SENSING ELEMENT - OVERHEAT, WINGS (LOOP A AND B) (21HF,22HF,23HF,24HF,25HF,
___________________________________________________________________________ 26HF,27HF,28HF,29HF,37HF,38HF,39HF,40HF,41HF,42HF...) - REMOVAL/INSTALLATION
____________________________________________________________________________
TASK 36-22-16-000-001
Removal of the Overheat Sensing Elements 29HF(45HF),56HF(72HF),81HF(80HF),83HF (82HF)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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 caps No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific access platform 2.8 m (9 ft. 2 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
1EFF : ALL 1 36-22-16Page 401 1 1 May 01/05R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004
36-22-16-000-002 R 53-35-11-000-001 R 53-35-13-000-002 R R 57-41-37-000-004 R R R 57-41-37-000-005
36-22-16-991-001 36-22-16-991-002 36-22-16-991-003 R 36-22-16-991-004 R 36-22-16-991-005
3. Job Set-up
__________ Extending the Slats on the GroundRemoval of the Cables 21HF(37HF),77HF(64HF) Removal of the Wing-to-Fuselage Fairings Removal of the Quick-Release Access Panels from the Belly Fairing Structure Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Removal of the NACA Duct Panel 521BB(621BB)Fig. 401Fig. 402Fig. 403 Fig. 404 Fig. 405
R (Ref. Fig. 401/TASK 36-22-16-991-001, 402/TASK 36-22-16-991-002, 403/TASK R 36-22-16-991-003, 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005)
Subtask 36-22-16-941-050
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position in the cockpit to tell persons not to operate the slat controls.
Subtask 36-22-16-860-057
B. Aircraft Maintenance Configuration
(1)
Extend the slats fully (Ref. TASK 27-80-00-866-004).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever on panel 114VU.
Overheat Sensing Elements and Cables - Access Panels
Figure 401/TASK 36-22-16-991-001
1EFF : ALL 1 36-22-16Page 403 1 1 May 01/05R 1 1 1CES 1
Overheat Sensing Elements Figure 402/TASK 36-22-16-991-002
1EFF : 1 1R 1CES ALL 1 11 1 36-22-16 Page 404 May 01/05
Overheat Sensing Elements Figure 403/TASK 36-22-16-991-003
1EFF : 1 1R 1CES ALL 1 11 1 36-22-16 Page 405 May 01/05
R Overheat Sensing Elements Figure 404/TASK 36-22-16-991-004
1EFF : 1 1 1CES ALL 1 111 36-22-16 Page 406 May 01/05
R Overheat Sensing Elements - Typical Assemblies Figure 405/TASK 36-22-16-991-005
1EFF : 1 1 1CES ALL 1 111 36-22-16 Page 407 May 01/05
Subtask 36-22-16-865-050
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 49VU AIR BLEED/ENG 1/CTL 49VU AIR BLEED/ENG 1/MONG 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 122VU AIR BLEED/ENG 2/CTL 122VU AIR BLEED/ENG 2/MONG 5CV 3HA1 2HA1 7CV 3HA2 2HA2 B06D12D11R21Z23Z22
Subtask 36-22-16-010-050
R D. Get Access
R R (1) Put the access platform in position below the applicable access panels.
R R R (2) Remove the applicable access panels, (Ref. TASK 53-35-13-000-002), (Ref. TASK 53-35-11-000-001), (Ref. TASK 57-41-37-000-004), (Ref. TASK 57-41-37-000-005): - FOR 56HF, 81HF remove 191EB, 191CT, 521AB, 521BB, 521CB
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM PNEUMATIC 气源 2(117)
