Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2d and S2r Series Airplanes (Us Federal Aviation Administration Regulation) (Faa) (2018 Edition) PDF Download
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Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727241143
Category :
Languages : en
Pages : 44
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Book Description
Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are adopting a new airworthiness directive (AD) to supersede AD (AD) 2006-07-15, which applies to Thrush Aircraft, Inc. Model 600 S2D and S2R (S-2R) series airplanes (type certificate previously held by Quality Aerospace, Inc. and Ayres Corporation). AD 2006-07-15 currently requires repetitive inspections of the 1/4-inch and 5/16-inch bolt hole areas on the wing front lower spar caps for fatigue cracking; replacement or repair of any wing front lower spar cap where fatigue cracks are found; and reporting of any fatigue cracks found to the FAA. AD 2006-07-15 also puts the affected airplanes into groups for compliance time and applicability purposes. Since we issued AD 2006-07-15, FAA analysis reveals that inspections are not detecting all existing cracks and shows the incidences of undetected cracks will increase as the airplanes age. Consequently, this AD retains the actions of AD 2006-07-15 and imposes a life limit on the wing front lower spar caps that requires replacement of the wing front lower spar caps when the life limit is reached. This AD also changes the requirements and applicability of the groups discussed above and removes the ultrasonic inspection method. We are issuing this AD to prevent wing front lower spar cap failure caused by undetected fatigue cracks. Such failure could result in loss of a wing in flight. This book contains: - The complete text of the Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727241143
Category :
Languages : en
Pages : 44
Get Book Here
Book Description
Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are adopting a new airworthiness directive (AD) to supersede AD (AD) 2006-07-15, which applies to Thrush Aircraft, Inc. Model 600 S2D and S2R (S-2R) series airplanes (type certificate previously held by Quality Aerospace, Inc. and Ayres Corporation). AD 2006-07-15 currently requires repetitive inspections of the 1/4-inch and 5/16-inch bolt hole areas on the wing front lower spar caps for fatigue cracking; replacement or repair of any wing front lower spar cap where fatigue cracks are found; and reporting of any fatigue cracks found to the FAA. AD 2006-07-15 also puts the affected airplanes into groups for compliance time and applicability purposes. Since we issued AD 2006-07-15, FAA analysis reveals that inspections are not detecting all existing cracks and shows the incidences of undetected cracks will increase as the airplanes age. Consequently, this AD retains the actions of AD 2006-07-15 and imposes a life limit on the wing front lower spar caps that requires replacement of the wing front lower spar caps when the life limit is reached. This AD also changes the requirements and applicability of the groups discussed above and removes the ultrasonic inspection method. We are issuing this AD to prevent wing front lower spar cap failure caused by undetected fatigue cracks. Such failure could result in loss of a wing in flight. This book contains: - The complete text of the Airworthiness Directives - Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727240535
Category :
Languages : en
Pages : 34
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Book Description
Airworthiness Directives - Piper Aircraft, Inc. Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - Piper Aircraft, Inc. Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Models PA-24, PA-24-250, and PA-24-260 airplanes. This AD was prompted by reports of cracks developing in the stabilator horn assembly. This AD requires replacement of the stabilator horn assembly and/or repetitive inspections of the stabilator horn assembly for corrosion or cracks, as applicable. Corrosion or cracks could lead to failure of the stabilator horn. Consequently, failure of the stabilator horn could lead to a loss of pitch control in flight. We are issuing this AD to correct the unsafe condition on these products. This book contains: - The complete text of the Airworthiness Directives - Piper Aircraft, Inc. Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: The Law The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727241242
Category :
Languages : en
Pages : 28
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Book Description
Airworthiness Directives - Various Aircraft Equipped With Wing Lift Struts (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - Various Aircraft Equipped With Wing Lift Struts (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are superseding Airworthiness Directive (AD) 99-01-05 R1, which applied to certain aircraft equipped with wing lift struts. AD 99-01-05 R1 required repetitively inspecting the wing lift struts for corrosion; repetitively inspecting the wing lift strut forks for cracks; replacing any corroded wing lift strut; replacing any cracked wing lift strut fork; and repetitively replacing the wing lift strut forks at a specified time for certain airplanes. This new AD retains all requirements of AD 99-01-05R1 and adds additional airplane models to the Applicability section. This AD was prompted by a report that additional Piper Aircraft, Inc. model airplanes should be added to the Applicability section. We are issuing this AD to correct the unsafe condition on these products. This book contains: - The complete text of the Airworthiness Directives - Various Aircraft Equipped With Wing Lift Struts (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 102
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Book Description
Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727237054
Category :
Languages : en
Pages : 48
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Book Description
Airworthiness Directives - Bombardier Model CL 600 2B19 (Regional Jet Series 100 and 440) Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - Bombardier Model CL 600 2B19 (Regional Jet Series 100 and 440) Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: This book contains: - The complete text of the Airworthiness Directives - Bombardier Model CL 600 2B19 (Regional Jet Series 100 and 440) Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727236699
Category :
Languages : en
Pages : 36
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Book Description
Airworthiness Directives - Boeing Co. Model 737-600, -700, -700C, -800, and -900 Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - Boeing Co. Model 737-600, -700, -700C, -800, and -900 Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are revising an earlier proposed airworthiness directive (AD) for the products listed above. That NPRM proposed to require installation of an automatic shutoff system for the center tank fuel boost pumps, installation of a placard in the airplane flight deck if necessary, and concurrent modification of the P5-2 fuel control module assembly. That NPRM also proposed to require revisions to the Limitations and Normal Procedures sections of the airplane flight manual to advise the flightcrew of certain operating restrictions for airplanes equipped with an automated center tank fuel pump shutoff control. Additionally, that NPRM proposed to require a revision to the Airworthiness Limitations (AWL) section of the Instructions for Continued Airworthiness (ICA) to incorporate AWL No. 28-AWL-19 and No. 28-AWL-23. That NPRM further proposed to require installation of a secondary control relay for the electrical control circuit of each of the two center tank fuel boost pumps. That NPRM was prompted by fuel system reviews conducted by the manufacturer. This action revises that NPRM by adding airplanes, adding additional operational testing of the automatic shutoff system for certain airplanes, removing the requirement for incorporating AWL No. 28-AWL-19 into the AWL section of the ICA, and adding an option of installation and maintenance of universal fault interrupters using a certain supplemental type certificate. We are proposing this supplemental NPRM to prevent center tank fuel pump operation with continuous low pressure, which could lead to friction sparks or overheating in the fuel pump inlet that could create a potential ignition source inside the center fuel tank. These conditions, in combination with flammable fuel vapors, could result in a center fuel tank explosion and consequent loss of the airplane. Since these actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes. This book contains: - The complete text of the Airworthiness Directives - Boeing Co. Model 737-600, -700, -700C, -800, and -900 Series Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 12
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Book Description
Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 12
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Book Description
Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727240603
Category :
Languages : en
Pages : 30
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Book Description
Airworthiness Directives - The Boeing Company Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - The Boeing Company Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are superseding airworthiness directive (AD) 2004-18-06 for certain The Boeing Company Model 737-200, -200C, -300, -400, and -500 series airplanes. AD 2004-18-06 required repetitive inspections to find fatigue cracking of certain upper and lower skin panels of the fuselage, and follow-on and corrective actions if necessary. AD 2004-18-06 also included a terminating action for the repetitive inspections of certain modified or repaired areas only. This new AD adds new inspections for cracking of the fuselage skin along certain chem-milled lines, and corrective actions if necessary. This new AD also reduces certain thresholds and intervals required by AD 2004-18-06. This AD was prompted by new findings of vertical cracks along chem-milled steps adjacent to the butt joints. We are issuing this AD to detect and correct fatigue cracking of the skin panels, which could result in sudden fracture and failure of the skin panels of the fuselage, and consequent rapid decompression of the airplane. This book contains: - The complete text of the Airworthiness Directives - The Boeing Company Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
Author: The Law Library
Publisher: Createspace Independent Publishing Platform
ISBN: 9781727240719
Category :
Languages : en
Pages : 30
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Book Description
Airworthiness Directives - The Boeing Company Model Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) The Law Library presents the complete text of the Airworthiness Directives - The Boeing Company Model Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition). Updated as of May 29, 2018 We are superseding an existing airworthiness directive (AD) for certain The Boeing Company Model 737-100 and -200 series airplanes. The existing AD currently requires various inspections for cracks in the outboard chord of the frame at body station (BS) 727 and in the outboard chord of stringer (S) 18A, and repair or replacement of cracked parts. This new AD adds airplanes to the applicability statement in the existing AD and adds inspections for cracks in the BS 727 frame outboard chords and the radius of the auxiliary chord, for certain airplanes. This new AD also removes the inspections of the outboard chord of S-18A required by the existing AD. This AD was prompted by several reports of fatigue cracking in the frame outboard chord at BS 727 and in the radius of the auxiliary chord on airplanes that were not affected by the existing AD. We are issuing this AD to detect and correct fatigue cracking of the outboard and auxiliary chords, which could result in reduced structural integrity of the outboard chord and consequent rapid decompression of the airplane. This book contains: - The complete text of the Airworthiness Directives - The Boeing Company Model Airplanes (US Federal Aviation Administration Regulation) (FAA) (2018 Edition) - A table of contents with the page number of each section
