Ultrasonic Testing
Ultrasonic Testing
- Boeing Standard, 737/747 PT4 53-00-02 PG22, FIG2, .072" Top Plate .215" Bottom Plate — T
- (5 Step Wedge, .050", .100", .150", .200" .250" X 1" Pads) — T
- Airbus Reference Standard, A320 52-81-06-PB4 Page 6, Figure 52-81-06-991-003-A — T
- (5 Step Wedge, .5, 1, 1.5, 2, 3mm Steps 5" X 1" Pads 2024-T3) — T
- (Airbus Standard A380 54-51-04) — T
- 15 Hole Standard 6al-4v, 1/8, 3/16, 1/4, 5/16, 3/8, 7/16, 1/2, 9/16, 5/8, 11/16, 3/4, 13/16, 7/8, 15/16, 1.0, .030 Corner Topside And .020 Corner Notches Bottom Side, .010, .020, .040 Surface Notches — T
- (Calibration Standard C130J-20-40-00-NEW TO 1C-130J-36 PG 1 FG 23) — T
- (Boeing Standard, 767 PART6 57-04-01:FIG3 PG5) — T
- (Surface Standard, .008"-.020"-.040" Deep Notches, 304L Stainless) — T
- (Boeing Standard 777 PT6 57-20-03 PG 18 FG 4) — T
- (Calibration Standard, ATR72 PT6 53-00-01:PAGE 609 FIG 601) — T
- (Boeing Standard 737 PT6 57-10-60 PG 11 FG 2) — T
- (Boeing Standard, 747 PT6 53-30-16: PG6 FIG1 SHEET1) — T
- Airbus Standard A320 57-29-10-PB4 PG 10 FG 57-29-10-991-004-A SHEET 01 — T
- (Boeing Standard 757 PT4 53-30-03 PG 14 FG 2) — T
- (Boeing Standard 737 PT6 57-10-62 PG 7 FG 2) — T
- (Calibration Standard, ATR42 PT4 53-56-52:PG405-408 FIG402) — T
- (10 Hole Standard, 3/16" To 1.0", .030" Thru Hole Notch, 2024T3 Aluminum) — T
- (Boeing Standard, 767 PT4 57-20-03 PG 7 FG 3) — T
- (Boeing Standard, 737 PT6 53-10-69:PG15 FIG2) — T
- (6 Step Wedge, .015, .030, .050, .070, .090 And .110 Thickness) — T
- (Boeing Standard, 737 PT6 51-00-00 PG 8 FG 4, .030 ± .004 Deep Notch) — T
- (Rolls Royce 40mmx40mmx6mm 4.2mm Hole Standard 6AL-4V) — T
- (Calibration Standard Figure 27 20-40-00 PG1) — T