Reference Standard

MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 7075-T6 ALUMINUM PER QQ-Q-250/12.

MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 4340

MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 4340 STEEL PER MIL-S-5000

MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 ALUMINUM BRONZE

MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 303SE CRES or 301 1/2 HARD CRES STEEL.

MCDONNELL DOUGLAS REFERENCE STANDARD 06-20-01 FIG.1 SHEETS 1-3. MATERIAL: 6AL-4V TITANIUM PER AMS 491 or MIL-T-9046

DOWTY AEROSPACE PROPELLERS PROBE GUIDE FIXTURE, SF340-61-A42

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628B FIG.603 SHEET 15C

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628D FIG.603 SHEET 15E

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 628D FIG.603 SHEET 15E

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 628F FIG.603 SHEET 15G

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 635 FIG.603 SHEET 23

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 636C FIG.603 SHEET 24

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 636C FIG.603 SHEET 24

DOUGLAS DC-10 WING CLEVIS REFERENCE STANDARD 6AL-6V or 6AL-4 TITANIUM, 54-10-11 PAGE 637 FIG.603 SHEET 25

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 639 FIG.603 SHEET 27

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 639 FIG.603 SHEET 27

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER)

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (LOWER)

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER)

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 640 FIG.603 SHEET 28 (UPPER)

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 641 FIG.603 SHEET 29

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 6AL-4V TITANIUM, 54-10-11 PAGE 641 FIG.603 SHEET 29

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 7075-T6 ALUMINUM, 54-10-11 PAGE 642 FIG.603 SHEET 30

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #1

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #2

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-18-53 #3

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4130 or 4340, 54-10-11 PAGE 651 FIG.603 SHEET 39, BOLT IDENTIFICATION 71658-7-35 #4

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 2024-T351 ALUMINUM, 54-10-11 PAGE 655 FIG.603 SHEET 43

DOUGLAS DC-10 WING PYLON REFERENCE STANDARD 4340 CARBON STEEL, 54-10-11 PAGE 617 FIG.603 SHEET 5

Boeing DC-9/MD-80 Reference Standard Design (1- Assembly) Figure 21, Sheet 1-5 Page 31-35, 7-5. Includes Test Report and Certificate of Conformance.

DC-3 REFERENCE STANDARD ..SECTION 3 PAGE 2 FIGURE 1.1

deHAVILLAND DASH 8 LFEC CALIBRATION STANDARD. PART 6 53-30-31 PAGE 7 FIGURE 3. Includes Test Report and Certificate of Conformance.

deHAVILLAND DASH 8 LFEC CALIBRATION STANDARD. PART 6 53-10-21 PAGE 5 FIGURE 3. Includes Test Report and Certificate of Conformance.

ALUMINUM BLOCK 2024-T3 3/64″ FLAT BOTTOM HOLE, 2.0″LX2.0″HX.375″W

EMBRAER 190/195 REFERENCE STANDARD, 190:00335-99999 OR POST-MOD SB 190-57-0031/02. PART 6 57-50-00, FIGURE 1-SHEET 1&2.

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .031″..Doubler = .040″..Filler = .031″..Stringer = .063″

EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .031″..Doubler 1 = .040″..Doubler 2 = .063″..Filler = ….

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .047″..Doubler = .050″..Filler = .047″..Stringer = .063″

EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .047″..Doubler 1 = .050″..Doubler 2 = .063″..Filler = ….

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .055″..Doubler = .063″..Filler = .055″..Stringer = .063″

EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .055″..Doubler 1 = .063″..Doubler 2 = .063″..Filler = ….

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .071″..Doubler = .080″..Filler = .071″..Stringer = .063″

EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .071″..Doubler 1 = .080″..Doubler 2 = .063″..Filler = ….

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .080″..Doubler = .098″..Filler = .080″..Stringer = .063″

EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .080″..Doubler 1 = .098″..Doubler 2 = .063″..Filler = ….

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-06-00 pages 6-9. Material: 2024-T3 Alclad Aluminum. Single Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .098″..Doubler = .110″..Filler = .098″..Stringer = .063″

EMBRAER 170/175 REFERENCE STANDARD PT 6 51-06-00 pages 7-10. Material: 2024-T3 Alclad Aluminum. Dual Doubler Configuration. Includes Test Report and Certificate of Conformance…Skin Thickness = .098″..Doubler 1 = .110″..Doubler 2 = .063″..Filler = ….

EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175 REFERENCE STANDARD DUAL DOUBLER CONFIGURATION PT 6 53-06-00 pages 6-10 REV.1, Material: 2024-T3 Alclad. Includes Test Report and Certificate of Conformance.

EMBRAER 190/195 REFERENCE STANDARD PT 6 53-23-00 pages 1-13. Material: 2024-T3 Alclad Aluminum. Repair Doubler Configuration. Includes Test Report and Certificate of Conformance. Repair Doubler = .125″ Fus Skin Thickness = .098″ Filler = .098″ Inner Doubler = .098″

EMBRAER 170/175 CALIBRATION STANDARD PT 4 54-50-00 Embraer 170 NDT 1967 Rev. 49, pages 11-13 and Embraer 175 NDT 5893 Rev. 25, pages 10-12. Includes Test Report and Certificate of Conformance.

EDDY CURRENT CIRCLE TEMPLATE, 0.750″Ø. 3 HOLE SIZES: .749″, .750″,.751″. MATERIAL: 2024-T351, 0.063″

EDDY CURRENT CIRCLE TEMPLATE, SELECT RIVET SIZES. 12 HOLE SIZES: .125″, .156″,.187″, .218″, .250″, .281″, .312″, .343″, .375″, .437″, .500″, .562″. MATERIAL: 2024-T351, 0.063″

EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 606

EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 615

Aeronautical Engineers Australia Reference Standard Fig.2 Page 5 DOC NO: MMS13829.001/1 and REF EO: EO13829.001/1

BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024″, .028″, .031″, .035″, .039″, .044″, .048″, .052″, .056″ .059″ +/-0.002, . PAD SIZE: 1.0″ x 1.0″ +/-0.010″, Material: 2024-T3 ALUMINUM. Chromic anodize and 1 coat of CMS 565-01 primer on chem mill side only. Chemical mill from stock thickness 0.063” (1.60 Includes certification Report Traceable to NIST and Certificate of Conformance(COC)

BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024″, .028″, .031″, .035″, .039″, .044″, .048″, .052″, .056″ .059″ +/-0.002, . PAD SIZE: 1.0″ x 1.0″ +/-0.010″, Material: 2124-T8 or 7075-T7 ALUMINUM. Chromic anodize and 1 coat of CMS 565-01 primer on chem mill side only. Chemical mill from stock thickness 0.063” (1.60 Includes certification Report Traceable to NIST and Certificate of Conformance(COC) Which Specifiy Conductivity Range of 35-45% IACS.

BRANTLY B2 MAIN ROTOR BLADE ROOT SKIN CALIBRATION STANDARD PG.2. MATERIAL: 2024-T3 ALUMINUM BARE & CLAD. Includes Test Report and Certificate of Conformance.

BRANTLY CALIBRATION STANDARD

CUSTOM SIKORSKY S61-N FLAT BOTTOM HOLE AFT REAR FUSELAGE REFERENCE STANDARD 51-10-05 FIGURE 7 (SHEETS 1-5). MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certiicate of Conformance.

MD REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02

CUSTOM EDDY CURRENT STANDARD, 2024-T351 ALUMINUM .063″/.050″. MS20426AD5 CSK RIVET 2 PLACES

REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.

REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DISBOND and CORE FIBERGLASS INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.

F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65

F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65

F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65

F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65

F15 REFERENCE STANDARD. MATERIAL: 2024-T3, OUTBOARD TORQUE BOX REAR SPAR, 68A115101, LOWER FLANGE FASTENER HOLES. Includes Test Report and Certificate of Conformance.

F15 REFERENCE STANDARD,6AL-4V 1F-15A-36

F15 REFERENCE STANDARD,6AL-4V

BOEING REFERENCE STANDARD. MATERIAL: 6AL-4V TITANIUM ROUND 2.50″ DIAMETER O.D. / 1.125″ DIAMETER I.D. EDM CORNER NOTCH: .030″ x .030″ +0.00/-0.002 WIDE

FOKKER 50/60 CALIBRATION STANDARD PART 6 53-30-09 PAGE 6 FIGURE 3. MATERIAL: 2024-T3 ALUMINUM. NOTE: ***DOES NOT INCLUDE 3M BELLY PROTECTIVE TAPE 8641

EMBRAER190/195 REFERENCE STANDARD PART 6 57-50-00 PAGE 5 FIGURE 1. Material: 6AL-4v Titanium. Includes Test Report and Certificate of Conformance.

EMBRAER 190/195 REFERENCE STANDARD PT 4 53-10-00 pages 1-12 Embraer 190-NDT 2824, 270-801-B. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175 REFERENCE STANDARD PT 6 53-10-00 pages 4-11. Includes Test Report and Certificate of Conformance.

EMBRAER 170/175/190/195 CALIBRATION STANDARD. PART NUMBER 171T17973-401. Includes Test Report and Certificate of Conformance.

DELRIN HOLDER ASSEMBLY

Honeywell Eddy Current Wheel Surface Standard. Material:2024-T6 Forged Aluminum. Includes Test Report and Certificate of Conformance.

CUSTOM MANUFACTURED BOEING REFERENCE STANDARD FOR ULTRASONIC INSPECTION 101/201

BOEING REFERENCE STANDARD KC10 FUEL COMPENSATOR CUTOUT-INSPECTION.( 301 GUIDE AND 302 GUIDE ARE PART OF INSPECTION AND SOLD SEPARATELY)

MESSIER-DOWTY REFERENCE STANDARD 631-32-181 2024-T3

British Aerospace test block. Material: 2024-T3 Aluminum .128: thick. Includes Test Report and Certificate of Conformance.

BOEING CUSTOM PLATE

CUSTOM REFERENCE STANDARD, H346 SPAR 4 STD-1 HOLE INTERFACE WITH FLAPS HINGE REWORK. MATERIAL: 7050-T7451 ALUMINUM. Includes Test Report and Certificate of Conformance.

ROMPAS BLOCK, 7075-T6 or 7075-T73 ALUMINUM ½” (12.5mm) or 1″ (25.4 mm) thick, 1″ radius opposite 2″ radius, with 5/64″ diameter side drilled hole (3/4″ deep flat bottom hole in 1″ thick version). SPECIFICATION: ASTM E-164. (Includes wooden case). Note: B777-200/300 Part 4 53-40-05 Page 8 Figure 2. Includes Material Certification and Certificate of Conformance.

MD STEP WEDGE, AL, .020, .040, .060 ,.080 ,.100

MD STEP WEDGE, AL, ..05, .100, .150, .200, .250

MD STEP WEDGE, AL, .300, .350, .400, .450, .500

McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K225) FIGURE 1.29, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance.

McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K5225 FIGURE 1.30, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance.

McDONNELL DOUGLAS ULTRASONIC REFERENCE STANDARD (MDC-K225) FIGURE 1.31, PG.1 SECTION 2-1. Includes Test Report and Certificate of Conformance.

MD11 SUBSURFACE ALUMINUM ETLF REFERENCE STANDARD FIG 1.10 (Sheets 1-5) Section 2-1 Pages 1-5. Includes Test Report and Certificate of Conformance.

MD11 SUBSURFACE ALUMINUM ETLF REFERENCE STANDARD FIG 1.11 (Sheets 1-5) Section 2-1 Pages 1-5. Includes Test Report and Certificate of Conformance.