767-200/300/300F/400ER AIRWORTHINESS LIMITATIONS767-200/300/300F/400ERAIRWORTHINESS LIMITATIONS (AWLs)D622T001-9-01JUNE 2019This document has EAR data with an Export Control Classification Number (ECCN) of 9E991.Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used fordevelopment, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws.Boeing claims copyright in each page of this document on to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collectivework. This document includes proprietary information owned by the Boeing Company and/or one or more third parties. Treatment of the document and the information it contains is governed by contract withBoeing. For more information, contact the Boeing Company, P.O. Box 3707, Seattle WA 98124. Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, BBJ, DC-8,DC-9, DC-10, MD-10, MD-11, MD-80, MD-88, MD-90, and the red-white-blue Boeing livery are all trademarks owned by The Boeing Company; no trademark license is granted in connection with thisdocument unless provided in writing by Boeing.COMPILED AND PUBLISHED BY:MAINTENANCE PROGRAMS ENGINEERINGBOEING COMMERCIAL AIRPLANE GROUPSEATTLE, WASHINGTONJUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-1
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767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSTABLE OF CONTENTSREVISIONS . 1.0-5LIST OF EFFECTIVE PAGES . 1.0-18A. SCOPE . 1.0-19B. AIRWORTHINESS LIMITATIONS - STRUCTURAL INSPECTIONS. 1.0-20C. AIRWORTHINESS LIMITATIONS - STRUCTURAL SAFE LIFE PARTS . 1.0-93D. AWLS - STRUCTURAL LIMIT OF VALIDITY (LOV). 1.0-95APPENDIX A – STRUCTURES BASELINE REQUIREMENTS. A.0-1A. SCOPE. A.0-1B. STRUCTURES BASELINE INSPECTION REQUIREMENTS . A.1-1JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-3
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767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSREVISIONSJULY 2014Original ReleaseThis revision contains no technical changes.Please see the 767 MPD Section 9, D622T001-9 for historical Revision Log information.NOVEMBER 2014Revised Subsection B. Airworthiness Limitations - Structural Inspections to add a paragraph which addresses special inspection requirements for operators that have incorporatedService Bulletin 767-23-0228.DECEMBER 2014Added a new Section D. AWLs - Structural Limit of Validity (LOV) as required by Title 14 Code of Federal Regulations (CFR) Section 26.21 (Amendment 26-6).FEBRUARY 2015Revised Structural Safe Life Parts section by reformatting for clarification and updating the 767-400ER life limits based on completion of the main landing gear full-scale fatigue testsand analysis.OCTOBER 2015Revised SSI 52-30-I02A to reflect changes made to the DTR Check Form requirements.Added SSI 57-10-I03B - Rear Spar Lower Chord and Skin - Wing Center Section - Hidden Locations - BBL 49.5, 62.05 and 73.0 for the -200SF and -300BCF to the table ofAirworthiness Limitations - Structural Inspections in Section B.Added Item 5 to the Table Notes for the Airworthiness Limitations - Structural Inspections Table and added a footnote to the following SSI Items affected by this new note: 57-10I01A, 57-10-I02C, 57-10-I03A, 57-10-I03B, 57-10-I03C, 57-10-I20A, 57-10-I24A, 57-20-I12C, 57-20-I15J, and 57-20-I16K.DECEMBER 2015Revised Section D. AWLs - Structural Limit of Validity (LOV) to add applicability for the 767-300BCF.JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-5
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2016Deleted the FAA Approval signature column from the Revision Log to improve the layout and provide consistency across all Section 9/AWL/CMR/SCI documents. Submittalsignatures will no longer be included in the Revision Log.Revised front matter under “REMOVAL OF EXCESS SEALANT WHEN INSPECTING” to update the reference to sealant of fuel tank fasteners to point to the 767 Special ComplianceItems/Airworthiness Limitations document, D622T001-9-04.Revised the Airworthiness Limitations - Structural Inspections Table in Section B by adding SSI 53-30-I08A - Fuselage Circumferential Skin and Stringer Splice - BS 434 for the767-300F, L/N 1108 and on.Revised SSI 57-53-I03I.2 to combine SSI/DTR Forms and their requirements into one SSI/DTR Form to cover all aircraft and added #5 Inboard Flap Support to the title forclarification.Revised SSI 57-53-I03J.1 to combine with SSI 57-53-I03J.2 DTR Form and their requirements into one SSI/DTR Form to cover all aircraft and added #5 Inboard Flap Support to thetitle for clarification and removed Flag Note 2 .Revised SSI 57-53-I03J.2 to combine SSI/DTR Forms and their requirements into one SSI/DTR Form to cover all airplane models and added #5 Inboard Flap Support to the titlefor clarification.Revised SSI 57-53-I03K to combine SSI/DTR Forms and their requirements into one SSI/DTR Form to cover all aircraft and added #5 Inboard Flap Support to the title for clarification.Deleted SSI 57-53-I03L.1 and 57-53-I03L.2 as those requirements are now covered in SSI 57-53-I03L.Revised SSI 57-53-I03L to combine SSI/DTR Forms and their requirements into one SSI/DTR Form to cover all aircraft and added #5 Inboard Flap Support to the title for clarification.JULY 2018Revised document header from 767 to 767-200/300/300F/400ER to list all derivatives.Revised Section A. Scope to add requirement for document to be used in its entirety. Added guidelines that provides a 24 month grace period of change incorporation.Revised Section B reference document names for consistency within this document. Revised to address the inclusion of Appendix A being added to the document to define thebaseline inspection program. Revised Threshold section to clarify A-Check and C-check inspection interval, after reaching threshold, to be 3,000 flight cycles, 24 months or 9,000flight hours for the C-check, and 300 flight cycles or 900 flight hours for the A-check. Revised structural inspection results reporting instructions. The manager of the FAA OversightOffice, the Transport Airplane Directorate, and the FAA have been removed from the list of required recipients. Revised Removal of Excess Sealant When Inspecting to add excesssealant removal instructions and added a table with detailed descriptions table for Excess Sealant. Added the word “Fuselage” to the beginning of phrase “Structural Inspections “regarding the Airworthiness Limitations document for the 767-300BCF.Revised definition of 767-300, 767-300ER from “300” to “300 PASS”, for clarity.Removed the two notes stating that some ALIs for the 767-200SF and 767-300BCF do not have corresponding DTR check forms. This is to clarify that all 200SF and 300BCF ALIsare included in the DTR Check Form Document.Removed "No DTR Check Form" notes from ALIs table to clarify that all ALIs are included in the DTR Check Form Document.(Continued on next pageJUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-6
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 52Revised the following SSIs to include the intercostal numbers for the inspection area:52-30-I05B52-30-I07B52-30-I09BRevised SSI 52-30-I07B to correct an error in the July 2016 revision of this document by adding 300F to the Type and Threshold column.Revised the following SSIs to remove the Flagnote 2 as inspection procedures for these items have been published in the applicable 767 Non-Destructive Testing 30-I07E52-30-I07FATA 53Revised 137 SSIs to make clarifications.Added the following 6 new -I29/53-60-I3153-50-I29A53-50-I29Ball 767 modelsall 767 modelsall 767 models except 767-300Fall 767 modelsall 767 models767-300 PassengerDeleted the following 3 SSIs:53-30-I01767-200SF item SF8A53-30-I01767-200SF item SF8B53-60-I29FFuselage frame inspections for the 767-200SF and 767-300BCF were reorganized and simplified such that 5 SSIs were merged into other existing SSIs. As a result, updates havebeen made to the SSI number and the Airplane/Engine Applicability of some of these SSIs.The updated 767-200SF fuselage frame inspection SSIs are the -I08A767-200SF53-10-I08B767-200SF and 767-300BCF item BCF353-10-I08C/53-30-I24C/53-60-I08C767-200SF and 767-300BCF item BCF553-30-I24C/53-60-I08C767-200SF and 767-300BCF item BCF6(Continued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-7
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 53, ContinuedThe updated 767-300BCF fuselage frame inspection SSIs are the following:53-30-I24A/53-30-I24B/53-50-I01A /53-50-I02A /53-60-I08A767-300BCF item BCF153-30-I24A/53-30-I24B767-300BCF item BCF2/BCF453-10-I08B767-200SF and 767-300BCF item BCF353-10-I08C/53-30-I24C/53-60-I08C767-200SF and 767-300BCF item BCF553-30-I24C/53-60-I08C767-200SF and 767-300BCF item BCF6The following 13 767-200SF SSIs, that had 767-200SF listed under the Airplane/Engine Applicability for a similar SSI on another airplane model, were separated into their own lineitem. This was done to clarify the difference between the DTR Check Form for the 767-200SF and the other 767 models in the D622T001-DTR 3-60-I06B53-60-I06C53-60-I06D53-60-I10767-200SF item SF2The threshold for SSI 53-60-I06B (767-200SF item) was changed from 40,000 cycles to 50,000 cycles.Of the 137 SSIs that were revised for clarifications, the following SSIs were changed more significantly than minor clarifications:The airplane model applicability was changed for the following 6 SSIs:53-30-I04ARHS I19AF153-50-I19(Continued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-8
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 53, ContinuedRevised the following 13 SSIs to change the inspection region:53-10-I10B53-30-I01767-200SF item 53-50-I06C767-200SF53-60-I10767-300BCF item BCF253-60-I10767-200SF item SF253-60-I10C53-60-I29A53-60-I29B53-60-I29DRevised the following SSIs to add or update required Flagnotes in the Airplane/Engine -10-I14A53-10-I20C53-10-I21ALine numbers 1- 75753-10-I21ALine numbers 758 and E53-30-I19F53-30-I19AD53-30-I20A53-30-I22D767-300 tinued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-9
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 53, ContinuedRevised the following SSIs to add or update required Flagnotes F and All 53-60-I06E53-60-I10C53-60-I14F53-60-I27A767-300 -80-I01CRevised the following SSIs to remove -80-I17(Continued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-10
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 54Revised 20 SSIs to clarify the title.Revised 59 SSIs to clarify the notes.Revised the following SSIs to change the recommended inspection 80C (Except 400E)54-50-I01cCF6-80C (400E) 8 Hours54-50-I03b52454-50-I04cCF6-80C (400E) 8 Hours54-50-I04eCF6-80C (400E) 8 Hours54-50-I17eCF6-80C (400E) 8 Hours54-50-I17eCF6-80C (400E) 8 Hours54-50-I17fCF6-80C (400E) 8 HoursRevised the following SSIs to change the recommended inspection type:54-50-I01cCF6-80C (400E) 8 Hours54-50-I04cCF6-80C (400E) 8 Hours54-50-I04eCF6-80C (400E) 8 4-50-I06CF6-80C (Except 400E)54-50-I10bCF6-80C (400E) 8 Hours54-50-I10bCF6-80C (400E) 8 Hours54-50-I14CF6-80C (400E) 8 Hours54-50-I14CF6-80C (400E) 8 Hours54-50-I17eCF6-80C (400E) 8 Hours54-50-I17fCF6-80C (400E) 8 Hours54-50-I18CF6-80C (400E) 8 Hours54-50-I18CF6-80C (400E) 8 Hours(Continued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-11
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 54, ContinuedAdded the following SSIs:54-50-I01d80C (400E) 8 Hours54-50-I01d80C (400E) 8 Hours54-50-I01e80C (400E)54-50-I13f80C (400E) 8 Hours54-50-I13f80C (400E) 8 Hours54-50-I16f80C (400E)54-50-I17gCF6-80C (400E) 8 Hours54-50-I17gCF6-80C (400E) 8 HoursRevised the following SSIs to add Flagnote 2 in the Airplane/Engine Applicability d the following SSIs to remove the Flagnote 2 as inspection procedures for these items have been published in the applicable 767 Non-Destructive Testing 50-I04a80C (400E)54-50-I04c80C (400E)54-50-I04e80C 0580C (Except 400E)54-50-I05a80C (400E)54-50-I06a80C (400E)54-50-I06c80C (400E)54-50-I06d80C (400E)54-50-I09a/I07/I08/I1280C (400E)54-50-I1052454-50-I10b80C (400E)54-50-I12b80C 1380C54-50-I13a80C (400E)(Continued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-12
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 54, ContinuedRevised the following SSIs to remove the Flagnote 2 as inspection procedures for these items have been published in the applicable 767 Non-Destructive Testing Manual,Continued:54-50-I13e80C (400E)54-50-I1480C (400E)54-50-I16a80C (400E)54-50-I16e80C (400E)54-50-I17a80C (400E)54-50-I17c80C (400E)54-50-I17e80C (400E)54-50-I17f80C (400E)ATA 55Revised 2 SSIs to clarify the titles.ATA 57Revised 180 SSIs to clarify the titles.Revised 23 SSIs to clarify the zones.Revised the following SSIs to clarify the data in the Airplane/Engine Applicability Column (as described):57-10-I03A200ER/300ER with center section fuel, with stage length 8 hours57-10-I03A200ER/300ER with center section fuel, with stage length 8 hours57-10-I03B200ER/300ER with center section fuel, with stage length 8 hours57-10-I03B200ER/300ER with center section fuel, with stage length 8 hours57-10-I03C200ER/300ER with center section fuel, with stage length 8 hours57-10-I03C200ER/300ER with center section fuel, with stage length 8 hours57-10-I24all except 200SF and 300BCF with stage length 8 hours57-10-I24all except 200SF and 300BCF with stage length 8 hours57-53-I04Yall except 400ERRevised the following SSIs to replace Flagnote 5 with Flagnote 6 in the Type and Threshold Column, to correct the inspection threshold:57-10-I03A200SF & 300BCF57-10-I03B200SF & 300BCF57-10-I03C200SF & 300BCF57-20-I15J200SF & 300BCF57-20-I16K200SF & 300BCF(Continued on next page)JUN 2019D622T001-9-01BOEING PROPRIETARY - Copyright (c) - Unpublished Work - See title page for detailsEXPORT CONTROLLED - EAR ECCN: 9E991Page 1.0-13
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONSJULY 2018, ContinuedATA 57, ContinuedRevised the following SSIs to add Flagnote 6 in the Type and Threshold Column, to correct the inspection threshold:57-20-I15K200SF & 300BCF57-20-I16L200SF & 300BCFRevised SSI 57-10-I02 for the 400ER to be applicable to airplanes with stage length 8 hours.Added SSI 57-10-I02 for the 400ER with stage length 8 hours.Revised SSI 57-20-I15E to remove 400ER effectivity for airplanes with stage length 8 hours and airplanes with stage length 8 hours.Revised the two SSIs for 57-20-I27 to combine SSI 57-20-I27 "for airplanes with stage length 8 hours" with SSI 57-20-I27 "for airplanes with stage length 8 hours.Revised SSI # for SSI 57-53-I03F - Inboard Flap Box Support No. 3/6 - Flap Attachment Bolts, IFS 251.25 to SSI 57-53-I03F.1 to differentiate it from bolt shank inspections.Revised SSI # for SSI 57-53-I03F - Inboard Flap Support No. 3/6 - Flap Attachment Bolts - Shank Location to SSI 57-53-I03F.2 to differentiate it from SSI 57-53-I03F.1Revised the threshold for SSI 57-10-I08 to correct a typographical error from 70,000 flight hours to 80,000 flight hours.Revised the following SSIs to add Flagnote 2 in the Airplane/Engine Applicability Column:57-20-I07400ER, and all airplane types L/N 922 and laterRevised the following SSIs to remove the Flagnote 2
Revised SSI 57-53-I03K to combine SSI/DTR Forms and their requirements into one SSI/DTR Form to cover all aircraft and added #5 Inboard Flap Support to the title for clarification. Deleted SSI 57-53-I03L.1 and 57-53-I03L.2 as those requirements are now covered in SSI 57-53-I03L.
Certification and Continuing Airworthiness, včetně Amendmentu 1. Dokument ICAO Airworthiness Manual (Doc 9760), Volume II byl vytvořen na základě materiálů obsažených v dokumentech Manual of Procedures for an Airworthiness Organization (Doc 9389), Continuing Airworthiness Manual (Doc 9642) a Airworthiness Techn
767 maintenance planning data d622t001-9 boeing proprietary - copyright (c) - unpublished work - see title page for details page 9.0-1 767 maintenance planning data (mpd) document section 9 airworthiness limitations (awls) and certification maintenance requirements (cmrs) d622t001-9 february 2014 compiled and published by: maintenance programs .
Continued airworthiness standards The current international standards for the continued airworthiness of aircraft are defined in the ICAO Airworthiness Manual (Doc 9760) published in 2001 and in Annex 6 - Operation Footnote 3 With t
This, Instructions for Continued Airworthiness, is intended to supplement the Model AS350 rotorcraft maintenance manuals provided by Eurocopter. The information, procedures, requirements, and limitations contained in this, Instructions for Continued Airworthiness, for
Conc Diagram- All Failures Cispa Data Avalon Date PCB Lot Number Igarashi TPS date codes. MB Panel Number VIAS Hole Location Failure 9-June'09 11-June'09 923 162 12-June'09 923 163,164 TBD TBD 1 13-June'09 923 164 15-June'09 923 166 16-June'09 923 167 17-June'09 923 168,171 18-June'09 923 171 19-June'09 923 171 20-June'09 923 171 22-June'09 923 173 23-June '09 923 179 24-June '09 923 .
(STANAG 4746) Airworthiness, “Lite” UAS (STANAG 4703) Airworthiness, Rotary Wing (STANAG 4702) Airworthiness, Fixed Wing (STANAG 4671) Weapons Integ. (STANAG 4737) Interoperability, (STANAG 4586) Data Link (STANAG 4660) Command & Control . C2 . ISR Data NATO Standardization Activities.
Maintenance Manual (MM) for the tailBeacon UAT transmitter as installed under STC SA04427CH. This document satisfies the requirements for continued airworthiness as defined by 14 CFR Part 23.1529 and Appendix A. Information in this document is required to maintain the continued airworthiness of the tailBeacon UAT transmitter. 5.1 Publications
used when setting windows hooks . Relies on the user api hook . User Api Hook Special hooking mechanism introduced to support Windows themes RegisterUserApiHook Can only be registered by privileged processes Requires the TCB privilege Caller must be running as SYSTEM Allows Windows to load a theme client module into every GUI application . Smashing the Atom . Theme Subsystem Introduced in .