W DOC AIRBUS | TSM A320F

Failure of the F/O Pitch Control SSTU


TASK 27-93-00-810-812-A
Failure of the F/O Pitch Control SSTU


1. Possible Causes
  • control rods, bellcranks and input levers of the transducer unit
  • SSTU-PITCH CTL, F/O [4CE4]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 27-93-00-810-979-A
Failure of the F/O Pitch Control (New-Generation Side-Stick Unit)
AMM 27-92-41-000-001
Removal of the Side Stick Assembly
AMM 27-92-41-000-002
Removal of the Transducer Units
AMM 27-92-41-400-001
Installation of the Side Stick Assembly
AMM 27-92-41-400-002
Installation of the Transducer Units
AMM 27-92-41-860-801
Identification of the Side Stick Installed on the Aircraft
AMM 27-96-00-710-020
Operational Test of the Side Stick Assembly (Activation for the BITE Test)
AMM 27-96-00-740-001
BITE Test of the EFCS (Ground Scanning)
3. Fault Confirmation
Subtask 27-93-00-860-099-A
A. Side Stick Identification
   (1) Do the identification of the side stick installed on the aircraft AMM 27-92-41-860-801:
     (a) If a new-generation side-stick unit is installed on the aircraft, refer to the trouble shooting procedure (Ref. TSM TASK 27-93-00-810-979).
     (b) If the side stick installed on the aircraft is not a new-generation side-stick unit, continue this procedure.
Subtask 27-93-00-700-072-A
B. Test
   (1) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
   (2) Do the BITE test of the EFCS (Ground Scanning) AMM 27-96-00-740-001.
4. Fault Isolation
Subtask 27-93-00-810-061-A
A. If the BITE test gives the maintenance message:
F/O PITCH CTL SSTU 4CE4
   (1) Examine the control rods, bellcranks and input levers of the transducer unit and take the corrective actions if necessary.
   (2) If no mechanical problems:
   (3) Install the F/O side stick assembly AMM 27-92-41-400-001.
Subtask 27-93-00-700-073-A
B. Do the operational test and the BITE test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:27:56 UTC