(2)
AMM 71-11-04/201, Fan Cowl Panels
(3)
AMM 78-31-00/201, Thrust Reverser System
B. Access
(1)
Location Zones
101/201 Control Cabin
502/503 Fan Cowl - Left Nacelle
504/505 Thrust Reverser - Left Nacelle
602/603 Fan Cowl - Right Nacelle
604/605 Thrust Reverser - Right Nacelle
(2)
Access Panels
5737/5837 Fan Cowl Assy
5738/5838 Thrust Reverser Cowl Assy
5739/5839 Thrust Reverser Cowl Assy
5746/5846 Fan Cowl Assy
C. Prepare to Remove the 5th-Stage Bleed Air Check Valve
S 864-003
(1)
Make sure the applicable engine is not in operation.
S 864-004
(2)
Put the forward thrust lever in the fully rearward position and attach a DO-NOT-OPERATE tag.
S 864-005
(3)
Put the start lever in the CUTOFF position and attach a DO-NOT-OPERATE tag.
(4)
Remove the pressure from the pneumatic system (AMM 36-05-00/201).
S 864-006
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36-11-35
ALL ú ú 01 Page 401 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 864-007
(5)
Open the applicable circuit breaker for the bleed air control on the P6 panel and attach a DO-NOT-CLOSE tag.
S 864-009
(6)
Attach a DO-NOT-OPERATE tag to the applicable BLEED switch.
S 864-023
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE THRUST REVERSER TO
_______ PREVENT THE OPERATION OF THE THRUST REVERSER. ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(7)
Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 014-010
(8)
Open fan cowl panels (AMM 71-11-02/201).
S 014-008
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS WHEN YOU OPEN THE THRUST REVERSERS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(9) Open the thrust reversers (AMM 78-31-00/201).
D. Remove the 5th-Stage Bleed Air Check Valve (Fig. 401)
S 934-013
(1)
Make a mark to show the position of the clamps which connect the 5th-stage bleed air check valve to the manifold duct.
S 034-011
(2)
Remove the V-band clamps which connect the 5th-stage bleed air check valve to the manifold duct.
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36-11-35
ALL ú ú 01 Page 402 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 024-012
(3) Remove the 5th-stage bleed air check valve.
(a) Discard the two E-seals.
TASK 36-11-35-404-001
3. 5th-stage Bleed Air Check Valve Installation
____________________________________________
A. Consumable Materials
(1) Cleaner - BMS 3-2 (AMM 20-30-31/201)
B. References
(1)
AMM 36-05-00/201, Pneumatic System
(2)
AMM 71-11-04/201, Fan Cowl Panels
(3)
AMM 78-31-00/201, Thrust Reverser System
C. Access
(1)
Location Zones
101/201 Control Cabin
502/503 Fan Cowl - Left Nacelle
504/505 Thrust Reverser - Left Nacelle
602/603 Fan Cowl - Right Nacelle
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