Specification for general requirements for construction and performance of airborne chemical oxygen generators.

NEPLATNÁ vydána dne 31.5.1989

Specification for gaseous breathing oxygen supplied for airborne application.

NEPLATNÁ vydána dne 28.9.1990

Specification for phenolic mouldings for aeronautical purposes.

NEPLATNÁ vydána dne 31.1.1966

Specification for aircraft material. Nickel-chromium-tungsten valve steel.

NEPLATNÁ vydána dne 31.1.1964

Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining (40-50 tonf/sq in: maximum size 1/2 inch diameter or minor sectional dimension) (primarily intended for the manufacture of nuts).

NEPLATNÁ vydána dne 31.1.1964

Specification for aircraft material. ´40´ carbon steel bright bars for machining (45-55 tonf/sq in: limiting ruling section 1 inch) (primarily intended for the manufacture of nuts).

NEPLATNÁ vydána dne 31.1.1964

Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 21/2 inches).

NEPLATNÁ vydána dne 8.6.1964

Specification for aircraft material. ´40´ carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section 3/4 inch) (primarily intended for the manufacture of machined bolts).

NEPLATNÁ vydána dne 31.1.1964

Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 11/8 inch).

NEPLATNÁ vydána dne 31.1.1964

Specification for aircraft material. 11/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 21/2 in).

NEPLATNÁ vydána dne 31.1.1964