DOC AIRBUS | AMM A320FTable of Idle Indications [IAE]
TASK 71-00-00-860-011-C-01
Table of Idle Indications
1. Reason for the Job
This task is for A5 engines only, which have SBE 72-0565 incorporated (SelectOne retrofit standard) or SBE 72-0560, SBE 72-0561, SBE 72-0562, SBE 72-0563, SBE 72-0564 and SBE 73-0203 (SelectOne production standard) incorporated or which have SBE 73-0236 incorporated (SelectTwo retrofit standard), including engines that have SB 72-0285 and SB 73-0237 incorporated (reduced ground idle option).
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 71-00-00-970-061-A ** ON A/C NOT FOR ALL
Subtask 71-00-00-860-178-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:27:57 UTC
Table of Idle Indications
1. Reason for the Job
This task is for A5 engines only, which have SBE 72-0565 incorporated (SelectOne retrofit standard) or SBE 72-0560, SBE 72-0561, SBE 72-0562, SBE 72-0563, SBE 72-0564 and SBE 73-0203 (SelectOne production standard) incorporated or which have SBE 73-0236 incorporated (SelectTwo retrofit standard), including engines that have SB 72-0285 and SB 73-0237 incorporated (reduced ground idle option).
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TASK 71-00-00-700-011-B | Test No.13 : Pretested Replacement Engine Test |
| TASK 71-00-00-710-012-B | Test No.3 : Idle Leak Check |
| TASK 71-00-00-710-013-C | Test No.11 : High Power Assurance Test |
| TASK 71-00-00-710-043-A | Normal Engine Automatic-Start Procedure |
| TASK 71-00-00-710-047-A | Normal Engine Manual-Start Procedure |
Engine Idle Indications (POST SBE 73-0203, PRE SBE 73-0222)Subtask 71-00-00-970-061-A ** ON A/C NOT FOR ALL
A. Reason for Tables
(1) The tables are included to specify normal engine operation when referenced by the procedures:
(3) Tables apply for static ground test only, after the engines have thermally stabilized.
Subtask 71-00-00-970-062-A ** ON A/C NOT FOR ALL (1) The tables are included to specify normal engine operation when referenced by the procedures:
- (Ref. AMM TASK 71-00-00-710-043)
- (Ref. AMM TASK 71-00-00-710-047)
- (Ref. AMM TASK 71-00-00-710-012)
- (Ref. AMM TASK 71-00-00-710-013)
- (Ref. AMM TASK 71-00-00-700-011)
(3) Tables apply for static ground test only, after the engines have thermally stabilized.
B. Parameter values
(1) Tolerances apply to all listed data.
(2) Altitude corrections apply to atmospheric pressure.
(3) Outside Air Temperature (OAT) is in degrees Celsius (deg C).
To convert from lb/hr to kg/hr, multiply by 0.4536.
4. Procedure(1) Tolerances apply to all listed data.
(2) Altitude corrections apply to atmospheric pressure.
(3) Outside Air Temperature (OAT) is in degrees Celsius (deg C).
NOTE: Take the OAT in the shade at the airplane nose gear.
(4) To convert from kg/hr to lb/hr, multiply by 2.2046. To convert from lb/hr to kg/hr, multiply by 0.4536.
Subtask 71-00-00-860-178-A ** ON A/C NOT FOR ALL
A. Table of Idle Parameters.
(1) Refer to the assurance tables.
(1) Refer to the assurance tables.
NOTE: Aircraft/Engines bleed configuration for the Table of Idle Parameters is:
- Bleeds OFF
- ECS Bleeds OFF
- Bleeds OFF
- ECS Bleeds OFF