AIRBUS REFERENCE STANDARD-99D51107295000 (Inch Version) Airbus Reference Standard A318-A321 51-10-11 Fig 604 Fastener (Ln9199). Includes Test Report And Certificate Of Conformance. SHEET A: THICKNESS: MIN – 0.055" / MAX - 0.12" SHEET B: THICKNESS: MIN – 0.063"/ MAX – 0.16" SHEET C: ANY THICKNESS Block Contains 9 Rivet Shank Hole Diameters (D) 0.16" – 0.22" mm STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 99D51107295000 MATERIAL – SHEET A and SHEET B is ALUMINUM−ALLOY, WITH CONDUCTIVITY RANGE 16−26 MS/m SHEET C is ALUMINUM−ALLOY OR TITANIUM SHEET/STIFFENER. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A51107299001 (Inch Version) Airbus Reference Standard A300-600 51-10-13 Fig 4 Fastener (Nas5410-48). Includes Test Report And Certificate Of Conformance. OVERALL DIMENSION -PLATE (1) – 6.5" (L) X 1.6" (W) X 0.08" (T) PLATE (2) – 6.5" (L) X 4" (W) X 0.071" (T) PLATE (1) & (2) - ASSEMBLED WITH SEALANT PLATE (3) – 6.5" (L) X 1.6" (W) X 0.08" (T) Block Contains (5) BOREHOLE WITH RIVET, DIA 0.19" (2) BOREHOLE WITHOUT RIVET, DIA 0.19" (1) BOREHOLE WITHOUT RIVET, DIA 0.16" (11) ENGRAVED NUMBERS DEPTH 0.006", ENGRAVED RANGE LINES DEPTH 0.002" ENGRAVE WIDTH – 0.04" (3) CORNER NOTCH – 0.2" (1) BORE NOTCH – 0.12" (1) CORNER NOTCH – 0.12" (2) SCREW, WASHER, NUT STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 99A51107299001 MATERIAL: 2024 ALUMINUM ALLOY. RIVET MATERIAL - CSK 100 - NSA 5410−48 SEALENT MATERIAL - PR 1422B NO. 09−002 NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A51107300000 (Inch Version) ALUMINUM ALLOY Airbus A330 Reference Standard For Subsurface Cracks In Al-Alloy 51-10-16-991-011-A. Part 6, Page 615 Figure 610procedure B. Includes Test Report And Certificate Of Conformance. OVERALL DIMENSION - 4" (L) X 2.5" (W) X 0.07" (T) 1. NOTCH - RADIUS 1" X DEPTH 0.04". 2. NOTCH – 2.5" (L) X 0.006" (W) X 0.05" (Deep) (2) ACRYL 5.1411 - Sq.0.4" X 0.4", 4" (L) (8) SCREW - DIN84 M4 or LOCAL PROCUREMENT STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 99A51107300000 MATERIAL: ALUMINUM ALLOY. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A53307274000 (Inch Version) 2024-T351 ALUMINUM AIRBUS A318/A319/A320/A321 REFERENCE STANDARD 51-10-16-991-005A, PAGE 10. MATERIAL: 2024-T351 ALUMINUM. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.5" (W) X 0.07" (T) 1. NOTCH - RADIUS 1" X DEPTH 0.04". 2. NOTCH – 2.5" (L) X 0.006" (W) X 0.05" (Deep) (2) ACRYL 5.1411 - Sq.0.4" X 0.4", 4" (L) (8) SCREW - DIN84 M4 or LOCAL PROCUREMENT STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 99A53307274000 MATERIAL: 2024-T351 ALUMINUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A55407291000 (Inch Version) ALUMINUM ALLOY AIRBUS REFERENCE STANDARD A318-A321 PT 5 51-10-19 PAGE 16 FIGURE 51-10-16-991-005-A. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.5" (W) X 0.07" (T) 1. NOTCH - RADIUS 1" X DEPTH 0.04". 2. NOTCH – 2.5" (L) X 0.006" (W) X 0.05" (Deep) (2) ACRYL 5.1411 - Sq.0.4" X 0.4", 4" (L) (8) SCREW - DIN84 M4 or LOCAL PROCUREMENT STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 99A55407291000 MATERIAL: ALUMINUM ALLOY. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-98A54003072000 (Inch Version) ALUMINUM AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 FIG 403 OVERALL DIMENSION - 10" (L) X 6" (W) X 0.25" (T) DEPTH - 0.013", 0.025", 0.04", 0.05" SPOT FACE – 0.8" X 0.8" STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 98A54003072000 MATERIAL: ALUMINUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-98A54003073000 (Inch Version) TITANIUM AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 FIG 404 OVERALL DIMENSION - 10" (L) X 6" (W) X 0.25" (T) DEPTH - 0.013", 0.025", 0.04", 0.05" SPOT FACE – 0.8" X 0.8" STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 98A54003073000 MATERIAL: TITANIUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-98A54403026000 (Inch Version) STEEL AIRBUS REFERENCE STANDARD A300-600 PT 4 54-50-23 OVERALL DIMENSION - 10" (L) X 6" (W) X 0.25" (T) DEPTH - 0.013", 0.025", 0.04", 0.05" SPOT FACE – 0.8" X 0.8" STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 98A54403026000 MATERIAL: STEEL. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99D57004001001 (Inch Version) ALUMINUM AIRBUS A318/319/320/321 REFERENCE STANDARD 51-63-03-PB1 PAGE 4 BLOCK CONTAINS 3 PLATES OVERALL DIMENSION – 7.5" (L) X 6" (W) TOP PLATE THICK – 0.08" MIDDLE PLATE THICK – 0.5" BOTTOM PLATE THICK – 0.08" CONTAIN (20) HOLES – Ø0.25", 0.27", 0.28", 0.29", 0.31", 0.33", 0.34", 0.36", 0.38", 0.39", 0.41", 0.42", 0.44", 0.45", 0.47", 0.48", 0.5", 0.52", 0.53" and 0.55". MIDDLE PLATE CONTAIN 2 CORNER NOTCH FOR EACH HOLE (20) TOP NOTCH – 0.02" (D) X 0.006" (W) (20) BOTTOM NOTCH – 0.006" (D)X 0.006" (W) (6) BOLT & NUT DIA -0.26". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99D57004001001 MATERIAL: ALUMINUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99D57004001002 (Inch Version) AIRBUS A318/319/320/321 REFERENCE STANDARD 51-63-03-PB1 PAGE 4 BLOCK CONTAINS 3 PLATES OVERALL DIMENSION – 7.5" (L) X 6" (W) TOP PLATE THICK – 0.08" MIDDLE PLATE THICK – 0.5" BOTTOM PLATE THICK – 0.08" CONTAIN (20) HOLES – Ø0.25", 0.27", 0.28", 0.29", 0.31", 0.33", 0.34", 0.36", 0.38", 0.39", 0.41", 0.42", 0.44", 0.45", 0.47", 0.48", 0.5", 0.52", 0.53" and 0.55". MIDDLE PLATE CONTAIN 2 CORNER NOTCH FOR EACH HOLE (20) TOP NOTCH – 0.02" (D) X 0.006" (W) (20) BOTTOM NOTCH – 0.006" (D)X 0.006" (W) (6) BOLT & NUT DIA -0.26". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99D57004001002 MATERIAL: ASME SA516 Gr 70, SA517, SA36 / A36. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99D57004000000 (Inch Version) Airbus Calibration Standard Block Set. A340-200/-300 51-63-03 Pg. 2-3, A300, A300-600, A310, A318/A319/A320/A321, A330, A340, A380 51-34-03, Figure 1 Sheett 1 Pg.1-2. BLOCK CONTAINS 3 PLATES OVERALL DIMENSION – 7.5" (L) X 6" (W) TOP PLATE THICK – 0.08" MIDDLE PLATE THICK – 0.5" BOTTOM PLATE THICK – 0.08" CONTAIN (20) HOLES – Ø0.25", 0.27", 0.28", 0.29", 0.31", 0.33", 0.34", 0.36", 0.38", 0.39", 0.41", 0.42", 0.44", 0.45", 0.47", 0.48", 0.5", 0.52", 0.53" and 0.55". MIDDLE PLATE CONTAIN 2 CORNER NOTCH FOR EACH HOLE (20) TOP NOTCH – 0.02" (D) X 0.006" (W) (20) BOTTOM NOTCH – 0.006" (D)X 0.006" (W) (6) BOLT & NUT DIA -0.26". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99D57004000000 MATERIAL: 2024-T351 ALUMINUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A53003001103 (Inch Version) AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION – 9.5" (L) X 5.5" (W) X 0.4" (T) CONTAINS (18) RIVET HOLES, (18) BORE HOLES (18) RIVET HOLE DIA – Ø0.37", 0.39", 0.41", 0.44", 0.45", 0.47", 0.5", 0.53", 0.55" (18) BORE HOLE DIA – Ø0.37", 0.39", 0.41", 0.44", 0.45", 0.47", 0.5", 0.53", 0.55" (9) CORNER NOTCHS – 0.04" (L) X 0.04" (D) (9) BORE NOTCHS - 0.02" L) X 0.4" (D) (9) RIVET NOTCHS DEPTH – 0.11", 0.12", 0.13", 0.13", 0.13", 0.14", 0.14", 0.16", and 0.16". (9) RIVET NOTCHS SIZE – 0.02" (L) X 0.006" (W) ALL NOTCHS WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99A53003001103 MATERIAL: 2024-T3 ALUMINUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A53003001104 (Inch Version) AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION – 9.5" (L) X 5.5" (W) X 0.4" (T) CONTAINS (18) RIVET HOLES, (18) BORE HOLES (18) RIVET HOLE DIA – Ø0.37", 0.39", 0.41", 0.44", 0.45", 0.47", 0.5", 0.53", 0.55" (18) BORE HOLE DIA – Ø0.37", 0.39", 0.41", 0.44", 0.45", 0.47", 0.5", 0.53", 0.55" (9) CORNER NOTCHS – 0.04" (L) X 0.04" (D) (9) BORE NOTCHS - 0.02" L) X 0.4" (D) (9) RIVET NOTCHS DEPTH – 0.11", 0.12", 0.13", 0.13", 0.13", 0.14", 0.14", 0.16", and 0.16". (9) RIVET NOTCHS SIZE – 0.02" (L) X 0.006" (W) ALL NOTCHS WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99A53003001104 MATERIAL: 6AL-4V TITANIUM. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99A53003001108 (Inch Version) AIRBUS REFERENCE STANDARD NTM A318/A319/A320/A321, A340_500_600 51-63-05-991-001-A. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION – 9.5" (L) X 5.5" (W) X 0.4" (T) CONTAINS (18) RIVET HOLES, (18) BORE HOLES (18) RIVET HOLE DIA – Ø 0.37", 0.39", 0.41", 0.44", 0.45", 0.47", 0.5", 0.53", 0.55" (18) BORE HOLE DIA – Ø 0.37", 0.39", 0.41", 0.44", 0.45", 0.47", 0.5", 0.53", 0.55" (9) CORNER NOTCHS – 0.04" (L) X 0.04" (D) (9) BORE NOTCHS - 0.02"(L) X 0.4" (D) (9) RIVET NOTCHS DEPTH – 0.11", 0.12", 0.13", 0.13", 0.13", 0.14", 0.14", 0.16", and 0.16". (9) RIVET NOTCHS SIZE – 0.02" (L) X 0.006" (W) ALL NOTCHS WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99A53003001108 MATERIAL: ASME SA516 Gr 70, SA517, SA36 / A36. NOTE: For special alloy request by mail.

AIRBUS REFERENCE STANDARD-99D57204125000 (Inch Version) AIRBUS REFERENCE STANDARD A318/319/320/321 NTM 57-29-04-PB4 PAGE 405 FIGURE 403. Includes Test Report and Certificate of Conformance. DIMENSION - 8" (L) X 1" (W) EDM SLOT AT 5 LOCATION (1 TO 5) EDM SLOT 1 AND 3, 55° AT FWD EDGE OF BORE EDM SLOT 4 AND 5, 45° AT AFT EDGE OF BORE EDM SLOT 2, 90° AT FWD EDGE OF BORE EDM SLOT DIMENSION – 0.16" (L) X 0.16" (D) X 0.006" (W) BORE DIA – 3.8". MACHINE 45°, 0.04" CHAMFER AT EDGE OF BORE DIA 5.1". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 99D57204125000 MATERIAL: ALUMINUM 2014-T652. NOTE: For special alloy request by mail.