FAA Biweekly AD Report 2015-09

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FAA Air Transport Association (ATA) of America 54, Nacelles/Pylons.

This AD applies to ATR-GIE Avions de Transport Régional Model ATR72-212A airplanes, certificated in any category, manufacturer serial numbers 468 through 719 inclusive, 723, 776, 777, 779, 821, and 837.
N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) ATR ATR72 Airplane Maintenance Manual (AMM) Job Instruction Card 54-11-61 DVI 10000, Detailed Visual Inspection of Forward Engine Mount, dated March 1, 2012.
(ii) ATR ATR72 AMM Job Instruction Card 71-20-00 DVI 10000, Detailled (sic) Visual Inspec[tion] of Engine Shockmounts, dated March 1, 2012.
FAA Air Transport Association (ATA) of America Code 57, Wings
This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category.
(1) Bombardier, Inc. Model CL-600-1A11 (CL-600) airplanes, serial numbers 1004 through 1085 inclusive.
(2) Bombardier, Inc. Model CL-600-2A12 (CL-601) airplanes, serial numbers 3001 through 3066 inclusive.
(3) Bombardier, Inc. Model CL-600-2B16 (CL-601-3A and CL-601-3R Variants) airplanes, serial numbers 5001 through 5194 inclusive.
(4) Bombardier, Inc. Model CL-600-2B16 (CL-604 Variants) airplanes, serial numbers 5301 through 5665 inclusive, and 5701 through 5953 inclusive.
N/A
TC AD CF-2014-01

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 600-0762, dated September 26, 2013.
(ii) Bombardier Service Bulletin 601-0631, dated September 26, 2013.
(iii) Bombardier Service Bulletin 604-57-007, Revision 01, dated November 12, 2014.
(iv) Bombardier Service Bulletin 605-57-005, Revision 01, dated November 12, 2014.
(v) Canadair Challenger Temporary Revision 5-157, Outboard Flap-Hinge Box Forward Lugs, dated July 8, 2013, to Canadair Challenger Time Limits/Maintenance Checks Manual, PSP 605.
(vi) Canadair Challenger Temporary Revision 5-158, Inboard Flap-Hinge Box Forward Lugs, dated July 8, 2013, to Canadair Challenger Time Limits/Maintenance Checks Manual, PSP 605.
(vii) Canadair Challenger Temporary Revision 5-262, Outboard and Inboard Flap-Hinge Box Forward Lugs, dated July 8, 2013, to Canadian Challenger Time Limits/Maintenance Checks Manual PSP 601.
(viii) Canadair Challenger Temporary Revision 5-275, Outboard Flap-Hinge Box Forward Lugs, dated July 8, 2013, to Canadian Challenger Time Limits/Maintenance Checks Manual PSP 601A-5.
(ix) Canadair Challenger Temporary Revision 5-276, Inboard Flap-Hinge Box Forward Lugs, dated July 8, 2013, to Canadian Challenger Time Limits/Maintenance Checks Manual PSP 601A-5.
(x) Task 57-50-00-121 Special Detailed Inspection of the Forward Lugs of the Inboard Flap Hinge Box of Section 5-10-30 of Part 2, ''Airworthiness Limitations,'' of Bombardier CL-605 Time Limits/Maintenance Checks Manual, Revision 8, dated July 8, 2013.
(xi) Task 57-50-00-121 Special Detailed Inspection of the Forward Lugs of the Inboard Flap Hinge Box of Section 5-10-30 of Part 2, ''Airworthiness Limitations,'' of Bombardier CL-604 Time Limits/Maintenance Checks Manual, Revision 20, dated July 8, 2013.
(xii) Task 57-52-01-102 Special Detailed Inspection of the Hinge-Box Forward Lugs of the Outboard Flap of Section 5-10-30 of Part 2, ''Airworthiness Limitations,'' of Bombardier CL-605 Time Limits/Maintenance Checks Manual, Revision 8, dated July 8, 2013.
(xiii) Task 57-52-01-102 Special Detailed Inspection of the Hinge-Box Forward Lugs of the Outboard Flap of Section 5-10-30 of Part 2, ''Airworthiness Limitations,'' of Bombardier CL-604 Time Limits/Maintenance Checks Manual, Revision 20, dated July 8, 2013.
FAA Air Transport Association (ATA) of America Code 27, Flight Controls
This AD applies to The Boeing Company Model 757-200, -200PF, -200CB, and -300 series airplanes; certificated in any category; as identified in Boeing Service Bulletin 757-27A0152, Revision 3, dated October 28, 2013, as revised by Boeing Service Bulletin 757-27A0152, Revision 4, dated August 26, 2014.
N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Service Bulletin 757-27A0152, Revision 3, dated October 28, 2013.
(ii) Boeing Service Bulletin 757-27A0152, Revision 4, dated August 26, 2014.
FAA Air Transport Association (ATA) of America Code 32, Landing Gear
This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 through 4109 inclusive.
N/A
TC AD CF-2013-40

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 84-32-67, dated July 8, 2009.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 26, Fire Protection
This AD applies to Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes, certificated in any category; all serial numbers.
AD 2013-26-05
EASA AD 2012-0189

(3) The following service information was approved for IBR on October 20, 2014, (79 FR 54897, September 15, 2014).
(i) Dassault Service Bulletin F20-785, also referred to as 785, dated June 11, 2012.
(ii) Dassault Service Bulletin F200-131, also referred to as 131, dated June 11, 2012.
FAA Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks
This AD applies to all Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes; and all Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes, Model A300 B4-605R and B4-622R airplanes, Model A300 F4-605R and F4-622R airplanes, and Model A300 C4-605R Variant F airplanes; certificated in any category.
FAA AD 2007-14-05
EASA AD 2013-0072

(3) The following service information was approved for IBR on June 1, 2015.
(i) Airbus A300-600 Airworthiness Limitations Section Part 3, Certification Maintenance Requirements, dated April 18, 2012.
(ii) Airbus A310 Airworthiness Limitations Section Part 3, Certification Maintenance Requirements, dated November 30, 2012.
(4) The following service information was approved for IBR on August 22, 2007 (72 FR 39307, July 18, 2007).
(i) Airbus A300-600 Certification Maintenance Requirements AI/ST5/829/85, Issue 12, dated February 2005.
(ii) Airbus A310 Certification Maintenance Requirements AI/ST5/849/85, Issue 12, dated February 2005.
FAA Air Transport Association (ATA) of America Code 57, Wings
This AD applies to Airbus Model A319-115, A319-132, A319-133, A320-214, A320-232, and A320-233 airplanes, certificated in any category, manufacturer serial numbers (MSN) 5817, 5826, 5837, 5848, 5855, 5864, 5875, 5886, 5896, 5910, and 5918 and subsequent.
FAA ADs 2014-26-53 and 2015-03-02
EASA AD 2015-0026

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Alert Operators Transmission A57N006-14, Revision 01, dated February 16, 2015.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 53, Fuselage
(1) This AD applies to The Boeing Company Model 737-600 and -700 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-53A1325, dated December 3, 2013. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE 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.
N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 737-53A1325, dated December 3, 2013.
(ii) Reserved
FAA Air Transport Association (ATA) of America Code 32, Landing Gear
This AD applies to Bombardier, Inc. Model CL-600-2E25 (Regional Jet Series 1000) airplanes, certificated in any category, serial numbers 19002 and subsequent
N/A
TC AD CF-2014-16

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Temporary Revision ALI-0472, dated February 27, 2014, to Section 1-32 of Part 2, Airworthiness Limitations, of the Bombardier CRJ Series Regional Jet Maintenance Requirements Manual, CSP B-053.
(ii) Reserved
FAA Air Transport Association (ATA) of America Code 54, Nacelles/pylons
This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, except for airplanes on which Airbus Modification 33844 or Modification 33847, as applicable, has been embodied in production.
(1) Airbus Model A318-111 and -112 airplanes.
(2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
N/A
EASA AD 2014-0064

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A320-54-1019, Revision 02, dated April 15, 2014.
(ii) Airbus Service Bulletin A320-54-1022, Revision 03, dated April 15, 2014.
FAA Air Transport Association (ATA) of America Code 24, Electrical power
This AD applies to all The Boeing Company Model 787 airplanes, certificated in any category
N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Multi Operator Message MOM-MOM-15-0248-01B, dated April 19, 2015. The date appears only on the first page of this document.
(ii) Boeing Multi Operator Message MOM-MOM-15-0248-01B(R1), dated April 20, 2015. The date appears only on the first page of this document.
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