Fault in the Slide Bottle Pressure for the LH MID Door
TASK 25-62-00-810-807-A
Fault in the Slide Bottle Pressure for the LH MID Door
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 25-62-00-710-062-B ** ON A/C NOT FOR ALL
Subtask 25-62-00-810-062-A ** ON A/C NOT FOR ALL
Subtask 25-62-00-860-072-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:27:02 UTC
Fault in the Slide Bottle Pressure for the LH MID Door
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 23-73-00-810-827-A | DEU-B - Fault in DEU-B 300RHx with connected systems/devices |
| AMM 23-73-00-740-005 | BITE-Test of the Cabin Intercommunication Data System (CIDS) through the CFDS |
| ASM 237327 | |
| AMM 23-73-47-000-001 | Removal of the Decoder/Encoder Unit B (300RH) |
| AMM 23-73-47-400-001 | Installation of the Decoder/Encoder Unit B (300RH) |
| AMM 25-62-49-000-001 | Inflation Reservoir, Escape-Slide - Removal |
| AMM 25-62-49-400-001 | Inflation Reservoir, Escape-Slide - Installation |
| ASM 256501 |
Subtask 25-62-00-710-062-B ** ON A/C NOT FOR ALL
A. Test
(1) Do the Interface and Power-Up Test of the Cabin Intercommunication Data System (CIDS) via the CFDS AMM 23-73-00-740-005.
4. Fault Isolation(1) Do the Interface and Power-Up Test of the Cabin Intercommunication Data System (CIDS) via the CFDS AMM 23-73-00-740-005.
Subtask 25-62-00-810-062-A ** ON A/C NOT FOR ALL
A. If the test gives a different maintenance message:
Subtask 25-62-00-810-113-A ** ON A/C NOT FOR ALL - Do the trouble shooting procedure related to the maintenance message.
B. If the test gives multiple maintenance messages:
Subtask 25-62-00-810-063-B ** ON A/C NOT FOR ALL - Do the trouble shooting procedure for the related DEU-B and connected systems/devices (Ref. TSM TASK 23-73-00-810-827).
C. If the test gives the maintenance message SLIDE BOTTLE 2L/ DEU-B 300RH4:
(1) Get access to the inflation reservoir AMM 25-62-49-000-001,
(a) Let temperature conditions become stable and then examine the pressure gage again.
(b) If the pressure gage continues to show an indication in AREA B:
Subtask 25-62-00-710-063-A ** ON A/C NOT FOR ALL (1) Get access to the inflation reservoir AMM 25-62-49-000-001,
NOTE: Only use the access procedure.
(2) Make sure that the pressure gage shows the correct pressure. NOTE: There are two different types of pressure gage (MODEL A and MODEL B). MODEL A has a green cursor which is temperature sensitive. MODEL B has a needle with an internal mechanism, which is temperature sensitive. They can give temporary low pressure indications when there are sudden changes from a cold to a warm environment. This usually occurs after a longer flight and the aircraft door is opened in a warm environment. The cursor/needle moves to changes in temperature faster than the gas pressure can react in the inflation reservoir.
(a) The indications for MODEL A are as follows: - AREA A (green cursor width) shows a correct pressure level.
- AREA B, which is half the range of AREA A, shows a pressure level that can be accepted if sudden temperature changes occurred in the last 60 minutes.
- The GREEN BAND shows a correct pressure level.
- AREA B, which has a range equal to AREA A, shows a pressure level that can be accepted if sudden temperature changes occurred in the last 60 minutes.
(a) Let temperature conditions become stable and then examine the pressure gage again.
(b) If the pressure gage continues to show an indication in AREA B:
- Replace the PRESSURE BOTTLE DOOR 2LH [7774MM] , AMM 25-62-49-000-001 and AMM 25-62-49-400-001.
- Replace the DEU-B [300RH4] , AMM 23-73-47-000-001 and AMM 23-73-47-400-001.
- Do a check and repair the wiring between the:
DEU-B [300RH4] connector C/27 and the SLIDE BOTTLE PRESS SENSOR connector A/A ASM 256501 and ASM 237327.
NOTE: Only use the close-up procedure.
D. Do the test as given in paragraph 3. A. to check the correct operation (no maintenance message is shown).
5. Close-upSubtask 25-62-00-860-072-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.