Ultrasonic Testing
Ultrasonic Testing
- (12 Hole Reference Standard, 1/8" Thru 3/4", W/.030" Corner Notc... — T
- (Calibration Standard, BAe 3100 PT6 53-10-15:PG408 FIG2) — T
- (Boeing Standard, 737 PT6 51-00-00 PG 8 FIG 3 Procedure 16, .188" Hole Di... — T
- (Surface Standard, .008"-.020"-.040" Deep Notches, 17-7 TH1050) — T
- (Calibration Standard, ATR72 51-60-00 PT6:PG628 FIG615 15-5PH) — T
- (Airbus Standard, A330 PT4 53-11-30:PG404 FIG403 - CAA+PRIMER+TOPC... — T
- (Boeing Standard, 737 PT6 51-00-00 PG 8 FIG 3 Procedure 16, .375" Hole Di... — T
- (5 Step Wedge, .100", .125", .150", .175" .200" X 1" Pads) — T
- (Cessna Standard, 525 Series Crew Side Window Frame) — T
- (Boeing Standard, 737 PT4 57-50-03:PG14 FIG 3) — T
- 6 Hole Standard, 3/4", 13/16", 7/8", 15/16", 1.0", 1 1/8" .030 Corner, 4340 Steel — T
- (Boeing Standard, 747 PT4 53-40-05:PG 4 FIG 2) — T
- (Boeing Standard 767 PT4 53-00-03 PG 25-26 FG 2) — T
- (Rolls Royce 40mmx40mmx6mm 5.95mm Hole Standard 4130 STEEL) — T
- (POSITIONING PLATES/SPACERS For CMM 32-49-01, B777 2612185 *Included With Holding Blocks*) — T
- (3 Hole Countersink Standard 7/32, 1/4, 9/32, .500 Thick Plate .020 Deep Notches On The CS And Inside The Hole, 6AL4V) — T
- (Boeing Standard 747 PT6 51-00-00 Procedure 1 PG5 FIG2, .4375 Diameter Hole) — T
- (Boeing Standard, 767 PT4 53-50-05: PG7 FIG3) — T
- (5 Step Wedge, .020" To .100" X .020", 5" X 1" Pads 606... — T
- (Airbus Standard, A310 PT4 57-10-26:FIG403 PG 405 - CAA + PRIMER) — T
- (Airbus Standard 53-31-22) — T
- (Boeing Standard 737 PT6 55-10-45 PG 6 FG 2) — T
- (A340 57-18-15) — T
- (Airbus Standard, A320 PT4 57-51-01:PG405 FIG403) — T