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.