Annexes 070-cqb Release 10
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- Words: 135
- Pages: 7
JAA Appendices
070
Technical Realization: LPLUS 2002
JAA Appendices, Subject: 070
Page Edition:12-2002
1
Table Of Contents 071-2084 A
..........................................................................................................5
071-10644 A, 071-10645A.....................................................................................6 071-12057 A
........................................................................................................7
JAA Appendices, Subject: 070
Page Edition:12-2002
2
071-2070 A
JAA Appendices, Subject: 070
Page Edition:12-2002
3
071-2083 A
JAA Appendices, Subject: 070
Page Edition:12-2002
4
071-2084 A
JAA Appendices, Subject: 070
Page Edition:12-2002
5
071-10644 A, 071-10645A
The graph below shows aeroplane cruising altitude versus cabin altitude when the aeroplane's pressure altimeter and cabin pressure Controller are set to 1013.2 mb. The graph is used to determine/select cabin altitude appropriate to the aeroplane's cruise altitude, and also, by a combination of the same parameters to determine the differential pressure prevailing at these altitudes.
JAA Appendices, Subject: 070
Page Edition:12-2002
6
071-12057 A
JAA Appendices, Subject: 070
Page Edition:12-2002
7
070
Technical Realization: LPLUS 2002
JAA Appendices, Subject: 070
Page Edition:12-2002
1
Table Of Contents 071-2084 A
..........................................................................................................5
071-10644 A, 071-10645A.....................................................................................6 071-12057 A
........................................................................................................7
JAA Appendices, Subject: 070
Page Edition:12-2002
2
071-2070 A
JAA Appendices, Subject: 070
Page Edition:12-2002
3
071-2083 A
JAA Appendices, Subject: 070
Page Edition:12-2002
4
071-2084 A
JAA Appendices, Subject: 070
Page Edition:12-2002
5
071-10644 A, 071-10645A
The graph below shows aeroplane cruising altitude versus cabin altitude when the aeroplane's pressure altimeter and cabin pressure Controller are set to 1013.2 mb. The graph is used to determine/select cabin altitude appropriate to the aeroplane's cruise altitude, and also, by a combination of the same parameters to determine the differential pressure prevailing at these altitudes.
JAA Appendices, Subject: 070
Page Edition:12-2002
6
071-12057 A
JAA Appendices, Subject: 070
Page Edition:12-2002
7
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