mark Steele.

Ed has been supporting Out-of-Production airplanes in the Fleet Chief position since 2002 and has extensive experience with the DC and MD model airplanes. Additionally, he served as Fleet Chief for the 737CL when support for that program transitioned from Puget Sound to Southern California.

If attachments are referred to, and are not present, please access them by logging into MyBoeingFleet Service Requests application. If you have further questions, you may contact the appropriate Airline Support Manager.

Service Request System : https://myboeingfleet.boeing.com/bsrs/c ... /4-1QMMXT3
(Note: MyBoeingFleet portal login is required to access link in the Service Request System)

SR App (Legacy) : https://myboeingfleet.boeing.com/servic ... torMessage

Courtney Makela
Director - Engineering Integration
Commercial Aviation Services
The Boeing Company

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four engine jock
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Posts: 373
Joined: Fri Feb 10, 2012 12:00 am
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Warning change for Axle Jacking and Airplane Maintenance Manual (AMM) Temporary Revisions Issued

#43

Postby four engine jock » Mon Jun 05, 2017 8:57 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0301-01B] Multi Operator Message
MESSAGE DATE: 02 Jun 2017 1722 US PACIFIC TIME / 03 Jun 2017 0022 GMT

This message is sent to all 737 and C-40A Operators, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Publications/Manuals

SERVICE REQUEST ID: 4-3790786963
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: 02-Jun-2017 23:59
PRODUCT TYPE: Maint. and Repair Document
PRODUCT LINE: SEVERAL
PRODUCT: AMM - Aircraft Maintenance Manual
ATA: 0700-00


SUBJECT: Information - Warning change for Axle Jacking and Airplane Maintenance Manual (AMM) Temporary Revisions Issued

REFERENCES:
/A/ Airplane Maintenance Manual (AMM) 07-11-03-580


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SUMMARY:
The purpose of this Multi-Operator Message (MOM) is to advise operators on recent changes to a warning in Airplane Maintenance Manual (AMM) 07-11-03-580 of the Airplane Maintenance Manual (AMM) for several Boeing airplane models pertaining to maintenance tasks when the axles are on jacks. The initial changes were to account for passenger loading in addition to cargo loading due to the effect of movement on the aircraft center of gravity and an increase to the loads on the axle jacks during maintenance.

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DESCRIPTION:
Boeing researched past reported incidents that happened while an airplane was on axle jacks and found 11 events where the airplane (various models) slipped off the axle jack. These incident reports provide substantiation of the increased risk of a jack slip with passenger loading activities. Subsequently, Boeing's intent was to warn operators to account for any shifting loads that included passenger loading while the airplane is on jacks.

However, Boeing recognizes the prior change of the warning had prohibitive wording that impacted customer operations. Boeing considers the operator is in the best position to manage their applicable loading/unloading procedures for passenger and/or cargo including weight and balance management during maintenance tasks when the axles are on jacks to prevent jack slips.

The latest changes to the various fleets were based on further review with the intent to revise the warning as a notice of precautionary guidance and not an instruction step or a requirement to perform.
The revised warnings were release via Temporary Revisions in May 2017 and are available on MyBoeingFleet.

WARNING: MOVEMENT OF CARGO, PASSENGERS, OR CREW INTO OR OUT OF
THE AIRPLANE WHILE THE AXLES ARE ON JACKS CAN CAUSE A
CHANGE IN THE CENTER OF GRAVITY AND CAUSE A HIGH LOAD
ON THE AXLE JACKS. IT CAN ALSO CAUSE THE AIRPLANE TO
FALL OFF THE JACKS.
INJURIES TO PERSONNEL AND DAMAGE TO EQUIPMENT
CAN OCCUR.


Boeing apologizes for any impact this has caused and has changed our processes to prevent occurrences like this from taking place in the future to include inserting additional technical checks in our controls. Although this is an atypical circumstance, this level of impact to customer operations has heightened our resolve to prevent any future occurrences.

Boeing recommends that operators become familiar with the contents of the temporary revision in order to minimize the impact to operations from axle jacking. If you have further questions you may contact your Field Service Representative.


If attachments are referred to, and are not present, please access them by logging into MyBoeingFleet Service Requests application. If you have further questions, you may contact the appropriate Airline Support Manager.

Service Request System : https://myboeingfleet.boeing.com/bsrs/c ... /4-1QOFZS4
(Note: MyBoeingFleet portal login is required to access link in the Service Request System)

SR App (Legacy) : https://myboeingfleet.boeing.com/servic ... torMessage


Steve O'Neal, Manager - Maintenance Engineering Michael Pelligra, Senior Manager - Maintenance Engineering

Chris Johnson-Pasqua
Director - Maintenance Engineering
Commercial Aviation Services
The Boeing Company

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four engine jock
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WINGS - Plates/Skin - Upper Aft Skin at Rear Spar from Wing Buttock Line 159 to 220 - Inspection - FAA NPRM

#44

Postby four engine jock » Wed Jun 07, 2017 9:43 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0307-01B] Multi Operator Message
MESSAGE DATE: 06 Jun 2017 1404 US PACIFIC TIME / 06 Jun 2017 2104 GMT

This message is sent to 737-100/-200/-300/-400/-500 Customers, Airlines For America, International Air Transport Association, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Engineering, Regulatory

SERVICE REQUEST ID: 4-3794246767
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: 20-Jul-2017 23:59
PRODUCT TYPE: Airplane
PRODUCT LINE: SERVERAL
PRODUCT: SERVERAL
ATA: 5730-00


SUBJECT: Information - WINGS - Plates/Skin - Upper Aft Skin at Rear Spar from Wing Buttock Line 159 to 220 - Inspection - FAA NPRM

REFERENCES:
/A/ 2017-NM-026-AD
/B/ SB 737-57A1329, Rev 00, Dated 16-Jan-2017

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SUMMARY:
Please be advised of the following notice from the FAA:

The FAA propose to adopt a new airworthiness directive (AD) for all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD was prompted by reports of cracking in the upper aft skin at the rear spar of the wings. This proposed AD would require repetitive inspections for cracking of the upper aft skin of the wings, and repair if necessary. We are proposing this AD to address the unsafe condition on these products.

Comments must be received by the FAA by July 20, 2017.

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DESCRIPTION:
Applicability:

This AD applies to all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category.

DESIRED ACTION:
==============
Please utilize one of the following methods for submitting comments:

Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.

Fax: 202-493-2251

Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

The complete text of the subject NPRM was noted in the Federal Register and will be accessible via the following World Wide Web address (enter the NPRM number from Ref /A/ in the search box and use your left mouse button to select "Go").

http://www.airweb.faa.gov/Regulatory_an ... t?OpenPage

Craig Richesin, Boeing Communication System Manager

Courtney Makela - Director
Engineering Integration
Customer Support
The Boeing Company

User avatar
four engine jock
Engine Run Up Poster
Posts: 373
Joined: Fri Feb 10, 2012 12:00 am
Location: My Office
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FUSELAGE - Skins - Section 41, 43, and 46 Skin Lap Splice Inspection - FAA Final Rule

#45

Postby four engine jock » Fri Jun 09, 2017 9:06 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0317-01B] Multi Operator Message
MESSAGE DATE: 08 Jun 2017 1653 US PACIFIC TIME / 08 Jun 2017 2353 GMT

This message is sent to all 767 Customers, Airlines For America, International Air Transport Association, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Engineering, Regulatory

SERVICE REQUEST ID: 4-3798213607
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: 13-Jul-2017 23:59
PRODUCT TYPE: Airplane
PRODUCT LINE: SEVERAL
PRODUCT: SEVERAL
ATA: 5315-00


SUBJECT: Information - FUSELAGE - Skins - Section 41, 43, and 46 Skin Lap Splice Inspection - FAA Final Rule

REFERENCES:
/A/ AD 2017-11-04
/B/ 2016-NM-068-AD; SR# 4-3435305259 dated 14-Nov-2016 /C/ SB 767-53A0264; Rev 01 dated 25-Apr-2016


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SUMMARY:
Please be advised of the following notice from the FAA:

The FAA is adopting a new airworthiness directive (AD) for all Boeing 767-200, -300, and -400ER series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the fuselage skin lap splices are subject to widespread fatigue damage (WFD). This AD requires repetitive inspections to detect any crack in the fuselage skin at the skin lap splices, and corrective actions if necessary. We are issuing this AD to address the unsafe condition on these products.

This AD is effective July 13, 2017.

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DESCRIPTION:
Applicability
(1) This AD applies to Boeing 767-200, -300, and -400ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 767-53A0264, Revision 1, dated April 25, 2016 (''ASB 767-53A0264 R1'').
(2) Installation of Supplemental Type Certificate (STC) ST01920SE (http://rgl.faa.gov/Regulatory_and_Guida ... =st01920se) does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01920SE is installed, a "change in product" alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.

DESIRED ACTION:
==============
The complete text of the subject AD was noted in the Federal Register and will be accessible via the following World Wide Web address:

http://rgl.faa.gov/Regulatory_and_Guida ... t?OpenPage

Enter the AD number from ref /A/ (excluding "AD") in the search box and use your left mouse button to select "Go".


Craig Richesin, Boeing Communication System Manager

Courtney Makela - Director
Engineering Integration
Customer Support
The Boeing Company

User avatar
four engine jock
Engine Run Up Poster
Posts: 373
Joined: Fri Feb 10, 2012 12:00 am
Location: My Office
Cuba

WINGS -Trailing Edge and Trailing Edge Devices-Inboard Flap Outboard Support Assembly Number 3 & 6 - FAA Final Rule

#46

Postby four engine jock » Fri Jun 09, 2017 9:06 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0316-01B] Multi Operator Message
MESSAGE DATE: 08 Jun 2017 1630 US PACIFIC TIME / 08 Jun 2017 2330 GMT

This message is sent to 767-200 Customers, Airlines For America, International Air Transport Association, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Engineering, Regulatory

SERVICE REQUEST ID: 4-3798213531
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: 24-Jul-2017 23:59
PRODUCT TYPE: Airplane
PRODUCT LINE: 767
PRODUCT: 767-200
ATA: 5750-00


SUBJECT: Information - WINGS -Trailing Edge and Trailing Edge Devices-Inboard Flap Outboard Support Assembly Number 3 & 6 - FAA Final Rule;Request for comments

REFERENCES:
/A/ AD 2017-12-01
/B/ SB 767-57A0134; dated 27-May-2016


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SUMMARY:
Please be advised of the following notice from the FAA:

The FAA is adopting a new airworthiness directive (AD) for certain Boeing 767-200 series airplanes. This AD requires repetitive inspections for damage of a certain drive arm assembly, and related investigative and corrective actions if necessary. This AD was prompted by a report indicating that during an inspection associated with a flap, the extend overtravel stops on an actuator crank arm assembly were making contact with an adjacent drive arm assembly when the flaps were retracted. We are issuing this AD to address the unsafe condition on these products.

This AD is effective June 23, 2017. Comments must be received by the FAA by July 24, 2017.

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DESCRIPTION:
Applicability
This AD applies to Boeing 767-200 series airplanes, equipped with 767-400ER flaps modified as specified in supplemental type certificate (STC) ST01329WI-D.

DESIRED ACTION:
==============
Please utilize one of the following methods for submitting comments:

Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.

Fax: 202-493-2251

Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

The complete text of the subject AD was noted in the Federal Register and will be accessible via the following World Wide Web address:

http://rgl.faa.gov/Regulatory_and_Guida ... t?OpenPage

Enter the AD number from ref /A/ (excluding "AD") in the search box and use your left mouse button to select "Go".


Craig Richesin, Boeing Communication System Manager

Courtney Makela - Director
Engineering Integration
Customer Support
The Boeing Company

User avatar
four engine jock
Engine Run Up Poster
Posts: 373
Joined: Fri Feb 10, 2012 12:00 am
Location: My Office
Cuba

707/720 AIRWORTHINESS LIMITATIONS (AWLs)

#47

Postby four engine jock » Wed Jun 21, 2017 9:10 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0338-01B] Multi Operator Message
MESSAGE DATE: 20 Jun 2017 1503 US PACIFIC TIME / 20 Jun 2017 2203 GMT

This message is sent to all 707/720 Customers, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Maintenance, Engineering

SERVICE REQUEST ID: 4-3812221717
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: No Action Required
PRODUCT TYPE: Maint. Planning and Programs
PRODUCT LINE: 707
PRODUCT: Maintenance Planning and Programs
ATA:


SUBJECT: Information - 707/720 AIRWORTHINESS LIMITATIONS (AWLs)

REFERENCES:


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SUMMARY:
This message is to inform operators that the 707/720 AIRWORTHINESS LIMITATIONS (AWLs), D6-7552-AWL, dated October 2016 is available on MyBoeingFleet for review and implementation.

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DESCRIPTION:
The 707/720 AIRWORTHINESS LIMITATIONS (AWLs), D6-7552-AWL, has been revised as part of an effort to standardize the Airworthiness Limitations across Boeing models. This revision also revises existing requirements and adds new requirements for fuel system inspections and for verifying electrical bonding resistance for various fuel system components.

The revised document was published on MyBoeingFleet June 8, 2017.

If attachments are referred to, and are not present, please access them by logging into MyBoeingFleet Service Requests application. If you have further questions, you may contact the appropriate Airline Support Manager.

Service Request System : https://myboeingfleet.boeing.com/bsrs/c ... /4-1QZ9F55
(Note: MyBoeingFleet portal login is required to access link in the Service Request System)

SR App (Legacy) : https://myboeingfleet.boeing.com/servic ... torMessage


Daniel F. Marandola - Senior Manager
Maintenance Programs Engineering
Commercial Aviation Services
The Boeing Company

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four engine jock
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Posts: 373
Joined: Fri Feb 10, 2012 12:00 am
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FUSELAGE - Frames - Body Station 727 Outboard Chord at Stringer 18A,

#48

Postby four engine jock » Mon Jul 03, 2017 8:17 am

FROM: THE BOEING COMPANY
TO: Boeing Correspondence (MOM)
[MESSAGE NUMBER:MOM-MOM-17-0359-01B] Multi Operator Message
MESSAGE DATE: 30 Jun 2017 1325 US PACIFIC TIME / 30 Jun 2017 2025 GMT

This message is sent to 737-100/-200/-300/-400/-500 Customers, Airlines For America, International Air Transport Association, Airline Resident Representatives, Regional Directors, Regional Managers and Boeing Field Service Bases.

CATEGORY: Engineering, Regulatory

SERVICE REQUEST ID: 3-3906690559
ACCOUNT: Boeing Correspondence (MOM)
DUE DATE: 14-Aug-2017 23:59
PRODUCT TYPE: Airplane
PRODUCT LINE: 737
PRODUCT: 737-100/-200/-300/-400/-500
ATA: 5311-00



SUBJECT: Information - FUSELAGE - Frames - Body Station 727 Outboard Chord at Stringer 18A, Inspection and Preventive Modification - FAA NPRM

REFERENCES:
/A/ 2016-NM-184-AD
/B/ SB 737-53A1166, Rev 02, dated 25-May-2006


- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
SUMMARY:
Please be advised of the following notice from the FAA:

The FAA propose to adopt a new airworthiness directive (AD) for all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD was prompted by reports of fatigue cracking in the frame outboard chord and in the radius of the auxiliary chord at a certain area. This proposed AD would require inspections to detect this cracking, and corrective action if necessary. We are proposing this AD to address the unsafe condition on these products.

Comments must be received by the FAA by August 14, 2017.

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
DESCRIPTION:
Applicability
This AD applies to all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category.

DESIRED ACTION:
==============
Please utilize one of the following methods for submitting comments:

Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.

Fax: 202-493-2251

Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

The complete text of the subject NPRM was noted in the Federal Register and will be accessible via the following World Wide Web address (enter the NPRM number from Ref /A/ in the search box and use your left mouse button to select "Go").

http://www.airweb.faa.gov/Regulatory_an ... t?OpenPage


Craig Richesin, Boeing Communication System Manager

Courtney Makela - Director
Engineering Integration
Customer Support
The Boeing Company


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