Airbus A318 A319 A320 A321 Aircraft Maintenance Manual – Chapter 30 Ice and Rain Protection
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Comprehensive Airbus A318, A319, A320, and A321 Aircraft Maintenance Manual (AMM) Chapter 30 covering Ice and Rain Protection systems. Features full technical descriptions, pneumatic schematics, MMEL deactivation and reactivation tasks, operational BITE testing, and removal/installation procedures for wing anti-ice valves, piccolo ducts, engine cowl heating, air data probe heat, windshield defogging, and drain masts.
Description
Airbus A318 A319 A320 A321 Aircraft Maintenance Manual – Chapter 30 Ice and Rain Protection
The Airbus A318 A319 A320 A321 Aircraft Maintenance Manual – Chapter 30 Ice and Rain Protection provides exhaustive line-maintenance, workshop, and troubleshooting instructions for technicians maintaining the ice and rain protection systems across the entire single-aisle family. Released under AES Revision No. 40, this dedicated AMM Chapter 30 document covers hot bleed air airfoil heating, nacelle intake protection, electrical flight-instrument probe heating, flight compartment windshield anti-icing and defogging, windshield wipers, rain repellent systems, and heated drain mast installations. Whether performing scheduled inspections, isolating class 3 faults on the Centralized Fault Display System (CFDS), or executing Master Minimum Equipment List (MMEL) valve locking procedures, this technical publication serves as the definitive reference manual.
Document & File Details
- Manual Type: Aircraft Maintenance Manual (AMM)
- Brand / Manufacturer: Airbus
- Covered Aircraft Models: Airbus A318, Airbus A319, Airbus A320, Airbus A321
- ATA Chapter: Chapter 30 (Ice and Rain Protection)
- Document Revision: Revision No. 40 (AES)
- Revision Date: May 01, 2012
- Language: English
- File Format: Portable Document Format (PDF)
- Total Page Count: 631 pages
IMAGES PREVIEW
Chapters & Sections Covered
- 30-00-00 Ice and Rain Protection – General: Overall system description and operation, general component layout, wing and engine anti-ice schematics, probe heating distribution, window heat schematics and glass cross-sections, drain mast locations, visual ice detection indicators, and complete AC/DC electrical bus power distribution diagrams.
- 30-10-00 Airfoil: Aerodynamic surface protection principles, thermal anti-icing delivery via engine bleed air, and internal hot air distribution across wing leading edge slats.
- 30-11-00 Wing Ice Protection: Full description and operation of LH and RH slat 3, 4, and 5 thermal protection, pneumatic supply downstream of precooler, cockpit overhead panel 25VU controls, warning logic, Electronic Centralized Aircraft Monitoring (ECAM) indications, and Multipurpose Control and Display Unit (MCDU) BITE displays.
- 30-11-00 Deactivation / Reactivation & Testing: MMEL Task 30-11-01 procedures to lock wing anti-ice control valves in CLOSED or OPEN positions, fault light deactivation/reactivation, 30-second ground operational testing, and pneumatic supply duct leak checks using Ground Air Power Carts (GAPC).
- 30-11-41 Duct – Telescopic: Removal and installation of leading-edge telescopic ducts at track 7/rib 13, including three-stage sliding sleeve inspection, link rod connections, torque values, and slat extension/retraction verification tests.
- 30-11-42 Duct – Anti-Ice: Detailed disassembly, seal replacement, insulation muff safety wiring, bonding strap continuity, and reassembly of fixed leading-edge anti-ice ducts across wing ribs 9 through 13.
- 30-11-51 Valve – Wing Anti-Ice Control: Removal, bench check, and installation procedures for wing anti-ice control valves 9DL and 10DL, actuator coupling alignments, and scheduled replacement of internal pneumatic valve filters (Task 30-11-51-960-001-A).
- 30-21-00 Engine Air Intake Ice Protection: High-pressure compressor 7th-stage bleed air routing, solenoid-operated nacelle anti-ice (NAI) butterfly shut-off valves, upstream motive pressure limits, flight phase ECAM warning inhibition logic, and manual locking override procedures.
- 30-21-00 Engine Anti-Ice Maintenance Tasks: MMEL deactivation and reactivation tasks for engine anti-ice valves locked in OPEN or CLOSED configurations, fault warning operational checks, partial power assurance testing, and NAI valve muscle pressure testing with test set 98D36003000003.
- 30-21-49 Ducts – Anti-Ice: Removal, installation, and rigging of engine intake anti-ice ducts No. 1 through No. 5, pylon anti-ice duct stop plate modifications, and TAI interbulkhead spray ring assembly procedures.
- 30-31-00 Probe Ice Protection: Independent electrical heating networks for CAPT, F/O, and STBY channels covering pitot tubes, static ports, Angle of Attack (AOA/alpha) sensors, and Total Air Temperature (TAT) probes, accompanied by Probe Heat Computer (PHC) functional tests and insulation resistance testing.
- 30-42-00 Windshield Anti-Icing and Defogging: Electrical heating film and resistance wire controls for cockpit front windshields, fixed side windows, and sliding windows, regulated between 35°C and 42°C by Window Heat Computers (WHC).
- 30-45-00 Windshield Rain Protection: Dual independent two-speed windshield wiper systems (95 cycles/min slow, 140 cycles/min fast) with parked aerodynamic stowage, rain repellent fluid can servicing, solenoid valves, and spray nozzle adjustments.
- 30-71-00 Drain Mast Ice Protection: Dual-power heated waste-water drain masts (4DU and 14DU) operating at 18.72 W on the ground and 313.6 W in flight, temperature sensors, and electronic control units.
- 30-72-00 & 30-73-00 Potable Water Ice Protection & Panel Heating: Heated service panels, fill/drain nipples (11DV), line heater elements, and BITE test routines.
- 30-81-00 Ice Detection: Visual cockpit center windshield post icing indicator installation, inspection, and LED illumination replacement.
Together, these organized chapters give aircraft engineers, line technicians, and airframe mechanics an end-to-end technical dossier. Every subsystem is documented from theory of operation and system schematics down to circuit breaker references on panels 49VU, 121VU, and 122VU, specific mechanical torque limits, expendable seal part numbers, and ground safety lockouts.
Pneumatic Wing Anti-Ice Operation & Component Servicing
The pneumatic wing ice protection system documented in this Airbus A318 A319 A320 A321 Aircraft Maintenance Manual – Chapter 30 Ice and Rain Protection utilizes engine bleed air extracted downstream of the precooler. Hot compressed air is delivered along the wing fixed leading edge to thermal anti-icing piccolo tubes inside slats 3, 4, and 5. Technicians will find complete functional descriptions of the electro-pneumatic wing anti-ice valves (FIN 9DL on the left wing and 10DL on the right wing), which are spring-loaded to the safe closed position in the event of electrical power interruption. The manual outlines the precise regulating parameters: valves maintain downstream air outlet pressure at 1.55 bar (22.48 psi) ± 0.17 bar (2.46 psi), with internal pressure switches triggering ECAM fault warnings if supply pressure drops below 0.9 bar (13.05 psi) or exceeds 2.2 bar (31.9 psi).
Detailed step-by-step procedures outline how to safely remove, inspect, and reinstall wing anti-ice control valves, including coupling torque specifications of 0.39 to 0.51 m.daN (34.5 to 45.1 lbf.in), locating pin engagements, and scheduled replacement of the integrated anti-ice valve filter (Material No. 19-010 lockwire and replacement O-rings). Furthermore, the maintenance text covers the complete maintenance sequence for the track 7 telescopic duct assemblies, guiding mechanics through extension, link rod torquing (0.6 to 0.9 m.daN / 53.1 to 79.6 lbf.in), alignment pins, and operational slat travel checks.
Complete Bookmarks
The complete bookmarks in the “Airbus A318 A319 A320 A321 Aircraft Maintenance Manual – Chapter 30 Ice and Rain Protection” are as follows:
+Chapter 30 – ICE AND RAIN PROTECTIONp. 1
+30-00 – ICE AND RAIN PROTECTION – GENERALp. 11
+30-00-00 – ICE AND RAIN PROTECTION – GENERALp. 11
+30-00-00 PB 001 CONF 00 – ICE AND RAIN PROTECTION – GENERAL – DESCRIPTION AND OPERATIONp. 11
+30-10 – AIRFOILp. 35
+30-10-00 – AIRFOILp. 35
+30-10-00 PB 001 CONF 00 – AIRFOIL – DESCRIPTION AND OPERATIONp. 35
+30-11 – WING ICE PROTECTIONp. 38
+30-11-00 – WING ICE PROTECTIONp. 38
+30-11-00 PB 001 CONF 00 – WING ICE PROTECTION – DESCRIPTION AND OPERATIONp. 38
+30-11-00 PB 401 CONF 00 – WING ICE PROTECTION – DEACTIVATION/REACTIVATIONp. 62
+30-11-00-040-001-A – Deactivation of the Wing Anti-Ice Control Valve to the CLOSED positionp. 62
+30-11-00 PB 501 CONF 00 – WING ICE PROTECTION – ADJUSTMENT/TESTp. 83
+30-11-00-710-001-A – Operational Test of the Wing Ice-Protection Systemp. 83
+30-11-00-790-001-A – Leak Test of the Wing Anti-Ice Ductsp. 88
+30-11-41 – DUCT – TELESCOPICp. 93
+30-11-41 PB 401 CONF 00 – DUCT – TELESCOPIC – REMOVAL/INSTALLATIONp. 93
+30-11-41-000-001-A – Removal of the Telescopic Ductp. 93
+30-11-42 – DUCT – ANTI-ICEp. 102
+30-11-42 PB 401 CONF 00 – DUCT – ANTI-ICE – REMOVAL/INSTALLATIONp. 102
+30-11-42-000-001-A – Removal of the Anti-Ice Ductp. 102
+30-11-51 – VALVE – WING ANTI ICE CONTROLp. 116
+30-11-51 PB 401 CONF 00 – VALVE – WING ANTI ICE CONTROL – REMOVAL/INSTALLATIONp. 116
+30-11-51-000-001-A – Removal of the Wing Anti-Ice Control Valvep. 116
+30-11-51-000-002-A – Removal of the Anti-Ice Valve Filterp. 123
+30-21 – ENGINE AIR INTAKE ICE PROTECTIONp. 132
+30-21-00 – ENGINE AIR INTAKE ICE PROTECTIONp. 132
+30-21-00 PB 001 CONF 13 – ENGINE AIR INTAKE ICE PROTECTION – DESCRIPTION AND OPERATIONp. 132
+30-21-00 PB 401 CONF 13 – ENGINE AIR INTAKE ICE PROTECTION – DEACTIVATION/REACTIVATIONp. 150
+30-21-00-040-010-C – Deactivation of the Engine Anti-Ice Valve in the OPEN Positionp. 150
+30-21-00 PB 501 CONF 00 – ENGINE AIR INTAKE ICE PROTECTION – ADJUSTMENT/TESTp. 163
+30-21-00-710-003-A – Operational Test of the NAI Valvep. 168
+30-21-49 – DUCTS – ANTI ICEp. 172
+30-21-49 PB 401 CONF 13 – DUCTS – ANTI ICE – REMOVAL/INSTALLATIONp. 172
+30-21-49-000-010-B – Removal of the Anti-ice Duct No. 1p. 172
+30-21-49-000-042-A – Removal of the Pylon Anti-ice Ductp. 198
+30-21-49-000-015-A – Removal of the Anti-Ice Interbulkhead Systemp. 203
+30-21-49 PB 501 CONF 13 – DUCTS – ANTI ICE – ADJUSTMENT/TESTp. 210
+30-21-49-820-001-A – Rig the Anti-ice Ductsp. 210
+30-21-49 PB 601 CONF 13 – DUCTS – ANTI ICE – INSPECTION/CHECKp. 221
+30-21-49-200-010-B – Detailed Visual Inspection of the Inlet Cowl Anti-Ice Supply Ducts and Associated Hardware in the Core Compartmentp. 221
+30-21-49-200-011-A – General Check of the Anti-Ice Ductsp. 230
+30-21-49-200-013-B – Detailed Check of the Anti-Ice Interbulkhead System with Component Removalp. 235
+30-21-51 – VALVE – ENGINE AIR INTAKE ANTI-ICEp. 245
+30-21-51 PB 401 CONF 13 – ANTI ICE VALVE – ENGINE AIR INTAKE – REMOVAL/INSTALLATIONp. 245
+30-21-51-000-010-B – Removal of the Engine Air Intake Anti-ice Valvep. 245
+30-21-51 PB 601 CONF 13 – ANTI ICE VALVE – ENGINE AIR INTAKE – INSPECTION/CHECKp. 253
+30-31 – PROBE ICE PROTECTIONp. 256
+30-31-00 – PROBE ICE PROTECTIONp. 256
+30-31-00 PB 001 CONF 00 – PROBE ICE PROTECTION – DESCRIPTION AND OPERATIONp. 256
+30-31-00 PB 401 CONF 00 – PROBE ICE PROTECTION – DEACTIVATION/REACTIVATIONp. 278
+30-31-00 PB 501 CONF 00 – PROBE ICE PROTECTION – ADJUSTMENT/TESTp. 323
+30-31-00-710-007-A – Functional Test of the Heating of the Angle of Attack Sensorp. 327
+30-31-00-720-001-A – Functional Test of the Insulation Resistance of the Pitot Probe Heaterp. 335
+30-31-34 – COMPUTER – PROBE HEAT (PHC)p. 339
+30-31-34 PB 401 CONF 00 – COMPUTER – PROBE HEAT (PHC) – REMOVAL/INSTALLATIONp. 339
+30-31-34-000-002-A – Removal of the Probe Heat Computer (PHC)p. 339
+30-42 – WINDSHIELD ANTI-ICING AND DEFOGGINGp. 345
+30-42-00 – WINDSHIELD ANTI-ICING AND DEFOGGINGp. 345
+30-42-00 PB 001 CONF 00 – WINDSHIELD ANTI-ICING AND DEFOGGING – DESCRIPTION AND OPERATIONp. 345
+30-42-00 PB 401 CONF 00 – WINDSHIELD ANTI-ICING AND DEFOGGING – DEACTIVATION/REACTIVATIONp. 370
+30-42-00 PB 501 CONF 00 – WINDSHIELD ANTI-ICING AND DEFOGGING – ADJUSTMENT/TESTp. 375
+30-42-34 – COMPUTER – WINDOW HEAT (WHC)p. 379
+30-42-34 PB 401 CONF 00 – COMPUTER – WINDOW HEAT (WHC) – REMOVAL/INSTALLATIONp. 379
+30-42-34-000-001-A – Removal of the Window Heat Computer (WHC)p. 379
+30-45 – WINDSHIELD RAIN PROTECTIONp. 384
+30-45-00 – WINDSHIELD RAIN PROTECTIONp. 384
+30-45-00 PB 001 CONF 00 – WINDSHIELD RAIN PROTECTION – DESCRIPTION AND OPERATIONp. 384
+30-45-00 PB 301 CONF 00 – WINDSHIELD RAIN PROTECTION – SERVICINGp. 406
+30-45-00-600-001-A – Servicing of the Rain Repellent Fluid Canp. 406
+30-45-00-600-002-A-01 – Servicing of the Rain Repellent Systemp. 411
+30-45-00 PB 401 CONF 00 – WINDSHIELD RAIN PROTECTION – DEACTIVATION/REACTIVATIONp. 417
+30-45-00-040-002-A – Deactivation of the Rain Repellent Systemp. 417
+30-45-00 PB 501 CONF 00 – WINDSHIELD RAIN PROTECTION – ADJUSTMENT/TESTp. 430
+30-45-00-720-002-A – Functional Test of the Rain Repellent Systemp. 433
+30-45-00 PB 601 CONF 00 – WINDSHIELD RAIN PROTECTION – INSPECTION/CHECKp. 439
+30-45-00-200-001-A – Inspection/Check of the Operation of the Windshield Wipers.p. 439
+30-45-41 – VALVE – RAIN REPELLENT SOLENOIDp. 442
+30-45-41 PB 401 CONF 00 – VALVE – RAIN REPELLENT SOLENOID – REMOVAL/INSTALLATIONp. 442
+30-45-41-000-001-A – Removal of the Rain-Repellent Solenoid Valvep. 442
+30-45-43 – GAGE ASSY – RAIN REPELLENT FLUIDp. 450
+30-45-43 PB 401 CONF 00 – GAGE ASSY – RAIN REPELLENT FLUID – REMOVAL/INSTALLATIONp. 450
+30-45-43-000-001-A – Removal of the Rain-Repellent Fluid Gage Assyp. 450
+30-45-44 – NOZZLE – SPRAYp. 458
+30-45-44 PB 401 CONF 00 – NOZZLE – SPRAY – REMOVAL/INSTALLATIONp. 458
+30-45-44-000-001-A – Removal of the Spray Nozzlep. 458
+30-45-44-400-001-A – Installation of the Spray Nozzlep. 461
+30-45-45 – RESERVOIR – RAIN REPELLENT BLOWOUTp. 464
+30-45-45 PB 401 CONF 00 – RESERVOIR – RAIN REPELLENT BLOWOUT – REMOVAL/INSTALLATIONp. 464
+30-45-45-000-001-A – Removal of the Check Valve and of the Rain Repellent Blowout Reservoirp. 464
+30-45-46 – CHECK VALVE – RAIN REPELLENTp. 470
+30-45-46 PB 401 CONF 00 – CHECK VALVE – RAIN REPELLENT – REMOVAL/INSTALLATIONp. 470
+30-45-46-000-001-A – Removal of the Rain-Repellent Check Valvep. 470
+30-45-51 – MOTOR CONVERTER – WIPERp. 477
+30-45-51 PB 401 CONF 00 – MOTOR CONVERTER – WIPER – REMOVAL/INSTALLATIONp. 477
+30-45-51-000-001-A – Removal of the Wiper Motor Converterp. 477
+30-45-52 – ARM – WIPERp. 483
+30-45-52 PB 401 CONF 00 – ARM – WIPER – REMOVAL/INSTALLATIONp. 483
+30-45-52-000-002-A – Removal of the Wiper Armp. 483
+30-45-52-400-002-A – Installation of the Wiper Armp. 487
+30-45-53 – BLADE – WIPERp. 494
+30-45-53 PB 401 CONF 00 – BLADE – WIPER – REMOVAL/INSTALLATIONp. 494
+30-45-53-000-001-A – Removal of the Wiper Bladep. 494
+30-71 – DRAIN MAST ICE PROTECTIONp. 499
+30-71-00 – DRAIN MAST ICE PROTECTIONp. 499
+30-71-00 PB 001 CONF 00 – DRAIN MAST ICE PROTECTION – DESCRIPTION AND OPERATIONp. 499
+30-71-00 PB 401 CONF 00 – DRAIN MAST ICE PROTECTION – DEACTIVATION/REACTIVATIONp. 510
+30-71-00-040-001-A – Deactivation of the Waste-Water Drain Mast Heating-Systemp. 510
+30-71-00 PB 501 CONF 00 – WASTE WATER ICE PROTECTION – ADJUSTMENT/TESTp. 515
+30-71-17 – SENSOR – TEMPERATUREp. 520
+30-71-17 PB 401 CONF 00 – SENSOR – TEMPERATURE – REMOVAL/INSTALLATIONp. 520
+30-71-17-000-001-A – Removal of the Waste-Water De-icing Sensorp. 520
+30-71-34 – CONTROL UNIT – WASTE WATER ICE PROTECTIONp. 525
+30-71-34 PB 401 CONF 00 – CONTROL UNIT – WASTE WATER ICE PROTECTION – REMOVAL/INSTALLATIONp. 525
+30-71-34-000-001-A – Removal of the Waste-Water Ice-Protection Control-Unitp. 525
+30-71-51 – DRAIN MASTp. 531
+30-71-51 PB 401 CONF 00 – DRAIN MAST – REMOVAL/INSTALLATIONp. 531
+30-71-51-000-001-A – Removal of the Drain Mastp. 531
+30-71-51-400-001-A – Installation of the Drain Mastp. 537
+30-71-51 PB 601 CONF 00 – DRAIN MAST – INSPECTION/CHECKp. 547
+30-71-51-200-001-A – Visual Inspection of the Drain Mastp. 547
+30-71-53 – HEATER ELEMENTp. 552
+30-71-53 PB 401 CONF 00 – HEATER ELEMENT – REMOVAL/INSTALLATIONp. 552
+30-71-53-000-001-A – Removal of the Waste-Water De-icing Heater Elementsp. 552
+30-72 – WATER SERVICING PANELS HEATINGp. 558
+30-72-00 – WATER SERVICING PANELS HEATINGp. 558
+30-72-00 PB 001 CONF 00 – WATER SERVICING PANELS HEATING – DESCRIPTION AND OPERATIONp. 558
+30-72-11 – THERMOSTAT – FILL/DRAIN/OVERFLOW NIPPLEp. 566
+30-72-11 PB 401 CONF 00 – THERMOSTAT – FILL/DRAIN/OVERFLOW NIPPLE – REMOVAL/INSTALLATIONp. 566
+30-72-11-000-001-A – Removal of the Thermostatp. 566
+30-72-52 – NIPPLE – FILL/DRAIN/OVERFLOWp. 572
+30-72-52 PB 401 CONF 00 – NIPPLE – FILL/DRAIN/OVERFLOW – REMOVAL/INSTALLATIONp. 572
+30-72-52-000-001-A – Removal of the Heated Fill/Drain Nipple 11DV and/or Overflow Nipple 13DVp. 572
+30-73 – POTABLE WATER ICE PROTECTIONp. 579
+30-73-00 – POTABLE WATER ICE PROTECTIONp. 579
+30-73-00 PB 001 CONF 00 – POTABLE WATER ICE PROTECTION – DESCRIPTION AND OPERATIONp. 579
+30-73-00 PB 501 CONF 00 – POTABLE WATER ICE PROTECTION – ADJUSTMENT/TESTp. 588
+30-73-17 – SENSORp. 593
+30-73-17 PB 401 CONF 00 – SENSOR – REMOVAL/INSTALLATIONp. 593
+30-73-17-000-001-A – Removal of the Potable-Water De-icing Sensorp. 593
+30-73-34 – CONTROL UNIT – POTABLE WATER ICE PROTECTIONp. 598
+30-73-34 PB 401 CONF 00 – CONTROL UNIT – POTABLE WATER ICE PROTECTION – REMOVAL/INSTALLATIONp. 598
+30-73-34-000-001-A – Removal of the Potable and Waste Water Ice Protection Control Unitp. 598
+30-73-53 – HEATER ELEMENTp. 603
+30-73-53 PB 401 CONF 00 – HEATER ELEMENT – REMOVAL/INSTALLATIONp. 603
+30-73-53-000-001-A – Removal of the Potable-Water De-icing Heater Elementsp. 603
+30-81 – ICE DETECTIONp. 611
+30-81-00 – ICE DETECTIONp. 611
+30-81-00 PB 001 CONF 00 – ICE DETECTION – DESCRIPTION AND OPERATIONp. 611
+30-81-21 – INDICATOR – VISUAL, ICINGp. 622
+30-81-21 PB 401 CONF 01 – INDICATOR – LIGHTED, ICING – REMOVAL/INSTALLATIONp. 622
+30-81-21-000-001-A – Removal of the Lighted Icing Indicatorp. 622
+30-81-21 PB 601 CONF 00 – INDICATOR – VISUAL, ICING – INSPECTION/CHECKp. 630
MMEL Valve Deactivation & Ground Testing Standards
When unexpected valve malfunctions occur on the line, maintaining operational dispatch capability is paramount. This manual provides direct compliance procedures for Master Minimum Equipment List dispatch under ATA 30-11 and ATA 30-21. Mechanics are guided through deactivating and securing the wing anti-ice control valves 9DL and 10DL in the CLOSED position using the integrated manual locking pin, lockwire (0.8 mm stainless steel annealed), and mandatory cockpit placards. For right-hand wing valve 10DL, deactivation to the OPEN position is fully detailed, highlighting specific flight operation limitations and slat overheat precautions.
Similar MMEL procedures govern the nacelle anti-ice valves (FIN 4000DN) on engine air intakes, including mechanical manual override limits (maximum 50 lbf.in / 0.56 m.daN applied to the hexagonal shaft nut) and locking pin placement. In addition, the guide provides comprehensive instructions for the 30-second ground operational test of the wing anti-ice system, complete with relay timing checks (relay 4DL and 5DL) to prevent thermal damage to extended slats, as well as ground leak testing instructions utilizing external Ground Air Power Carts connected to the high-pressure receptacle on access panel 191DB.
Electrical Probe, Window Heat & Waste Water Heating Systems
Beyond pneumatic thermal systems, this manual provides detailed coverage of the high-amperage electrical de-icing networks managed by dedicated avionics computers. Technicians gain access to wiring and sensor diagrams for the Probe Heat Computers (PHC 1, 2, and 3), controlling 115V AC supplies to pitot probes, Angle of Attack sensors, and TAT sensors, alongside 28V DC power routed to static ports. Ground/flight detector logic, automatic probe heat startup upon first engine start, and ground temperature attenuation are fully mapped.
The flight deck windshield anti-icing and defogging chapter details the construction and heating circuits of front laminated glass (incorporating chemical-reinforced plies and continuous heating films) and side acrylic windows. Temperature regulation by the dual Window Heat Computers (WHC 1 and 2) is documented with sensor resistance charts holding temperatures between 35°C (95°F) and 42°C (107.6°F). Complete removal, installation, and inspection routines are also provided for two-speed windshield wiper motor converters, rain repellent solenoid valves, and fuselage waste-water drain masts (4DU and 14DU), ensuring total aircraft dispatch readiness in cold-weather and icing conditions.
Professional Technical Capability & Instant PDF Delivery
Carrying the correct OEM technical documentation is vital for ensuring aviation safety, structural integrity, and strict airworthiness compliance. The Airbus A318 A319 A320 A321 Aircraft Maintenance Manual – Chapter 30 Ice and Rain Protection equips licensed aircraft maintenance technicians, avionics specialists, base maintenance supervisors, and flight operations personnel with the precise instructions required to diagnose faults, replace line-replaceable units (LRUs), perform leak checks, and execute MMEL deactivations safely. Utilizing genuine maintenance specifications prevents accidental pneumatic duct blowouts, avoids expensive slat thermal deformation, and guarantees proper rigging of telescopic joints and flight control interlocks.
Delivered as an instant high-resolution PDF download immediately following purchase, this manual requires no waiting for physical media. It can be accessed on demanding ramp environments, line stations, or workshop tablets, laptops, and desktop computers, and is fully printable for inclusion in physical maintenance work orders and task sign-off packets.
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