European aviation safety agency


EXAMPLE OF G550 OXYGEN SYSTEM: OXYGEN REQUIRED FOR DE-PRESSURIZATION AND CONTINUED CRUISE



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EXAMPLE OF G550 OXYGEN SYSTEM: OXYGEN REQUIRED FOR DE-PRESSURIZATION AND CONTINUED CRUISE

CRUISE

ALTITUDE (FT)



TIME

(HR:MIN)


REQUIRED BOTTLE PRESSURE AT DISPATCH

NUMBER OF PASSENGERS

0

1

2

4

6

8

10

15

19

25000

1:00

413

447

482

551

621

690

759

932

1071

1:30

508

560

613

717

822

927

1031

1293

1502

2:00

603

673

743

883

1023

1163

1303

1653

1933

2:30

699

786

874

1049

1225

1400

1575

2014




3:00

794

899

1005

1215

1426

1637

1847







3:30

890

1013

1136

1382

1628

1874










4:00

985

1126

1266

1548

1829













4:30

1080

1239

1397

1714

2030













5:00

1176

1352

1528

1880
















20000

1:00

369

397

424

479

534

589

644

782

892

1:30

440

481

522

605

687

770

852

1058

1223

2:00

510

565

620

730

840

950

1060

1334

1554

2:30

581

650

718

855

993

1130

1267

1611

1885

3:00

651

734

816

981

1146

1310

1475

1887




3:30

722

818

914

1106

1298

1491

1683

2163




4:00

792

902

1012

1232

1451

1671

1890







4:30

863

986

1110

1357

1604

1851










5:00

933

1070

1208

1482

1757

2031










15000

1:00

342

355

369

397

425

453

481

550

606

1:30

396

416

436

476

517

557

597

698

778

2:00

450

477

503

556

608

661

713

845

950

2:30

505

537

570

635

700

765

830

992

1122

3:00

559

598

637

714

791

869

946

1140

1295

3:30

614

659

703

793

883

973

1063

1287

1467

4:00

668

719

770

873

975

1077

1179

1435

1639

4:30

722

780

837

952

1066

1181

1296

1582

1811

5:00

777

840

904

1031

1158

1285

1412

1730

1984

Based on pressure reading at 70ºF.

Includes oxygen for three crewmembers breathing 100% oxygen for emergency descent plus two minutes. Normal dillution for remainder of flight.

Increase oxygen required by 37 PSIG for each crewmember on oxygen at/above FL410 for each 60 minutes.

Maximum system pressure is 1800 PSIG. Values in excess of 1800 are shown for interpolation purposes only.






CAT.IDE.235

Oxygen – Minimum Requirements for Supplemental Oxygen for Pressurised Aeroplanes

SUPPLY FOR:

DURATION AND CABIN PRESSURE ALTITUDE

  1. Occupants of flight crew compartment seats on flight crew compartment duty

(a) The entire flying time when the cabin pressure altitude exceeds 13 000 ft.

(b) The remainder of the flying time when the cabin pressure altitude exceeds 10 000 ft but does not exceed 13 000 ft, after the initial 30 minutes at these altitudes, but in no case less than:

(1) 30 minutes’ supply for aeroplanes certified to fly at altitudes not exceeding 25 000 ft; and

(2) 2 hours’ supply for aeroplanes certified to fly at altitudes of more than 25 000 ft.

  1. Required cabin crew members

(a) The entire flying time when the cabin pressure altitude exceeds 13 000 ft, but not less than 30 minutes’ supply.

(b) The remainder of the flying time when the cabin pressure altitude exceeds 10 000 ft but does not exceed 13 000 ft, after the initial 30 minutes at these altitudes.

  1. 100% of passengers

The entire flying time when the cabin pressure altitude exceeds 15 000 ft, but in no case less than 10 minutes’ supply.

  1. 30% of passengers

The entire flying time when the cabin pressure altitude exceeds 14 000 ft but does not exceed 15 000 ft.

  1. 10% of passengers

The remainder of the flying time when the cabin pressure altitude exceeds 10 000 ft but does not exceed 14 000 ft, after the initial 30 minutes at these altitudes.




3. Oxygen Service

Panel Pressure

Gauges


D

2

0

May be inoperative provided the associated cockpit gauge is operative and monitored.

None required.

None required.

An Inoperative Placard will be placed on Oxygen Service Panel Gauges and will be noted on ADLS.

4. Portable Oxygen

*** Dispensing Units

(Bottle and Mask)


B

-

-

Any in excess of those required by Operating Requirements may be inoperative or missing provided required distribution is maintained throughout aeroplane.

NOTE: Any bottle not properly serviced is considered inoperative and should be removed.



None required.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

5. Oxygen Supply

Warning Systems



C

2

0

May be inoperative provided associated cockpit gauge is operative and monitored.

None required.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

6. Protective Breathing

*** Equipment (PBE)



D

-

-

(M) Any in excess of that required may be inoperative or missing provided the inoperative PBE is placarded inoperative, removed from the installed location and placed out of sight so it cannot be mistaken for a functional unit.

Maintenance will ensure the inoperative PBE is removed from its installed location or placed out of sight.

Flight crew may accomplish this task if properly qualified and authorised.



None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

7. Electronic Equipment

*** Rack Oxygen Pressure

Gauges


D

-

0

May be inoperative provided cockpit gauges are operative.

None required.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

8. Cockpit Oxygen

Pressure Indications



C

-

0

May be inoperative provided:

  1. Oxygen Service Panel Pressure Gauges are operative and checked before every takeoff, and

  2. Crew Oxygen Off and Passenger Oxygen Off messages are not displayed on the CAS prior to every takeoff.

None required.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

9. First Aid Oxygen

D

-

-

(M) Any bottle in excess of those required may be inoperative provided the inoperative equipment is placarded inoperative, removed from the installed location (if portable) and placed out of sight so it cannot be mistaken for a functional unit.

Maintenance will ensure the inoperative bottle is removed from its installed location (if portable) or placed out of sight.

Flight crew may accomplish this task if properly qualified and authorised.



None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

10. High Landing Field

*** Elevation Passenger

Oxygen Controller

High Altitude Switch

(GV-SP/GIV-X)


D

1

0

May be inoperative provided the maximum Landing Field Elevation does not exceed 14,500 feet.

None required.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.

1) High Altitude

*** Switch Light

(GV-SP/GIV-X)


D

1

0

May be inoperative provided the switch position is verified to be depressed in whenever the Landing Field Elevation exceeds 14,500 feet.

None required.

None required.

An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.



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