Removal of the Reheater
TASK 21-52-31-000-001-A
Removal of the Reheater
Two persons are necessary to do this task.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 21-52-31-861-051-A Subtask 21-52-31-865-050-A
Subtask 21-52-31-020-051-A
[Rev.10 from 2021]
2026.04.02 06:11:29 UTC
Removal of the Reheater
WARNING:
MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE.
HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING:
DO NOT TOUCH THE UNIT UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).
CAUTION:
BE VERY CAREFUL WHEN YOU DO WORK ON OR NEAR THE AIR-CONDITIONING DUCTS. THE DUCTS ARE MADE OF THIN MATERIAL AND YOU CAN EASILY BREAK THEM.
NOTE: The procedure is the same for reheaters 10HM3 and 11HM3.
1. Reason for the JobTwo persons are necessary to do this task.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | CAP - BLANKING |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | 1 | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [10HM3] (REHEATER) | |
| 191KB | |
| FOR [11HM3] (REHEATER) | |
| 192KB | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 21-52-16-000-001-A | Removal of the Water Extractor |
| TASK 21-52-23-000-003-A | Removal of the Pipe Assembly between the Anti-Ice Valve (if installed) and the Bypass Air Duct of the Primary Heat Exchanger |
| TASK 21-52-31-200-001-A | Attachment Components (In-Service Wear Limits) - Reheater |
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 53-35-13-000-002-A | Removal of the Quick-Release Access Panels from the Belly Fairing Structure |
Subtask 21-52-31-861-051-A Subtask 21-52-31-865-050-A
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 21-52-31-941-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 10HM3 (REHEATER) | |||
| 49VU | AIR COND/TEMP CTL/SYS 1 CHAN B/28VDC | 52HH | D08 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/PACK TEMP/CTL SYS1/1/115VAC | 1HH | X22 |
| 122VU | AIR COND/PACK TEMP/CTL SYS1/1/28VDC | 3HH | X21 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/1/28VDC | 4HH | Y19 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/1/115VAC | 2HH | Y18 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/115VAC | 49HH | X22 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN A/28VDC | 51HH | X21 |
| 122VU | AIR COND/TEMP CTL SYS 1/CHAN B/115VAC | 50HH | Y18 |
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 11HM3 (REHEATER) | |||
| 122VU | AIR COND/PACK TEMP/CTL SYS1/2/115VAC | 21HH | W22 |
| 122VU | AIR COND/PACK TEMP/CTL SYS1/2/28VDC | 23HH | W21 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/2/28VDC | 24HH | Y21 |
| 122VU | AIR COND/PACK TEMP CTL SYS2/2/115VAC | 22HH | Y20 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/115VAC | 53HH | W22 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN A/28VDC | 55HH | W21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/28VDC | 56HH | Y21 |
| 122VU | AIR COND/TEMP CTL SYS 2/CHAN B/115VAC | 54HH | Y20 |
C. Safety Precautions
(1) On the overhead panel, on AIR COND panel 30VU:
(a) Make sure that:
(2) On the HP ground connector, put the WARNING NOTICE(S) in position to tell persons not to supply the ground air.
Subtask 21-52-31-010-050-A ** ON A/C NOT FOR ALL (1) On the overhead panel, on AIR COND panel 30VU:
(a) Make sure that:
- The APU BLEED pushbutton switch is released (the ON legend is off).
- The ENG 1 BLEED and the ENG 2 BLEED pushbutton switches are released (the OFF legends are on).
(2) On the HP ground connector, put the WARNING NOTICE(S) in position to tell persons not to supply the ground air.
D. Get Access
(1) Remove the access panels from the belly fairing structure (Ref. AMM TASK 53-35-13-000-002):
(a) FOR [10HM3] (REHEATER)
(b) FOR [11HM3] (REHEATER)
(2) Remove the water extractor (Ref. AMM TASK 21-52-16-000-001):
(a) FOR [10HM3] (REHEATER)
Subtask 21-52-31-010-050-B ** ON A/C NOT FOR ALL (1) Remove the access panels from the belly fairing structure (Ref. AMM TASK 53-35-13-000-002):
(a) FOR [10HM3] (REHEATER)
(b) FOR [11HM3] (REHEATER)
(2) Remove the water extractor (Ref. AMM TASK 21-52-16-000-001):
(a) FOR [10HM3] (REHEATER)
- 10HM8.
- 11HM8.
D. Get Access
(1) Remove the access panels from the belly fairing structure (Ref. AMM TASK 53-35-13-000-002):
(a) FOR [10HM3] (REHEATER)
(b) FOR [11HM3] (REHEATER)
(2) Remove the water extractor (Ref. AMM TASK 21-52-16-000-001):
(a) FOR [10HM3] (REHEATER)
4. Procedure(1) Remove the access panels from the belly fairing structure (Ref. AMM TASK 53-35-13-000-002):
(a) FOR [10HM3] (REHEATER)
(b) FOR [11HM3] (REHEATER)
(2) Remove the water extractor (Ref. AMM TASK 21-52-16-000-001):
(a) FOR [10HM3] (REHEATER)
- 10HM8.
- 11HM8.
Subtask 21-52-31-020-051-A
A. Removal of the Reheater
(1) Disconnect the electrical connector (25):
(b) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(5) Remove the screw of the clamps (35), and bend the clamps (35) carefully to remove them.
(6) Remove the sleeves (17) and (26) from the flanges (15) and (29):
(a) Turn the sleeves (17) and (26) when you disconnect them.
(7) Remove the nut (8), the washer (9) and the screw (11) and disconnect the bonding strap (10).
(8) Remove the clamp (22).
(9) Remove the nuts (4) and the washers (5).
(10) Hold the reheater (12):
(a) Remove the bolts (7) and the bushings (6).
(b) Disconnect the support rods (77) and (81) and remove the reheater (12) from the aircraft.
(11) Remove and discard the seals (16) and (28), and the packing (23).
(12) Put the PLUG-BLANKING in each disconnected line end.
Subtask 21-52-31-020-052-A (1) Disconnect the electrical connector (25):
CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
(a) Disconnect the electrical connector (25).(b) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
CAUTION:
MAKE SURE THAT THE ELECTRICAL WIRE(S) IS(ARE) DISCONNECTED BEFORE YOU DISCONNECT THE BONDING STRAP(S).
(2) If applicable, disconnect the bonding strap (30) from the reheater (12): NOTE: The bonding strap (30) is only applicable for the pack-air conditioning system with the anti-ice valve.
(a) For the reheater (12) with the bonding tab: - Remove the nut (31), the washer (34) and the screw (19) and disconnect the bonding strap (30).
- Remove the screw (19) and the washer (34) and disconnect the bonding strap (30).
NOTE: The retaining cables (18) and (27) will twist, if you do not hold the hexagonal part of the retaining cables (18) and (27).
(4) Disconnect the retaining cables (18) and (27).(5) Remove the screw of the clamps (35), and bend the clamps (35) carefully to remove them.
(6) Remove the sleeves (17) and (26) from the flanges (15) and (29):
(a) Turn the sleeves (17) and (26) when you disconnect them.
(7) Remove the nut (8), the washer (9) and the screw (11) and disconnect the bonding strap (10).
(8) Remove the clamp (22).
(9) Remove the nuts (4) and the washers (5).
(10) Hold the reheater (12):
(a) Remove the bolts (7) and the bushings (6).
(b) Disconnect the support rods (77) and (81) and remove the reheater (12) from the aircraft.
(11) Remove and discard the seals (16) and (28), and the packing (23).
(12) Put the PLUG-BLANKING in each disconnected line end.
B. Removal of the Attachment Components
(1) Record the positions of the support rods to use in the Installation procedure.
(2) Hold the support rods (77) and (81) and remove the nuts (4), washers (5), bolts (7) and bushings (6).
(3) Remove the support rods (77) and (81) from the bracket (20).
(4) Do the inspection of the components for in-service wear (Ref. AMM TASK 21-52-31-200-001).
(1) Record the positions of the support rods to use in the Installation procedure.
(2) Hold the support rods (77) and (81) and remove the nuts (4), washers (5), bolts (7) and bushings (6).
(3) Remove the support rods (77) and (81) from the bracket (20).
(4) Do the inspection of the components for in-service wear (Ref. AMM TASK 21-52-31-200-001).
Reheater