Specification for general design requirements for aircraft oxygen systems and equipment.

NEPLATNÁ vydaná dňa 31.10.1985

3 per cent nickel-chromium-molybdenum case-hardening steel.

NEPLATNÁ vydaná dňa 28.2.1969

Procedure for inspection, testing and acceptance of steel sheet and strip.

NEPLATNÁ vydaná dňa 15.6.1996

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in).

NEPLATNÁ vydaná dňa 31.1.1964

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (45/55 tonf/sq in: limiting ruling section 6 in).

NEPLATNÁ vydaná dňa 31.1.1964

Specification for aircraft material. ´55´ carbon steel (normalized) (45/55 tonf/sq in: limiting ruling section 4 in).

NEPLATNÁ vydaná dňa 31.1.1964

Specification for aircraft material. ´55´ carbon steel (hardened and tempered) (55/65 tonf/sq in: limiting ruling section 11/8 in).

NEPLATNÁ vydaná dňa 31.1.1964

Procedure for inspection and testing of steel tubes.

NEPLATNÁ vydaná dňa 28.2.1978

Specification for aircraft material. High pressure seamless copper tubes.

NEPLATNÁ vydaná dňa 4.5.1945

Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm).

NEPLATNÁ vydaná dňa 30.11.2009