R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 21-52-24-865-052
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
R (1) FOR 10HM4
 (a) 1HH, 2HH, 3HH, 4HH, R (2) FOR 11HM4
 (a) 21HH, 22HH, 23HH, 24HH.
R  **ON A/C 401-499, 
 Subtask 21-52-24-865-052-A 
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):  
R  (1) FOR 10HM4 
 (a) 49HH, 50HH, 51HH, 52HH,  
R  (2) FOR 11HM4 
 (a) 53HH, 54HH, 55HH, 56HH. 
 **ON A/C ALL 
 Subtask 21-52-24-710-050 
 F. Test 
 (1) Do the pre-conditioning through the HP ground connector (Ref. TASK 12-33-21-618-001) or with the APU (Ref. TASK 12-33-21-618-001). 
 (2) Do a leak check of the heat exchanger unit connections. 
 NOTE : Minimum leakage is permitted. After the pack operates some____ minutes, the leakage of air will reduce because the seals have their correct operating temperature. 
 (3) After approx. 15 minutes stop the pre-conditioning (Ref. TASK 12-33-21-618-001) or (Ref. TASK 12-33-21-618-001). 
 (4) Do the operational test of the cockpit and cabin temperature control (Ref. TASK 21-63-00-710-004). 
R 1EFF : ALL 1 21-52-24Page 443 1 1 Aug 01/05 1 1 1CES 1
 5. Close-up
________ Subtask 21-52-24-410-051
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.
 (2)
 Install the access panel (Ref. TASK 53-35-13-400-002)
 FOR 10HM4
 191KB,
 FOR 11HM4
 192KB.
 (3) Remove the warning notice(s). Subtask 21-52-24-862-050
 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). 
R 1EFF : ALL 1 21-52-24Page 444 1 1 Aug 01/05 1 1 1CES 1
 TASK 21-52-24-000-001- 01 
 Removal of the Heat Exchanger Unit 10HM4 (11HM4) (From the Air Conditioning Pack) 
 NOTE : The procedure is the same for the heat exchanger unit 10HM4 and 11HM4.____ 
 1. Reason for the Job__________________ 
 Self Explanatory 
 2. Job Set-up Information______________________ 
 A. Fixtures, Tools, Test and Support Equipment 
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------- 
No specific  blanking plugs 
 B. Referenced Information 
 -------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- 
21-52-23-000-001 21-52-41-000-001 53-35-13-000-002 CMM 215200  Removal of the Pipe Assembly between the Main Heat Exchanger and the Air Cycle MachineRemoval of the Air Conditioning Pack 10HM (11HM)Removal of the Quick-Release Access Panels from the Belly Fairing Structure 
R  **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399, 
 21-52-24-991-001  Fig. 401  
R  **ON A/C 151-199, 401-499,  
R R  21-52-24-991-001-A  Fig. 401A 
R 1EFF : ALL 1 21-52-24Page 445 1 1 Aug 01/05 1 1 1CES 1
 **ON A/C ALL 
 3. Job Set-up__________ 
 Subtask 21-52-24-010-052 
 A. Get Access 
 (1) Remove the access panel/s (Ref. TASK 53-35-13-000-002). 
 (a) FOR 10HM4 - 191KB; 
 (b) FOR 11HM4 - 192KB. 
 4. Procedure_________ 
 Subtask 21-52-24-020-052 
 A. Removal of the Heat Exchanger Unit  
R  **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399, 
 (Ref. Fig. 401/TASK 21-52-24-991-001)  
R  **ON A/C 151-199, 401-499,  
R R (Ref. Fig. 401A/TASK 21-52-24-991-001-A)  
**ON A/C ALL 
 NOTE : Turn the sleeves (16), (88) and (59) when you move them or when____ you remove them. This will help to prevent damage to the internal seals. 
 (1) Remove the air conditioning pack (Ref. TASK 21-52-41-000-001). 
 NOTE : Make sure that the air conditioning pack is securely fastened____ in the correct support stand (Ref. CMM 215200) before you remove any of the pack components. 
R 1EFF : ALL 1 21-52-24Page 446 1 1 Aug 01/05 1 1 1CES 1 Damage to the individual components could occur if it is not correctly supported.
 (2)
 Remove the pipe assembly (Ref. TASK 21-52-23-000-001).
 (3)
 Remove the clamp (9) and the sleeve (8).
 (4)
 Remove the nut (45), the washer (44), the bonding strap (41) and the screw (42).
 
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