-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-12-00-010-001 32-12-00-410-001 32-21-00-200-002 32-22-00-010-001 32-22-00-410-001 32-46-00-740-001 32-69-00-740-001
33-41-00-710-001 33-42-00-710-001 33-47-00-710-002 33-48-00-710-002
33-49-00-710-001 33-51-15-400-001
34-10-00-710-007 34-11-15-200-001 34-11-18-710-001
34-11-19-000-001
34-11-19-400-001
34-13-00-710-001 34-22-00-710-001
34-36-00-710-001 34-36-00-710-002 34-36-00-710-003 34-36-00-720-001 34-36-00-720-002 34-41-00-730-001 34-41-00-740-002 34-41-11-000-004
34-41-11-400-005
34-42-00-740-002 34-43-00-740-001 34-48-00-710-001 34-51-00-710-001 34-52-00-740-004 34-53-00-710-002 34-55-00-710-001 49-00-00-710-004 49-00-00-710-008
1EFF : ALL
1
R 1 1CES Open the Main Gear Doors for AccessClose the Main Gear Doors after AccessGeneral Visual Inspection of the Nose Landing GearNose Gear Doors - Ground Doors OpeningNose Gear Doors - Ground Doors ClosingBITE Test of the BSCUBITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is OperativeOperational Test of the Navigation LightsOperational Test of the Landing LightsOperational Test of the Logo LightsOperational Test of the Anti-Collision/Strobe LightingOperational Test of the Wing and Engine Scan LightsInstallation of the Emergency Overwing Lights 60WL (61WL, 62WL, 63WL)Test of the Angle of Attack WarningInspection/Check of the Pitot Probe (9DA1,9DA2,9DA3)Test of the TAT Sensor (11FP1, 11FP2) without the CFDSRemoval of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3)Installation of the Angle of Attack Sensor (3FP1, 3FP2, 3FP3)Operational Test of the AIR DATA Switching FunctionOperational Check of the standby compass including light test and visual checkOperational Test of the ILSOperational Test of the GPSOperational Test of the ILSFunctional Test of the ILSFunctional Test of the ILSSystem Test of the Weather RadarBITE Test of the Weather RadarRemoval of the Weather Radar Antenna Assembly (7SQ,11SQ)Installation of the Weather Radar Antenna Assembly (7SQ,11SQ)BITE Test of the Radio AltimeterBITE Test of the TCASOperational Test of GPWS Ground Self-test FunctionOperational Test of the DMEBITE Test of the ATCOperational Test of the ADFOperational Test of the VOR/MKROperational Test of the APU (4005KM) (GTCP 36-300)Operational Test of the APU (APS 3200)
1 05-51-18Page 603
1 Aug 01/051 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-00-00-710-010 Operational Test of the APU (131-9(A)) 53-15-11-200-001 Detailed Inspection of the Radome 55-32-11-000-001 Removal of the Vertical Stabilizer Leading-Edge 55-34-11-000-001 Removal of the Vertical Stabilizer Tip 56-11-11-000-001 Removal of the Windshield 56-11-11-200-001 Inspection of the Windshields 56-11-12-000-001 Removal of the Fixed Windows 56-11-12-200-001 Inspection of the Fixed Windows 56-12-11-000-001 Removal of the Sliding Windows 56-12-11-200-001 Inspection of the Sliding Windows 73-21-60-720-040 Functional Test of the Electronic Control Unit (ECU) 73-29-00-710-040 Operational Test of the FADEC on the ground (with
Engine Motoring)
78-31-00-710-042 Operational Test of the Thrust Reverser System
05-51-18-991-001 Fig. 601
**ON A/C 001-049, 051-099, 101-149, 201-299,
05-51-18-991-002 Fig. 602
R **ON A/C 151-199, 401-499,
05-51-18-991-002-A Fig. 602A
**ON A/C 301-399,
05-51-18-991-002-B Fig. 602B
**ON A/C ALL
3. Job Set-up
__________
Subtask 05-51-18-941-052
A. Not Applicable
Subtask 05-51-18-210-077
B. General
(1)
Lightning
(a)
Lightning always has two or more attachment points (one entry and one exit) on the aircraft skin.
(b)
Lightning moves back along the surface of the aircraft (swept stroke zone) between the entry and exit point. This can cause a chain of scattered attachment points along a line in the direction of travel of the aircraft.
(c)
Lightning hits some areas more frequently than others.
(2)
Aircraft zoning (Ref. Fig. 601/TASK 05-51-18-991-001)
(a)
The aircraft is divided into three zones related to the probability of lightning strike:
(b)
Zones 1 and 2 are divided into A and B areas related to the probability of continued attachment of the arc (hang on). The probability of arc hang on is low in A areas and high in B areas.
1_ Zone 1:
- surfaces where there is a high probability of initial
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