Tool Description: PROCEDURE

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DZZ7501

Description: PROCEDURE

In stock: 0

Sources: 1

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Partial Match

004-50337-05XX

Description: ACCEPTANCE TEST PROCEDURE SETUP DISK

In stock: 0

Sources: 1

For Aircraft*: N/A

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076-0237-701

Description: PROCEDURE REV.G

In stock: 0

Sources: 1

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127-.100

Description: BOEING STANDARD, 737 PT6 51-00-00 FIG4:PG1 PROCEDURE 12

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Sources: 1

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140158

Description: 140158;Procedure;Verification;CD;RGS-2000NG

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Sources: 1

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140159

Description: 140159;Procedure;Verification;CD;ATC-5000NG

In stock: 0

Sources: 1

For Aircraft*: N/A

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185

Description: BOEING REFERENCE STANDARD PT 6 51-00-00 FIG 13 & 777-200/300 51-00-04 PROCEDURE 1 PAGE 8. Includes Test Report and Certificate of Conformance.

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Sources: 2

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186G

Description: BOEING STANDARD 737/747 PT6 51-00-00 PROCEDURE 1 PG5 FIG2, .563 DIAMETER HOLE

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186H

Description: BOEING STANDARD 737/747 PT6 51-00-00 PROCEDURE 1 PG5 FIG2, .625 DIAMETER HOLE

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186J

Description: BOEING STANDARD 737/747 PT6 51-00-00 PROCEDURE 1 PG5 FIG2, .750 DIAMETER HOLE

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189

Description: BOEING REFERENCE STANDARD PT 6 51-00-01 FIG 4 PG.13 & 737 PT 6 51-00-00 PROCEDURE 23 PG.11 FIG.7. Includes Test Report and Certificate of Conformance.

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Sources: 7

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21-8588

Description: EDDY CURRENT PROCEDURE

In stock: 0

Sources: 1

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272

Description: Boeing Reference Standard, 727 PT 6 55-10-27 PROCEDURE 2 Figure 1 (Sheets 1- 2) Pages 4- 5. Material: 7075-T6 Aluminum and AL-NI Bronze Bushing Per AMS 4640. Includes Test Report and Certificate of Conformance.

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Sources: 1

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29491220711

Description: TOOL - CALIBRATION PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: A330
A330-200
A330-300
A330 Freighter
A330-200 Freighter
A340
A340-200
A340-300
A340-500
A340-600

Photos:

36-3131-01

Description: AUTOMATIC TEST TAPE AND TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: A310
A310-200
A310-300
A310F
A310-200F
A310-300F
A300B2
A300
A300B4/C4
A300-600/600C/601
A300-600ST Beluga
A300F
A300-600 Combi
A300C4/F4 Freighter
A300-600F Freighter

Photos:

36-3131-03

Description: AUTOMATIC TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: A310
A310-200
A310-300
A310F
A310-200F
A310-300F
A300B2
A300
A300B4/C4
A300-600/600C/601
A300-600ST Beluga
A300F
A300-600 Combi
A300C4/F4 Freighter
A300-600F Freighter

Photos:

36-3131-04

Description: TEST PROCEDURES

In stock: 0

Sources: 1

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36-3131-11

Description: AUTOMATIC TEST PROCEDURES

In stock: 0

Sources: 1

For Aircraft*: A310
A310-200
A310-300
A310F
A310-200F
A310-300F
A300B2
A300
A300B4/C4
A300-600/600C/601
A300-600ST Beluga
A300F
A300-600 Combi
A300C4/F4 Freighter
A300-600F Freighter

Photos:

36-3214-02

Description: AUTOMATIC TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: A310
A310-200
A310-300
A310F
A310-200F
A310-300F
A300B2
A300
A300B4/C4
A300-600/600C/601
A300-600ST Beluga
A300F
A300-600 Combi
A300C4/F4 Freighter
A300-600F Freighter

Photos:

38-3131-02

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: A310
A310-200
A310-300
A310F
A310-200F
A310-300F
A300B2
A300
A300B4/C4
A300-600/600C/601
A300-600ST Beluga
A300F
A300-600 Combi
A300C4/F4 Freighter
A300-600F Freighter

Photos:

7919970

Description: TEST PROCEDURE

In stock: 0

Sources: 1

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7923395

Description: TEST PROCEDURE

In stock: 0

Sources: 1

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Photos:

7925143

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

7953927

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

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7962515

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

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8011486-508

Description: SUPPORT FOR DISASEMBLY AND ASSEMBLY (TEST PROCEDURES)

In stock: 0

Sources: 1

For Aircraft*: A319
A318
A319 (Sharklets)
A320-100/200
A321-100/200
A320-200 (Sharklets)
A321-200 (Sharklets)
A330
A330-200
A330-300
A330 Freighter
A330-200 Freighter
A340
A340-200
A340-300
A340-500
A340-600
A380
A380-800F Freighter

Photos:

856A1520

Description: CHILLING, KIT HPTR & HPCR ASSEMBLY PROCEDURE

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Sources: 1

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856A1520G01

Description: CHILLING, KIT HPTR & HPCR ASSEMBLY PROCEDURE

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Sources: 1

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856A1520G02

Description: CHILLING, KIT HPTR & HPCR ASSEMBLY PROCEDURE

In stock: 0

Sources: 5

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856A2678

Description: SOFTWARE-FAN TRIM BALANCE PROCEDURE, CFM56

In stock: 0

Sources: 1

Photos:

980-4750-702

Description: PROCEDURE REV.C

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Sources: 1

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98D07203005222

Description: LABEL INSTALLATION PROCEDURE

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Sources: 1

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998-2232-506

Description: ACCEPTANCE TEST PROCEDURE

In stock: 0

Sources: 1

Photos:

998-2551-508

Description: ACCEPTANCE TEST PROCEDURE SETUP DISK

In stock: 0

Sources: 1

Photos:

998-2687-504

Description: ACCEPTANCE TEST PROCEDURE SETUP DISK

In stock: 0

Sources: 1

Photos:

99A53803004001

Description: AIRBUS REFERENCE STANDARD A300-600 53-15-23 FIGURE 603 PROCEDURE A PG. 605-606 . Includes Test Report and Certificate of Conformance.

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99D57204188000

Description: AIRBUS A320 CALIBRATION STANDARD FIGURE 2 PROCEDURE D. A320 FWD SPAR LOWER FLANGE RIB 22-27. Includes Test Report and Certificate of Conformance.

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A320 51-10-04

Description: Airbus A318/A319/A320/A321 51-10-04 Page 402 Figure 401, Measurement of Remaining Thickness in Large Blended Out Areas-Procedure A. Material: 6Al-4v Titanium. Steps: 0.5mm, 1mm, 2mm, 3mm, 4mm, 5mm +/-.05mm(.002"). Step Pad Size: 20mm(.787") x 20mm(.7...

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Sources: 1

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AF-5036G1

Description: PROBE GUIDE Material: Delrin. Diameter 0.430 ±0.025 (10.92mm ±0.064). Used in Boeing procedure 57-53-03 Part 6. Includes Certificate of Conformance.

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AF-5036G2

Description: PROBE GUIDE Material: Delrin. Diameter 0.515 ±0.025 (13.08mm ±0.064). Used in Boeing procedure 57-53-03 Part 6. Includes Certificate of Conformance.

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Sources: 1

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AF-5257G

Description: PROBE GUIDE Material: Lucite. Diameter 1.50" ±0.02 . Used in Boeing procedure 55-10-27 Part 6. Includes Test Report and Certificate of Conformance

In stock: 0

Sources: 1

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AF-MBB403-7-1

Description: CUSTOM STAINLESS STEEL EDDY CURRENT ROTARY PROBE INCLUDING COLLAR, FREQUENCY 100KHz-2MHz WITH 4 PIN FISCHER CONNECTOR. REFERENCE: AIRBUS A300-600 FIGURE 603 PART 6 53-19-27 PAGE 604 PROCEDURE A. Includes Test Report and Certificate of Conformance.

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Sources: 1

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AFNDT-1016-6S-TI

Description: CUSTOM 6 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6, 51-00-02 PROCEDURE 1..... Hole Sizes: .188", .250", .313", .375" .438" .500". MATERIAL: 6AL-4V Titanium. Inc...

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Sources: 1

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AFNDT-2008/SS

Description: AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PAGES 1-7 FIGURE 2 and 3 & 32-42-05 FIGURE 11 PROCEDURE 1 PAGE 15. MATERIAL: 304 STAINLESS STEEL. Includes Test Report and Certificate of Conformance.

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Sources: 1

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AFNDT-2054AL

Description: CUSTOM ALUMINUM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1016-NDT1021, 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. WITH HOLE DIAMETERS: .156",.250",.312",.375",.437",.500". CORNER E...

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AFNDT-2054AL-1

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Sources: 1

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AFNDT-2054AL-2

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Sources: 1

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AFNDT-2054CS-1

Description: CUSTOM REFERENCE STANDARD PER BOEING SPECIFICATION NDT1040-NDT1045, 707, 727, 737, 747 PT 6 51-00-00 FIG 19, 757, 767 PT 6 51-00-17, 777 PT 6 51-00-05 PROCEDURE 2, 787 PT 6 51-00-04 PROCEDURE 1. DIAMETERS: .156",.250",.312",.375",.437",.500". CORN...

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AFNDT-2054CS-2

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Sources: 1

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AFNDT-2227Ti-1

Description: 8 Hole Calibration Standard, Hole Sizes; 1/8" 5/32", 3/16", 1/4", 5/16", 3/8", 7/16", 1/2", EDM NOTCH: .050" x .050" x .005" +0.000/-.002" BOEING REFERENCE STANDARD PT. 6 757 51-00-14 FIG.3, 737 PT 6 51-00-00 FIG 3 PROCEDURE 17, PG.8 MATERIAL(6AL-4V) TIT

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AFNDT-3187AL

Description: METRIC 10 STEP CALIBRATION BLOCK, 0.6mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm ± .05mm. Pad Size: 20mm X 20mm. Per Airbus Procedure A 51-10-04. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance.

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Sources: 1

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AFNDT-3187TI

Description: METRIC 10 STEP CALIBRATION BLOCK, 0.6mm, 1.0mm, 1.5mm, 2.0mm, 2.5mm, 3.0mm, 3.5mm, 4.0mm, 4.5mm, 5.0mm ± .05mm. Pad Size: 20mm X 20mm. Material: 6AL-4V Titanium. Per Airbus Procedure A 51-10-04. Includes Test Report and Certificate of Conformance.

In stock: 0

Sources: 1

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AFNDT-3292AL

Description: CUSTOM 20 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .(1/8", 5/32",3/16", 7/32", 1/4", 9/32", 5/16", 11/32", 3/8",13/32"

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Sources: 1

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AFNDT-3295

Description: CUSTOM HOLE STANDARD IN 4340 OR 4340M STEEL PER BOEING PART NUMBER NDT1083 PART 6 51-00-00 PROCEDURE 19. EDM CORNER NOTCH SIZES: .030" x .030" x .005" +/- .002". 13 HOLE SIZES: 3/16, 7/32, 1/4, 9/32, 5/16, 11/32, 3/8, 13/32, 7/16, 15/32, 1/2, 17/32, 9/

In stock: 0

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AFNDT-3320AL

Description: 6 Hole reference standard (Aluminum 7075-T6 manufactured in accordance with Boeing Specification 51-00-02 Part 6 Procedure 1 or 2. Hole Sizes: 15/32", 17/32", 9/16", 11/16", 5/8", 3/4" ( .020" x .020" x .005" +/- .002), ( .030" x .030" x .005" +/- .002

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Sources: 1

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Photos:

AFNDT-3329AL

Description: 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(.313), 11/32”(.343), 3/8”(.375), 7/16”(.437), 1/2”(.500), 9/16”(.562), 5/8”(.625), 3/4”(.750 Ø, 3 S

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AFNDT-3329ST

Description: CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(.

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AFNDT-3329TI

In stock: 0

Sources: 1

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AFNDT-3390AL

Description: CUSTOM 10 HOLE FLAT BOTTOM REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .218", .250", 312", .375" .437" .500",.562", .625",

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Sources: 1

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Photos:

AFNDT-3391AL

Description: CUSTOM 10 HOLE FLAT BOTTOM HOLE REFERENCE STANDARD ASSEMBLY PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .875", 1.00", 1.125", 1.250" 1.375", 1.500",

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Sources: 1

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Photos:

AFNDT-3405AL

Description: CUSTOM 15 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: 3/16”(.188), 7/32”(.218),1/4”(.250), 9/32”(.281), 5/16”(.

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Sources: 1

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Photos:

AFNDT-3456AL

Description: CUSTOM 19 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737 PT 6 51-00-00 Procedure16 Figure 3 , 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Total of 19 Hole Sizes: .128", .159", .189", .2

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AFNDT-3507

Description: Custom 2 hole BOEING REFERENCE STANDARD MANUFACTURED PER 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance. ....HOLE SIZES: 0.344" (11/32''),0.562"...

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Sources: 1

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Photos:

AFNDT-3669-1043

Description: BOEING COUNTERSINK REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER 100° COUNTERSINK HOLE. MATERIAL: 43404340M STEEL. SIZE: 2.0" X .375" THICK( ROUNDSQUARE. INCLUDES TEST REPORT AND CERTIFICATE OF CONFORMANCE.

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Sources: 1

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Photos:

AFNDT1016-12S-2024

Description: CUSTOM 12 HOLE REFERENCE STANDARD PER BOEING SPECIFICATION STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Hole Sizes: .188", .219", .250",.282", 313", .344", .375" .438" .500",.563", .

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Sources: 1

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Photos:

AFNDT1016-12S-7075

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Sources: 1

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AL-BOEING REF STD PART6 51-00-0

Description: AL REF STANDARD FOR BOEING NDT PART 6 51-00-00 PROCEDURE 16

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ANDT1079

Description: BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. Includes Test Report and Certificate of Conformance. FASTENER (BACR15BB5AD-4, BACR15BB6AD-4, BACR15BB7AD-4, BACR15BB8AD-4, ALL ALODINE)

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Sources: 4

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Photos:

ANDT1080

In stock: 0

Sources: 2

For Aircraft*: N/A

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ANDT1081

Description: BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENER (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance.

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Sources: 2

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Photos:

ANDT1082

Description: BOEING REFERENCE STANDARD 737 PT6 53-30-00: PG 7-8 FIG 2 Procedure 7/ 767 PT6 53-00-07: PG 6-7 FIG 2. FASTENERS: (BACR15BB5AD-5, BACR15BB6AD-5, BACR15BB7AD-5, BACR15BB8AD-5, ALL ALODINE). Includes Test Report and Certificate of Conformance.

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Sources: 3

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Photos:

DAC ETBS AL-1T 2024-T3 0.063

Description: MD-80 REFERENCE STANDARD ETFL PROCEDURE 5, 06-10-02.005. MATERIAL: 2024-T3 ALUMINUM 0.063". Includes Test Report and Certificate of Conformance.

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Sources: 1

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DAC ETBS AL-1T/ 0.032

Description: MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 7075-T7 ALUMINUM .032". Includes Test Report and Certificate of Conformance.

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Photos:

DAC ETBS AL-1T/ 0.071

Description: MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 2024-T3 ALUMINUM .071". Includes Test Report and Certificate of Conformance.

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Sources: 1

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Photos:

DAC ETBS AL-1T/ 0.090

Description: MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 7075-T6 ALUMINUM .090". Includes Test Report and Certificate of Conformance.

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Sources: 1

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Photos:

DAC ETBS AL-1T/0.080

Description: MD-80 REFERENCE STANDARD ETFL PROCEDURE 5 Part 6 06-10-02 Page F1 Figure 1. Material: 2024-T3 ALUMINUM .080". Includes Test Report and Certificate of Conformance.

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

DZZ7411

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

DZZ7540

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

DZZ7553

Description: INSP TEST PROCEDURE

In stock: 0

Sources: 1

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Photos:

DZZ7601

Description: TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

ETBS AL-1T/2024-T3 0.032

Description: MD REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

F27404000

Description: SUPPORT-ASSY DISASSY AND TEST PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: A380
A380-800F Freighter

Photos:

FA02242TL1

Description: SUPPORT FOR ASSEMBLY AND DISASSEMBLY PROCEDURES

In stock: 0

Sources: 1

For Aircraft*: A380
A380-800F Freighter

Photos:

FA02242TL5

Description: SUPPORT FOR TEST PROCEDURES

In stock: 0

Sources: 1

For Aircraft*: A380
A380-800F Freighter

Photos:

FTI-190-57-0056

Description: COLD EXPANSION PROCEDURE

In stock: 0

Sources: 1

For Aircraft*: N/A

Photos:

LMT-76036

Description: WATER WASH NOZZLE (PROCEDURE II)

In stock: 0

Sources: 1

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Photos:

LMT-777

Description: SPRAYER (PROCEDURE I)

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Sources: 1

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Photos:

Model #2019

Description: Hydraulic Test Stand (Hydraulic and leak testing procedures 10 GPM minimum)

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Sources: 1

For Aircraft*: N/A

Photos:

NDT1016

Description: BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance.

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Sources: 3

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Photos:

NDT1017

Description: BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance.

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Sources: 2

For Aircraft*: N/A

Photos:

NDT1018

Description: BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance.

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Sources: 3

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Photos:

NDT1019

Description: BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance.

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Sources: 3

For Aircraft*: N/A

Photos:

NDT1020

Description: BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance.

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Sources: 2

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Photos:

NDT1021

Description: BOEING REFERENCE STANDARD 737, 747, 757, 767 PT 6 51-00-16 FIG 16, 777 PT 6 51-00-02 PROCEDURE 3, 787 PT 6 51-00-02 PROCEDURE 1. Includes Test Report and Certificate of Conformance.

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Sources: 2

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Photos:

NDT1041

Description: BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.250” DIAMETER. Includes Test Report and Certificate of Conformance.

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Sources: 2

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Photos:

NDT1042

Description: BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.313” DIAMETER. Includes Test Report and Certificate of Conformance.

In stock: 0

Sources: 2

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NDT1043

Description: BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.375” DIAMETER. Includes Test Report and Certificate of Conformance.

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NDT1043CS

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Sources: 1

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NDT1044

Description: BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.438” DIAMETER. Includes Test Report and Certificate of Conformance.

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NDT1045

Description: BOEING REFERENCE STANDARD 737 PT6 51-00-00 PROCEDURE 19, 0.500” DIAMETER. Includes Test Report and Certificate of Conformance.

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NDT1083-.157

Description: BOEING REFERENCE STANDARD 757 Part 6 51-00-17 Page 7 Figure 3. Material: Low Alloy Steel, Such as,4330 or 4340. Procudures vary with Plane Model. All Models for this Reference Standard. Provide Custom Hole Size and Procedure. Includes Test Report and Cert

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NDT1083-.5625

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NDT1083-.630

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NDT1083-0.5620

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NDT1083-0.563

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NDT1083-0.625

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NDT1083-0.630

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NDT1083-0.688

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NDT1083-0.695

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NDT1083-0.750

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NDT1083-0.787

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NDT1083-0.812

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NDT1083-0.813

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NDT1083-0.875

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NDT1083-0.938

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NDT1083-1.000

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NDT1083-1.286

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Sources: 1

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NDT1083-1.347

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NDT1084-.156/.5

Description: Boeing Standard, 18 holes, 2 columns, 1 with notches and 1 without, 2024-T3, 737/747 PT6 51-00-00: PG8 FIG3 Procedure 16, .156, .171, .1875, .203, .218, .25, .265, .281, .312, .328, .343, .375, .39, .406, .437, .453, .468, .5

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NDT1084-.156/.5-1

Description: BOEING STANDARD, 18 HOLES, 4 COLUMNS, 3 WITH NOTCHES AND 1 WITHOUT, 2024-T3, 737/747 PT6 51-00-00: PG8 FIG3 PROCEDURE 16, .156, .171, .1875, .203, .218, .25, .265, .281, .312, .328, .343, .375, .39, .406, .437, .453, .468, .5

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NDT1084-.218

Description: BOEING STANDARD, 737/757 PT6 51-00-00 PG 8 FIG 3 PROCEDURE 16, .218" HOLE DIAMETER

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NDT1084-.546/.937-1

Description: Boeing Standard, 8 holes, 4 columns, 3 with notches and 1 without, 2024-T3, 737/747 PT6 51-00-00: PG8 FIG3 Procedure 16, 35/64, 37/64, 41/64, 11/16, 49/64, 13/16, 7/8, 15/16

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NDT1084-.750