(0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
 Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-005 USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
cotter pin  49-16-04 03 -070  D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage
 and in the Wings (this does not include the tanks)-
24-41-00-861-002  Energize the Aircraft Electrical Circuits from the
 External Power
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 29-00-00-864-001  Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action
 29-14-00-614-002  Pressurization of the Hydraulic Reservoirs through
 the Ground Connector
 49-16-00-710-002  Operational Test of the Air Intake Flap and Diverter
 (APS 3200)
 52-41-00-010-001  Open the APU Doors for Access
 52-41-00-410-001  Close the APU Doors after Access
 49-16-43-991-003  Fig. 401
 49-16-43-991-004  Fig. 402
 3. Job Set-up__________
 Subtask 49-16-43-860-050

 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the warning notice is in position on the panel 25VU to tell persons not to start the APU

 (2)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (3)
 Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001)

 (4)
 Make sure that the access platform is below the APU compartment.

 (5)
 Make sure that the APU access doors 315AL, 316AR are open (Ref. TASK 52-41-00-010-001).

 (6)
 Make sure that the LIGHT control switch is set to the ON position.

 Subtask 49-16-43-865-054
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
 4. Procedure
_________
 (Ref. Fig. 401/TASK 49-16-43-991-003, 402/TASK 49-16-43-991-004) Subtask 49-16-43-210-053
 A. Preparation for Installation
 (1)
 Do an inspection of the air intake flap (8) for damage, dents and cracks and do an inspection of the seal lip (9) for damage. Replace the flap if necessary.

 (2)
 Do an inspection of the seal profile (15) for damage. If necessary, replace the seal profile.

 Subtask 49-16-43-560-050
 B. Preparation of a Replacement Component (if necessary)
 (1)
 Remove the seal profile (15).

 (a) Remove the screws (18), the washers (17), the bracket (16) and then the seal profile (15) from the flap (8).

 (2)
 Installation of the the new seal profile (15).

 Air Intake Measurements
 Figure 402/TASK 49-16-43-991-004

 CES

 (a) Put the new seal profile (15) (15) and the bracket (16) in position.
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER
_______ SPECIAL MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 (b)
 Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (18) and the washers (17).

 (c)
 Install the screws (18) and the washers (17). Do not fully tighten the screws at this time.
　
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