Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in)
€165.00
TRACTION AND ELONGATION TESTS IN AIRCRAFT FABRICS.
€16.00
COTTON AND LINEN FABRICS USED IN AIRCRAFT.
OBTETION OF TEST SAMPLES IN AIRCRAFT FABRICS.
DETERMINATION OF THE WEIGHT OF FABRICS USED IN AIRCRAFT.
Testing of notched-bar tensile strength of titanium alloys (Pratt and Whitney test)
€60.75
Nickel-copper wrought alloy; NiCu30Ti, creep-resistant, filler metal (Monel 60)
€24.39
Nickel-copper wrought alloy; NiCu30Al, creep-resistant (K-Monel) (for bars and forged pieces)
€34.30
Nickel-copper wrought alloy; NiCu30Al, creep-resistant, filler metal (K-Monel)
CONDITIONING OF FABRICS USED IN AIRCRAFT, TO DETERMINE ITS CHARACTERISTICS.
Flax reinforcement webbing for aeronautical purposes
AIRCRAFT FABRIC. CLASSIFICATION, CHARACTERISTICS, RECEPTION AND MAINTENANCE.
€20.00
DETERMINATION OF THE NATURE OF FIBERS IN FABRICS FOR AIRCRAFT LINING.
DETERMINATION OF FINISH AND WASTE MATERIALS IN FABRICS FOR AIRCRAFT.
DETERMINATION OF PROHIBITED MATTERS IN FABRICS FOR AIRCRAFT.
