AIRBUS REFERENCE STANDARD-99A53307292001 (Metric Version) 2024 ALUMINUM ALLOY

Airbus Reference Standard A318-A321 51-10-15-991-004-A Fasteners: (Nas5410-48). Includes Test Report And Certificate Of Conformance.

OVERALL DIMENSION - TOP SKIN - 230mm (L) X 100mm (W) X 1.6mm (T)

TOP SKIN DOUBLER -230mm (L) X 64mm (W) X 0.6mm (T)

BOTTOM SKIN - 230mm (L) X 125mm (W) X 1.6mm (T)

BOTTOM SKIN DOUBLER - 230mm (L) X 50mm (W) X 0.6mm (T)

Block Contains:

(28) RIVET HOLE DIA - 4.8mm, Note - NSA5410−48 (8 Rivet as modified length).

(4) PILOT HOLE DIA - 1.5mm.

(10) A CORNER NOTCH - 3mm (L) X  0.15mm (W) X 1.6mm (D)

(2) B CORNER NOTCH - 5mm (L) X 0.15mm (W) X 1.6mm (T)

(4) C CORNER NOTCH - 7mm (L) X 0.15mm (W) X 1.6mm (T)

(4) THRU NOTCH - 9.5mm (L) X 0.5mm (W) X 1.6mm (D)

STANDARD/MANUFACTURE REFERENCE/PART NUMBER - 99A53307292001

MATERIAL: 2024 ALUMINUM ALLOY. 

STRINGER - DAN21 AK 28 x22 x 1.6

SEALENT MATERIAL - PR 1422B, NO. 09−002

NOTE: For special alloy request by mail.