(1) Deviation #1: ETSO‑C78 §4.1 General (Marking)/TSO C78 – (b) marking
The regulator being mask-mounted to compose a single piece of equipment, Intertechnique has added the markings required in ETSO-C78 §4.1/TSO C78 (b) to the markings required in ETSO-C89 §4.1/TSO C89 (b) on plates attached to the regulator. Intertechnique claims that these deviations have already been approved by the FAA for LODA for mask-regulator MC10 series by letter MCB/11/26 dated Nov. 26, 1973.
(2) Deviation #2 ETSO-C78 FAA standard associated with ETSO‑C78 §3.3 (a)/TSO C78 §3.3 (a)
The regulator being mask-mounted to compose a single piece of equipment, Intertechnique has performed the inward leakage test on the mask-regulator assembly and cumulated the maximum mask inward leakage (0.1 L/min STPD as in ETSO-C78 FAA standard associated with ETSO-C78 §3.3 (a)/TSO C78 §3.3 (a)) and the maximum regulator inward leakage (0.1 L/min STPD as in ETSO-C89 FAA Standard associated with ETSO-C89 §4.4 (a)/TSO C89 §4.4 (a)). Though, the maximum mask-regulator inward leakage considered for the tests was 0.2 L/min STPD. Intertechniqueclaims that the deviation has already been accepted by the FAA in LODA for mask-regulator MC10 series by letter MCB/11/26 dated Nov. 26, 1973.
(3) Deviation #3 ETSO‑C78 FAA standard associated with ETSO‑C78 §3.4 (a)/TSO C78 §3.4 (a) and ETSO‑C89 FAA Standard associated with ETSO‑C89 §4.1 (a)/TSO C89 §4.1 (a)
The regulator being mask-mounted and so integrating the whole inspiratory circuit, Intertechnique has performed the inspiratory resistance test on the regulator only and cumulated the maximum mask inspiratory resistance (ETSO C78 FAA standard associated with ETSO-C78 §3.4 (a)/TSO C78 §3.4 (a)) and the maximum regulator inspiratory resistance (ETSO C89 FAA Standard associated with ETSO-C89 §4.1(a)/TSO C89 §4.1 (a)).
The maximum mask-regulator inspiratory resistance considered for the test is defined as follows:
Flow (L/min STPD) |
Suction pressure (inches H2O) as per TS0 C78 § 3.4 (a) |
Suction pressure (inches H2O) as per TS0 C89 § 4.1 (a) |
Suction pressure (inches H2O) maximum value |
20 |
0.6 |
0.4 |
1 |
70 |
1.5 |
0.8 |
2.3 |
100 |
2.5 |
1.0 |
3.5 |
Intertechnique claims that the deviation has already been accepted by the FAA in LODA for mask-regulator MC10 series by letter MCB/11/26 dated Nov. 26, 1973.
(4) Deviation #4 ETSO‑C89 FAA Standard associated with ETSO‑C89 §4.4 (c)/TSO C89 §4.4 (c) and ETSO‑C89 FAA Standard associated with ETSO‑C89 §4.4 (d)/TSO C89 §4.4 (d)
(5) Deviation #5 ETSO C89 FAA Standard associated with ETSOC89 §4.2 (a)/TSO C89 §4.2 (a)
This diluter schedule proposal results from a recent study analyzing the hypoxia protection to 45 000 ft according to the pre-breathing dilution schedule and the& altimetric pressure breathing. This study has been exposed to the SAE A10 (Aircraft Oxygen Equipment Committee) group members in May 2006. This study is attached as a complete file in Annex 1.
(6) Deviation #6 ETSO‑C89 FAA Standard associated with ETSO‑C89 §4.3 (a)/TSO C89 §4.3 (a)
Altitude (ft) |
Minimum Positive pressure (H2O Inch) Per TSO C89 §4.3 (a) |
Minimum Positive pressure (H2O Inch) Per IN/div>Pressure schedule> |
Maximum Positive pressure (H2O Inch) Per TSO >C89 §4.3 (a) |
Maximum Positive pressure (H2O Inch) Per IN pressure schedule |
30000 |
0 |
0 |
3.5 |
3.5 |
40000 |
0 |
1.8 |
5.0 |
12 |
42000 |
4.5 |
5.6 |
7.5 |
12 |
44000 |
9.0 |
8.6 |
11.0 |
12 |
45000 |
11.0 |
10.0 |
12.0 |
12 |