Skip to content

A gradual release of Avioverse begins in October 2026. Request early access →

CS 25.1443 Minimum mass flow of supplemental oxygen

Large Aeroplanes (CS-25) · CS-25 · EAR revision 26 Jan 2023

IRImplementing rule

CS 25.1443Minimum mass flow of supplemental oxygen

(a)If continuous flow equipment is installed for use by flight-crew members, the minimum mass flow of supplemental oxygen required for each crew member may not be less than the flow required to maintain, during inspiration, a mean tracheal oxygen partial pressure of 149 mmHg when breathing 15 litres per minute, BTPS, and with a maximum tidal volume of 700 cm3 with a constant time interval between respirations.

(b)If demand equipment is installed for use by flight-crew members, the minimum mass flow of supplemental oxygen required for each crew member may not be less than the flow required to maintain, during inspiration, a mean tracheal oxygen partial pressure of 122 mmHg, up to and including a cabin pressure altitude of 10668 m (35 000 ft), and 95% oxygen between cabin pressure altitudes of 10668 m (35 000) and 12192 m (40 000 ft), when breathing 20 litres per minute BTPS. In addition, there must be means to allow the crew to use undiluted oxygen at their discretion.

(c)For passengers and cabin crew members, the minimum mass flow of supplemental oxygen required for each person at various cabin pressure altitudes may not be less than the flow required to maintain, during inspiration and while using the oxygen equipment (including masks) provided, the following mean tracheal oxygen partial pressures:

(1)At cabin pressure altitudes above 3048 m (10 000 ft) up to and including 5639 m (18,500 ft), a mean tracheal oxygen partial pressure of 100 mmHg when breathing 15 litres per minute, BTPS, and with a tidal volume of 700 cm3 with a constant time interval between respirations.

(2)At cabin pressure altitudes above 5639 m (18 500 ft) up to and including 12192 m (40,000 ft), a mean tracheal oxygen partial pressure of 83·8 mmHg when breathing 30 litres per minute, BTPS, and with a tidal volume of 1100 cm3 with a constant time interval between respirations.

(d)If first-aid oxygen equipment is installed, the minimum mass flow of oxygen to each user may not be less than 4 litres per minute, STPD. However, there may be a means to decrease this flow to not less than 2 litres per minute, STPD, at any cabin altitude. The quantity of oxygen required is based upon an average flow rate of 3 litres per minute per person for whom first-aid oxygen is required.

(e)If portable oxygen equipment is installed for use by crew members, the minimum mass flow of supplemental oxygen is the same as specified in sub-paragraph (a) or (b) of this paragraph, whichever is applicable (see AMC 25.1443(e)).

IR · CS 25.1443 — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

AMCAcceptable means of compliance

AMC 25.1443(e)Minimum mass flow of portable oxygen equipment

Show the text

Cabin crew members are also ‘crew members’. Therefore, CS 25.1443(e) is applicable to portable oxygen equipment (POE) used by cabin crews. This means that the minimum mass flow provided to the portable oxygen dispensing unit of the POE must comply with the minimum mass flow required to fulfil the mean tracheal oxygen partial pressure requirements specified by CS 25.1443(a) or (b), as applicable.

Consequently, even if masks compliant with ETSO C64 are used as part of the POE, compliance with CS 25.1443(a) or (b) will have to be demonstrated for the complete POE up to:

— the maximum cabin altitude after a depressurisation event, when the POE is used as a primary means to provide hypoxia protection for the cabin crew; or

— the maximum possible level-off altitude after a depressurisation of the aeroplane, but not exceeding 7 620 m (25 000 ft), when the POE is installed to allow cabin crew mobility in aeroplanes where the passenger oxygen system design allows for levelling off at altitudes between 3 048 m (10 000 ft) and 7 620 m (25 000 ft) after a depressurisation event (typically a passenger oxygen system with a gaseous oxygen source or a chemical oxygen generator with sufficient capacity).

AMC · AMC 25.1443(e) — CS-25 · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

All rules in SUBPART F – EQUIPMENT

Consolidated from the EASA Easy Access Rules (revision 26 Jan 2023, extracted 13 Oct 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

Ask Metis about CS 25.1443 →

Metis opens with Avioverse in October 2026 · request early access.