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NONDESTRUCTIVE TEST (NDT) MANUALManual No.: 2-120483-800This document and all information and expression contained herein are the property of B/E Aerospace, Inc., and shall not be disclosed in whole orin part or used for design or installation except when such user possesses direct, written authorization from B/E Aerospace, Inc.Export Sensitive:Information contained herein is subject to United States Government Export Regulations. This data may not be resold, diverted, transferred,transshipped, made available to a foreign national within the United States, or otherwise disposed of in any other country outside of its intendeddestination, either in original form or after being incorporated through an intermediate process into other data without the prior written approval ofthe appropriate U.S. Government agency with jurisdiction over the content of this export.TP-1Mar 29/16
The NDT Manual is furnished either as a printed manual, digital product, or any combination of thetwo. This manual is reissued with all obsolete data deleted and all updated pages added.Changes are indicated on the List of Effective Pages (LEP). The pages that are altered will beidentified on the LEP by an “R” (Revised), “A” (Added), “O” (Overflow – changes to the documentstructure and/or page layout), or “D” (Deleted). Each page in the LEP is identified by Subject, PageNumber, and Page Date.Replaced or obsolete pages should be removed and destroyed.The NDT Manual is kept by revision service. A list of effective pages is provided with each revision.To obtain the latest revision to the manual contact:B/E Aerospace3110 Commerce ParkwayMiramar, FL 33025USAPhone: 954-443-4530Fax: 954-443-4963www.beaerospace.comTP-2Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALREVISION HISTORYRevisionDescriptionDateIRInitial Release.May 14, 2013AReformat of the manual from a collection of individual documents toa complete manual with List of Effective Pages.The content of the previous individual documents remainsunchanged.Sept. 23, 2013BComplete revision of section 51-EQ-03/301.Nov. 20, 2013CChange in manual owner from EMTEQ to B/E Aerospace. Replaceall references to EMTEQ with B/E Aerospace. Change EMTEQ logoto B/E Aerospace logo.There are no changes to the published inspection procedures madeby this revision of the manual.Mar. 29, 2016Manual No.: 2-120483-800RH-1Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALRECORD OF REVISIONSRetain this record in the front of the manual. On receipt of revisions, insert pages in the manual. Enterrevision number, date issued, date inserted and initials.Rev.DateIssuedIRMay 14/12ASept 23/13BNov 20/13CMar 29/16DateInsertedManual No.: 2-120483-800ByRev.DateIssuedDateInsertedByRR-1Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALRECORD OF TEMPORARY REVISIONSRetain this record in the front of the manual. On receipt of temporary revisions, insert pages in themanual. Enter temporary revision number, date issued, date inserted and initials.Temporary RevisionNo.:DateManual No.: 2-120483-800InsertedDateTemporary RevisionByNo.:DateInsertedDateByRTR-1Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALLIST OF EFFECTIVE PAGESSUBJECT/CHAPTERTitle PagePAGEDATESUBJECT/CHAPTERPAGEDATETP-1RMar 29/16122RMar 29/16TP-2RMar 29/16123RMar 29/16Revision HistoryRH-1RMar 29/16124RMar 29/16Record of RevisionRR-1RMar 29/16125RMar 29/16Record of TemporaryRevisionRTR-1AMar 29/16126RMar 29/16127RMar 29/16List of Effective PagesLEP-1RMar 29/16128RMar 29/16LEP-2RMar 29/16129RMar 29/16LEP-3RMar 29/16130RMar 29/16TOC-1RMar 29/16131RMar 29/161RMar 29/16132RMar 29/16133RMar 29/16134RMar 29/16135RMar 29/16136RMar 29/16137RMar 29/16138RMar 29/16139RMar 29/16140RMar 29/16141RMar 29/16142RMar 29/16143RMar 29/16144RMar 29/16Table of ContentIntroductionEDDY CURRENTGeneral InformationManual No.: 2-120483-80051-EQ-01101RMar 29/16102RMar 29/16103RMar 29/16104RMar 29/16105RMar 29/16106RMar 29/16107RMar 29/16108RMar 29/16109RMar 29/16110RMar 29/16111RMar 29/16112RMar 29/16113RMar 29/16114RMar 29/16115RMar 29/16116RMar 29/16117RMar 29/16118RMar 29/16119RMar 29/16120RMar 29/16121RMar 29/16Equipment SuppliersAluminum partsubsurface inspectionMultilayer51-EQ-02201RMar 29/16202RMar 29/16203RMar 29/1651-EQ-03301RMar 29/16302RMar 29/16303RMar 29/16304RMar 29/16LEP-1Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALSUBJECT/CHAPTERAluminum Parts SurfaceInspection(Meter Display)Aluminum PartsFastener Hole Inspection(Impedance Plane)Manual No.: 2-120483-800PAGEDATESUBJECT/CHAPTERPAGEDATE305RMar 29/16506RMar 29/16306RMar 29/16507RMar 29/16307RMar 29/16508RMar 29/16308RMar 29/16509RMar 29/16308RMar 29/16510RMar 29/16309RMar 29/16310RMar 29/16311RMar 29/16312RMar 29/16Aluminum Part FastenerHole Inspection (RotaryScanner)51-EQ-0451-EQ-06601RMar 29/16602RMar 29/16603RMar 29/16604RMar 29/16401RMar 29/16605RMar 29/16402RMar 29/16606RMar 29/16403RMar 29/16607RMar 29/16404RMar 29/16608RMar 29/16405RMar 29/16609RMar 29/16406RMar 29/16610RMar 29/16407RMar 29/16611RMar 29/16408RMar 29/16409RMar 29/16410RMar 29/16411RMar 29/16412RMar 29/16413RMar 29/16414RMar 29/16415RMar 29/16416RMar 29/16417RMar 29/1651-EQ-05501RMar 29/16502RMar 29/16503RMar 29/16504RMar 29/16505RMar 29/16Surface CrackInspection of FayingSurfaceDetection of Cracks atEdge of Cutouts51-EQ-07701RMar 29/16702RMar 29/16703RMar 29/16704RMar 29/16705RMar 29/16706RMar 29/1651-EQ-08801RMar 29/16802RMar 29/16803RMar 29/16804RMar 29/16805RMar 29/16806RMar 29/16807RMar 29/16LEP-2Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALSUBJECT/CHAPTERPAGEDATE808RMar 29/16809RMar 29/16810OMar 29/16SUBJECT/CHAPTERPAGEDATEPENETRANTMethod of InspectionManual No.: 2-120483-80051-EQ-09901RMar 29/16902RMar 29/16903RMar 29/16904RMar 29/16905RMar 29/16906RMar 29/16907RMar 29/16908RMar 29/16909RMar 29/16LEP-3Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALTABLE OF CONTENTSINTRODUCTION . 1EDDY CURRENTGENERAL INFORMATION . 101EQUIPMENT SUPPLIERS . 201ALUMINUM PART SUBSURFACE INSPECTION – MULTILAYER . 301ALUMINUM PARTS SURFACE INSPECTION (METER DISPLAY) . 401ALUMINUM PARTS FASTENER HOLE INSPECTION (IMPEDANCE PLANE DISPLAY) 501ALUMINUM PART FASTENER HOLE INSPECTION (ROTARY SCANNER) . 601SURFACE CRACK INSPECTION OF FAYING SURFACE . 701DETECTION OF CRACKS AT EDGE OF CUTOUTS . 801PENETRANTMETHOD OF INSPECTION . 901Manual No.: 2-120483-800TOC-1Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALINTRODUCTION1. GeneralA. Detection of structural damage and defects before they deteriorate to a critical state is a necessity toassure structural integrity of the aircraft. Inspection techniques to discover such defects are presented inthis manual; Eddy Current & Penetrant. As other methods of tests are found adequate, they will beadded to this manual.B. The intent of this manual is to provide nondestructive testing methods to support B/E Aerospace DesignApprovals (e.g. Supplemental Type Certificates (STC)) only.2. Manual ArrangementA. This manual is broken into two separate parts, Eddy Current test and Penetrant test. They containspecific information and procedures pertaining to each test method. The aircraft maintenance personnelperforming these tests are required to be adequately trained in the test methods and test equipmentdescribed in this manual, no effort is being made to include instructions for operating the various typesof equipment used for the tests. However, where needed specific operating procedures are suggested.3. Subject NumberingA. Each part of this manual is subdivided by the use of the three-element pseudo ATA-100 numberingsystem (e.g. 51-EQ-08). First number denotes the ATA chapter the second denotes it is a B/EAerospace procedure, and the third denotes the subject number.4. List of Effective PagesA. A List of Effective Pages at the front of the manual lists all of the pages contained in the manual andindicates the date of which the page was last revised.INTRODUCTIONManual No.: 2-120483-800Page 1Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUALGENERAL INFORMATION1. GeneralA. This subject describes the functions and features of equipment and materials necessary to conductEddy Current tests. Equivalent test instruments, (Table 101), are allowable provided that all tests, asdefined in each procedure, can be performed with the same results. Other equivalent material andequipment substitutes may also be used. Specific inspections may require equipment and materials notlisted here, but described in the specific document.B. The requirements of this subject should be followed unless otherwise noted by a specific document.2. Flaw Detection SystemsA. Meter Display Instrument (Ref. Figure 101)(1) Description(a) Meter display instruments feature a scale usually graduated in milliamperes and movablemeter needle. The amplitude of needle movement is proportional to the impedance of the testcircuit. The electronics of some instruments can be switched to allow the meter to indicatePhase angle. Some instruments have dual meters, one indicating milliamperes and oneindicating phase angle.NOTE: Meter display instruments are acceptable for flaw detection only when used inconjunction with an appropriately adjusted audio or visual flaw alarm.(2) Required Features(a) Frequency range and sensitivity required by specific test.(b) Adjustable Audio or Visual defect alarm.1)Alarm activation must not affect the display needle position.(c) Lift-off effect suppression to not more than 10% of reference standard notch response.(d) Circuitry to support reflectance (Driver/Receiver) probes if instrument is to be used for suchtests.(3) Desirable Features(a) Indication recording capability.(b) Phase rotation capability.B. Impedance Plane Display Instrument (Ref. Figure 101)(1) Description(a) Impedance plane display instruments feature a “flying dot" on a CRT, LCD, or video display.The position of the flying dot indicates the impedance of the test circuit, but also displays theeffect of both resistance and reactance presenting both phase and amplitude information. Theresultant information often creates unique signatures of different conditions influencing thesensor, such as conductivity, permeability, cracks, liftoff, spacing, and thinning, makingrecognition of defects easier and more reliable. Indications are displayed in "real Time" andcan be stored for variable lengths of time to reduce the risk of missing defect indications.(2) Required Features(a) Frequency range and sensitivity required by specific test(b) Display presentation storage capabilityEFFECTIVITYEDDYALL AIRCRAFTCURRENTManual No.: 2-120483-80051-EQ-01Page 101Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUAL(c) Phase rotation capability(d) Circuitry to support reflectance (Driver/Receiver) probes if instrument is to be used for suchtests.(3) Desirable Features(a) Separately adjustable X and Y gain in .5V per division steps.(b) Indication recording capability.(c) Motorized open hole probe scanner with time base display.C. Linear Time Base Display Instruments (Ref. Figure 103)(1) Description(a) Linear time base display instruments are usually used with rotating open hole probe scanners.The horizontal position of the signal on the display indicates sensor clock position in the holeand the vertical peak of the signal indicates amplitude of the response.(2) Required Features(a) Same as those of the impedance plane display instrument.(b) Adjustable filters for noise reduction.(3) Desirable Features(a) Indication recording capability(b) Switchable to impedance plane display for further signal analysisD. Bargraph Display Instruments (Ref. Figure 104)(1) Description(a) Bargraph display Instruments feature an LCD readout bar scale graduated in voltage sensitiveincrements. The position of the display indication is adjustable from one bar to full scale.(2) Required Features(a) Frequency range and sensitivity required by a specific test.(b) Signal-to-noise ratio of at least 3-to-1(3) Desirable Features(a) Adjustable audio or visual defect alarm1)Alarm activation must not affect display bar scale position.E. Probes(1) Required Features(a) Compatibility with instrument used (indicated by sensitivity, stability and lift off characteristics).EFFECTIVITYALL AIRCRAFT1)Many probes work equally well with instruments marketed by several differentmanufactures (sometimes requiring only connector adapters).2)Some probes work only with an instrument produced by one manufacturer, but theprobes are manufactured by several sources.3)Some probes are designed for a particular instrument, but will work with others if usedwith special adapters incorporating balance or trimmer coils.EDDY CURRENTManual No.: 2-120483-80051-EQ-01Page 102Mar 29/16
NONDESTRUCTIVE TEST (NDT) MANUAL4)If doubt exists about applicability, contact the probe and instrument manufacturers.(b) Manufacturer part number and nominal frequency range marked on probe (or on integralinstrument connector/lead assembly if probe marking not practical).(c) Stability and low noise throughout usable frequency range, producing at least a 3 to 1 systemsignal to noise ratio.(2) Desirable Features(a) Probes incorporating removable leads are often preferred for the following reasons:1)Reduce storage space required and less storage damage.2)Promote prompt correction of system noise caused by faulty leads (system weak link).3)Easier and more economical to repair in the field than integral leads.(b) Probe coil(s) should be shielded whenever possible to reduce effects of
B Complete revision of section 51-EQ-03/301. Nov. 20, 2013 C Change in manual owner from EMTEQ to B/E Aerospace. Replace all references to EMTEQ with B/E Aerospace. Change EMTEQ logo to B/E Aerospace logo. There are no changes to the published inspection procedures made by this revision of the manual. Mar. 29, 2016 . NONDESTRUCTIVE TEST (NDT) MANUAL RR-1 Manual No.: 2-120483
