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ATR 42-300
Aircraft Handling Manual
ATR 42-300
AIRCRAFT HANDLING MANUAL
TABLE OF CONTENT
1.2 Exterior dimensions
1.3 Ground clearance
2.2 Standardized
5. Form

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Summary of Contents for ATR 42-300

  • Page 1: Table Of Contents

    ATR 42-300 Aircraft Handling Manual ATR 42-300 AIRCRAFT HANDLING MANUAL TABLE OF CONTENT 1. General 1.1 List of aircraft 1.2 Exterior dimensions 1.3 Ground clearance 1.4 Weight and balance definitions 2. Aircraft limitations and features 2.1 Certificate limitations 2.1.1 Aircraft gross weight limitations 2.1.2 Performance operating weight...
  • Page 2: General

    ATR 42-300 AIRCRAFT HANDLING MANUAL GENERAL GENERAL 1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft Model Registration number Configuration ATR 42 LY-ETM Cargo...
  • Page 3: Weight And Balance Definitions

    ATR 42-300 AIRCRAFT HANDLING MANUAL GENERAL 1.2 WEIGHT AND BALANCE DEFINITION BASIC WEIGHT Aircraft weight including the furnishing fixed equipment. DRY OPERATING WEIGHT Basic weight plus crew. Operational items (such as ballast fuel, stretcher …, if applied). (DOW) DEADLOAD Gross weight of the cargo, mail, baggage and empty ULDs.
  • Page 4 ATR 42-300 AIRCRAFT HANDLING MANUAL GENERAL %MAC (Percentage of Mean The location of the aircraft CG relative to Aerodynamic Chord) the leading edge of mean aerodynamic chord (MAC) Index The parameter used to express the variation or location of CG which is the shortened moment of a...
  • Page 5: Aircraft Limitations And Features

    ATR 42-300 AIRCRAFT HANDLING MANUAL GENERAL Ballast fuel The fuel in lieu of payload which is specifically loaded for longitudinal balance control. Usable fuel Fuel available for aircraft propulsion. Unusable fuel Fuel can not be used to technical limitations and must be included in weight and balance concerns.
  • Page 6 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES 2.2 STANDARDIZED WEIGHT AND INDEX FUEL CARGO KG INDEX A INDEX B INDEX C INDEX D INDEX E INDEX F INDEX 0-50 0-600 51-100 601-1000 101-150 1001-1400 151-200 1401-1800 201-250 1801-2200...
  • Page 7 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Config. Configuration Info A/C REG Mass Kg Index Aircraft prepared for Cargo- services. Crew 2/0. LY-ETM 10291 For additional crew see B. For additional crew: Index Observer seat Kg/Index -5.0 Version vs. max...
  • Page 8 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES 2.3 STANDARDIZED WEIGHT PER CREW Standard weight Charter Specification Definition of age (KG) flight Crew Cockpit crew...
  • Page 9: Aircraft Servicing

    Issue the new loadsheet when change in fuel figures ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING AIRCRAFT SERVICING 3.1 ARRANGEMENT OF GROUND HANDLING EQUIPMENT This diagram shows an example of the arrangement of ground handling equipment for the ATR 42- 300 aircraft:...
  • Page 10 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 3.2 SERVICING POINTS This diagram shows the locations of the servicing points of the ATR 42-300 aircraft from a top view: NOTE A: Air conditioning E: Electrical F: Fuel H: Hydraulic O: Oil Engine...
  • Page 11 The specification of the DC GPU for ATR 42 requires the ground unit to be able to provide a steady current of 300 to 400 Amp under 28 volts to insure correct functioning of all electrical services prior to startup.
  • Page 12 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING CAUTIONS : When using a mobile GPU, check voltage and frequency to be within limits. Voltage below or above specified limits may cause damage to aircraft electrical equipment. A mobile GPU must never be left connected to a tractor when the GPU power cable is connected to an aircraft.
  • Page 13 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 2 – DC Power not used light (white): is on when DC external power is connected to the aircraft, and DC external power contactor is opened. 3 – Interphone Jack: used by ground mechanic to connect a headset to communicate with crew.
  • Page 14 1 – EXT PWR pushbutton: AVAIL illuminates green when conditions of DC external power connection are met allows to connect DC external power ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 3.3.1 CONNECTING EXTERNAL POWER, FLIGHT DECK MANNED Before connecting external power, according to the procedure below, you must be aware of the WARNINGS and CAUTIONS as described in 3.3 EXTERNAL POWER.
  • Page 15 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 3.3.3 CONNECTING EXTERNAL POWER, FLIGHT DECK UNMANNED Before connecting external power, according to the procedure below, you must be aware of the WARNINGS and CAUTIONS as described in 3.3 EXTERNAL POWER. Follow these steps to connect external power to the aircraft: Externally.
  • Page 16 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 3.5 AIRCRAFT DOORS 3.5.1 REAR DOOR (left side) Rear door is an outward opening, non plug type door with a net opening of 64 cm (25 in) wide (without hand-rail(s)) and 1.73 m (68 in) high.
  • Page 17 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 3.5.2 CREW ENTRY DOOR The Crew Entry door is located on the left side of the fuselage and it is embedded in the Large Cargo Door. The Crew Entry door is outward opening non plug type door with a net opening of 944 mm (24 in) wide and 1889 mm (48 in) high.
  • Page 18 The service door is an outward opening, non plug type door with a net opening of 69 cm (27”) wide and 1.27 m (50”) high. Opened position is forward. This door is blocked closed and can be operated for maintenance purpose only. ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING 3.5.4 INTERNAL DOORS...
  • Page 19 3.5.5 LARGE CARGO DOOR The large cargo door is an outward opening, non plug type door hinged at its upper edge giving a net clear opening of 2946 mm (116 in) wide by 1803 mm (71 in) high and with a max opening angle of 110°. Door actuation system...
  • Page 20 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING...
  • Page 21 ATR 42-300 AIRCRAFT HANDLING MANUAL AIRCRAFT SERVICING...
  • Page 22: Loading

    ATR 42-300 AIRCRAFT HANDLING MANUAL LOADING LOADING 4.1 CARGO COMPARTMENT The cargo compartment extends from the cockpit partition 45.44 feet to the aft pressure bulkhead. The cargo compartment is designed to load one 88 inch wide by 54 inch pallet and three 88 inch wide by 108 inch long pallets with a maximum localized load height of 64 inches and a maximum pallet side height of 55.11 inches.
  • Page 23 ATR 42-300 AIRCRAFT HANDLING MANUAL LOADING 4.2 CARGO COMPARTMENT SPECIFICATIONS 1. Cargo Compartment Height………………………………………………………………………………….68.9” Width (floor)……………………………………………………………..………………89” Length…………………………………………………………………...……………45.44” Overall Usable Cargo Volume……………………………………….……..1,533cubic feet Maximum Floor loading………………………………….……81.9 pounds per square foot 2. Door Openings Large Cargo Door……………………………………………………….116.00” x 71.00” Rear Door………………………………………………………………………..27” x 50”...
  • Page 24 When it is necessary to install the forward transverse crash net at its forward limit (STA 6620), port and starboard attachment points must be translated for the same length respect to the forward limit. ATR 42-300 AIRCRAFT HANDLING MANUAL LOADING 4.4 PACKAGE SIZE DIMENSIONS...
  • Page 25 Cargo Compartment (Large Cargo Door):...
  • Page 26 ATR 42-300 AIRCRAFT HANDLING MANUAL LOADING 4.5 CARGO COMPARTMENT FLOOR CAPABILITY The dimensions, maximum available, width and height for the loads are presented in the figure 4.1. Figure 4.1...
  • Page 27 The ATR 42-300 has a “nose heavy” tendency. Because of this, no tail stand is provided for this aircraft. For the ATR 42-300 to tip on its tail during ground loading, the aircraft would have to reach 63% MAC. To protect it from tip up, stations 17319 and 19557 (compartment F), must be loaded last and completely unloaded first during any loading/unloading operation.
  • Page 28 Containerized freight volume 30.0 m³ (1,057 cu. ft) Bulk available volume 11.9 m³ (421 cu. ft) Figure 4.2 The ATR has three sections to carry one full cookie sheet in the two aft sections and 1½ cookie sheets in the forward section. 9G Bulkhead...
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  • Page 32 13 Ft 5.4 in. 4.100 m 26 Ft 6.9 in. 8.100 m 80 Ft 7.4 in. 24.572 m ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 4 of 764...
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  • Page 41 (two on each side) in order to remove the doors in case of emergency. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
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  • Page 45 (two on each side) in order to remove the doors in case of emergency. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
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  • Page 50 Is ON when all door hooks and latch locks are fully engaged. Note : The door can be locked and latched only from outside. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 22 of 764...
  • Page 51 A machined door with a net opening of 17.5 cm (7") wide and 15 cm (6") high is located immediately below the CAPT side window. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 23 of 764...
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  • Page 61 One light is provided in the toilet, illuminating when associated door is locked. Note : Emergency flash lights are provided (see 1.07). Mod : 5067 or 5171 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 33 of 764...
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  • Page 63 Illuminates amber when the emergency light system is deactivated. Light illuminate blue when associated switch is selected ON. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 35 of 764...
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  • Page 65 The blue it is extinguished. Light illuminate blue when associated switch is selected ON. Mod : 1547 + 1548 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 37 of 764...
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  • Page 78 AviationLearning.net 1.03 PNEUMATIC SYSTEM MAY 98 20.1 DESCRIPTION (See schematic p 7/8) Compressed air is bled from the engine compressors at the LP or HP stages. The pneumatic system consists of all the systems designed to supply air to the various aircraft systems, zones or engines, with associated control, monitoring and indicating components.
  • Page 79 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 51 of 764...
  • Page 80 AviationLearning.net 1.03 PNEUMATIC SYSTEM MAY 98 20.1 DESCRIPTION (See schematic p 7/8) Compressed air is bled from the engine compressors at the LP or HP stages. The pneumatic system consists of all the systems designed to supply air to the various aircraft systems, zones or engines, with associated control, monitoring and indicating components.
  • Page 81 Note : In case of OVHT, the associated bleed system may be recovered after a cooling time. Mod : 4584 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 53 of 764...
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  • Page 84 X VALVE OPEN light The light illuminates amber when the GRD X FEED valve is open. Mod : 4584 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 56 of 764...
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  • Page 88 - Bleed air leak (Loop u 153°C/307°F). D See BLEED LEAK procedure in chapter 2.05.08 Mod : 4584 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 60 of 764...
  • Page 89 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 61 of 764...
  • Page 90 AviationLearning.net 1.03 P 7/8 PNEUMATIC SYSTEM NOV 99 20.5 SCHEMATIC ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 62 of 764...
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  • Page 95 The toilet is ventilated by differential pressure through a vent line. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 67 of 764...
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  • Page 99 The toilet is ventilated by differential pressure through a vent line. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 71 of 764...
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  • Page 111 (On lateral panel) Isolating valves DC ESS BUS (CAB VENT) (on lateral panel) R Mod : 4273 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 83 of 764...
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  • Page 115 (on lateral panel COMPT and DUCT TEMP IND) Isolating valves DC ESS BUS (CAB VENT) (on lateral panel) Mod : 4273 ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 87 of 764...
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  • Page 137 AviationLearning.net 1.03 PNEUMATIC SYSTEM MAY 98 20.1 DESCRIPTION (See schematic p 7/8) Compressed air is bled from the engine compressors at the LP or HP stages. The pneumatic system consists of all the systems designed to supply air to the various aircraft systems, zones or engines, with associated control, monitoring and indicating components.
  • Page 138 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 110 of 764...
  • Page 139 AviationLearning.net 1.03 PNEUMATIC SYSTEM MAY 98 20.1 DESCRIPTION (See schematic p 7/8) Compressed air is bled from the engine compressors at the LP or HP stages. The pneumatic system consists of all the systems designed to supply air to the various aircraft systems, zones or engines, with associated control, monitoring and indicating components.
  • Page 140 Note : In case of OVHT, the associated bleed system may be recovered after a cooling time. Mod : 4584 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 112 of 764...
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  • Page 143 X VALVE OPEN light The light illuminates amber when the GRD X FEED valve is open. Mod : 4584 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 115 of 764...
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  • Page 147 - Bleed air leak (Loop u 153°C/307°F). D See BLEED LEAK procedure in chapter 2.05.08 Mod : 4584 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 119 of 764...
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  • Page 149 AviationLearning.net 1.03 P 7/8 PNEUMATIC SYSTEM NOV 99 20.5 SCHEMATIC ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 121 of 764...
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  • Page 154 The toilet is ventilated by differential pressure through a vent line. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 126 of 764...
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  • Page 158 The toilet is ventilated by differential pressure through a vent line. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 130 of 764...
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  • Page 170 (On lateral panel) Isolating valves DC ESS BUS (CAB VENT) (on lateral panel) R Mod : 4273 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 142 of 764...
  • Page 171 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 143 of 764...
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  • Page 174 (on lateral panel COMPT and DUCT TEMP IND) Isolating valves DC ESS BUS (CAB VENT) (on lateral panel) Mod : 4273 ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 146 of 764...
  • Page 175 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 147 of 764...
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  • Page 179 AviationLearning.net 1.03 P 15/16 AIR CONDITIONING NOV 99 R Mod : 4273 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 151 of 764...
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  • Page 181 AviationLearning.net 1.03 P 15/16 AIR CONDITIONING NOV 99 Mod : 4273 ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 153 of 764...
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  • Page 207 120 seconds (cruise), STICK PUSHER FAULT amber light will come on to notify the crew that stick pusher is inhibited. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 208 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 180 of 764...
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  • Page 214 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 186 of 764...
  • Page 215 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) 20.1 DESCRIPTION 20.2 CONTROLS 20.3 OPERATION R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 187 of 764...
  • Page 216 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 188 of 764...
  • Page 217 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 189 of 764...
  • Page 218 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 190 of 764...
  • Page 219 It is controlled by a HF control box through its transceiver. R Mod : 0032 or 2267 or 4331 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 191 of 764...
  • Page 220 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 192 of 764...
  • Page 221 In case of audio control panel loss, two AUDIO SEL pbs allow to select one VHF on each side. Mod 4928 or 5007 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 222 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 194 of 764...
  • Page 223 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 195 of 764...
  • Page 224 Generated by GPWS (refer to chapter 1.15) Generated by TCAS (when installed, refer to 1.05.20) Mod : 5017 or 5018 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 196 of 764...
  • Page 225 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 197 of 764...
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  • Page 227 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 199 of 764...
  • Page 228 - MEM : successive actions cycle the six memory channels through the display. Mod 0043 + (4928 or 5007) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 200 of 764...
  • Page 229 124.990 , 128.390 , 128.400 , 129.990 and 134.990 without disturb emission and reception. Mod 0043 + (4928 or 5007) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 201 of 764...
  • Page 230 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 202 of 764...
  • Page 231 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 203 of 764...
  • Page 232 Selects either of two transponders that may be controlled by the control box. Mod. : 0043 + 4497 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 204 of 764...
  • Page 233 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 205 of 764...
  • Page 234 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 206 of 764...
  • Page 235 Aircraft on ground (and electrically supplied), when the emergency beacon is triggered after 30 seconds, the mechanical horn is triggered too. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 236 Note : On the affected side PA, interphone and other VHF can not be used any longer. CALLS PB(s) See 1.05.10 p 3 Mod : 5017 or 5018 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 208 of 764...
  • Page 237 Aircraft on ground (and electrically supplied), when the emergency beacon is triggered after 30 seconds, the mechanical horn is triggered too. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 238 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 210 of 764...
  • Page 239 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 211 of 764...
  • Page 240 : * Pulled out : selects modes (TEL SUP CAR or TEL PLT CAR) in case of ITU channel selection. R Mod : 0032 or 2267 or 4331 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 212 of 764...
  • Page 241 R Mod : 0032 or 2267 or 4331 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 213 of 764...
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  • Page 248 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 220 of 764...
  • Page 249 A target that has satisfied the TCAS threat detection logic and thus requires a traffic advisory. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 221 of 764...
  • Page 250 Information given to the pilot pertaining to the position of another aircraft in the immediate vicinity. The information contains no resolution information. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 222 of 764...
  • Page 251 - The mode S ATC transponder will not function during some portion of the self-test sequence. R Mod : 0043 + (3832 or 8259) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 223 of 764...
  • Page 252 R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 224 of 764...
  • Page 253 - The mode S ATC transponder will not function during some portion of the self-test sequence. R Mod : 0043 + (3832 or 8259) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 225 of 764...
  • Page 254 Mod : (3832 or 8259) + 5146 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 226 of 764...
  • Page 255 - below 1100 ft AGL when aircraft is climbing. - below 900 ft AGL when aircraft is descending. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 227 of 764...
  • Page 256 RA. In this case, the RA will terminate without a CLEAR OF CONFLICT" annunciation. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 228 of 764...
  • Page 257 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 229 of 764...
  • Page 258 Two seperate networks (left and right) run individually and can be connected in case of generation failure thanks to bus tie contactors (BTC). ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 259 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 231 of 764...
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  • Page 262 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 234 of 764...
  • Page 263 * When DC STBY BUS reaches undervoltage (amber UNDV light comes ON), this bus may be recovered by selecting OVERRIDE pb. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 264 In both cases, the BUS TIE CONTACTOR closes and affected DC BUS is automatically supplied form the remaining generator. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 236 of 764...
  • Page 265 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 237 of 764...
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  • Page 269 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 241 of 764...
  • Page 270 - One UTLY BUS automatically shed after a source overload D See SVCE and UTLY BUS SHED procedure in chapter 2.05.04 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 271 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 243 of 764...
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  • Page 278 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 250 of 764...
  • Page 279 Note : Two AC electrical networks are supplied by the inverters : 115 VAC and 26 VAC. Only one is shown on the schematics. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 280 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 252 of 764...
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  • Page 293 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 265 of 764...
  • Page 294 - F/O PANELS - NAVIGATION (Back-up DC SVCE BUS) - ANNUNCIATOR LT TEST - BEACON (Back-up DC SVCE BUS) ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 266 of 764...
  • Page 295 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 267 of 764...
  • Page 296 - F/O PANELS - NAVIGATION (Back-up DC SVCE BUS) - ANNUNCIATOR LT TEST - BEACON (Back-up DC SVCE BUS) ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 268 of 764...
  • Page 297 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 269 of 764...
  • Page 298 INDICATING/RE - F/O CLOCK CORDING - MFC 2B (Primary) LANDING GEAR - WOW 2 CTL Secondary IND ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 270 of 764...
  • Page 299 - FUEL CLOG IND 2 - EEC 2 (Normal) - IDLE GATE FAIL IND - Press, Temp IND 2 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 271 of 764...
  • Page 300 INDICATING/RE - F/O CLOCK CORDING - MFC 2B (Primary) LANDING GEAR - WOW 2 CTL Secondary IND ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 272 of 764...
  • Page 301 - FUEL CLOG IND 2 - EEC 2 (Normal) - IDLE GATE FAIL IND - Press, Temp IND 2 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 273 of 764...
  • Page 302 (Back up DC ESS BUS SECT 1) NAVIGATION - STBY HORIZON Back up - ADC 1 Back up - ADC 2 Back up ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 274 of 764...
  • Page 303 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 275 of 764...
  • Page 304 - WING, EMPENNAGE BOOTS B and ENG 2 BOOTS A and B (Back-up DC BUS 2) - HORNS ANTI-ICING IND and CTL ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 276 of 764...
  • Page 305 (Back-up - DC BUS 1) - DC BUS 2) ENGINE CTL - CL FIRE IND 1 and 2 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 277 of 764...
  • Page 306 BOOTS A and B (Back-up DC BUS 2) - HORNS ANTI-ICING IND and CTL Mod : 4372 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 278 of 764...
  • Page 307: Lights

    (Back-up - DC BUS 1) - DC BUS 2) ENGINE CTL - CL FIRE IND 1 and 2 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 279 of 764...
  • Page 308 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 280 of 764...
  • Page 309 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 281 of 764...
  • Page 310 - STARTING PUMP 1 and 2 and MOTIVE FLOW VALVES 1 and 2 R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 282 of 764...
  • Page 311 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 283 of 764...
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  • Page 313 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 285 of 764...
  • Page 314 - STARTING PUMP 1 and 2 and MOTIVE FLOW VALVES 1 and 2 R Mod : 4273 + 4372 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 286 of 764...
  • Page 315 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 287 of 764...
  • Page 316: Adf

    - VOR/ILS/MKR 1 - SGU 1 - CAPT EADI - CAPT EHSI - RMI F/O - ADF 1 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 288 of 764...
  • Page 317 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 289 of 764...
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  • Page 332 AviationLearning.net EMERGENCY EQUIPMENT 1.07 P 3/4 GENERAL DEC 95 SCHEMATICS ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 304 of 764...
  • Page 333 25 000 ft to 13 000 ft, 26 minutes to continue the flight between 13 000 ft and 10 000 ft) in addition to the cockpit crew 120 minutes consumption. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 334 (pb pressed in) Passengers supply valve is open. ON illuminates blue. (pb released) Passengers supply valve is closed. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 306 of 764...
  • Page 335 25 000 ft to 13 000 ft, 26 minutes to continue the flight between 13 000 ft and 10 000 ft) in addition to the cockpit crew 120 minutes consumption. Mod : 4292 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 307 of 764...
  • Page 336 PAX SUPPLY ON" Lt A light indicator ON" illuminates white when the pax supply valve is open. Mod. : 4292 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 308 of 764...
  • Page 337 Note : If the pilot wishes to use the oxygen mask again and recover the mask micro, it just has to open the container doors. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 338 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 310 of 764...
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  • Page 341 AviationLearning.net EMERGENCY EQUIPMENT 1.07 P 7/8 OXYGEN SYSTEM NOV 97 20.4 SCHEMATICS Mod. : 4292 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 313 of 764...
  • Page 342 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 314 of 764...
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  • Page 347 SERVICE DOOR PASSENGER/CREW DOOR Note : Be sure that safety pin is removed. Mod. : 4019 + 4358 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 319 of 764...
  • Page 348 SERVICE DOOR PASSENGER/CREW DOOR Note : Be sure that safety pin is removed. Mod. : 4019 + 4358 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 320 of 764...
  • Page 349 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 321 of 764...
  • Page 350 Toilets are equipped wih one photoelectric smoke detector. In case of smoke detection, SMOKE" signal is sent to CCAS through the MFC. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 351 TOILETS WASTE BIN FIRE EXTINGUISHING SYSTEM The system operates automatically when fire is detected (when the temperature is greater than 78°C (172°F). ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 323 of 764...
  • Page 352 In case of smoke detection, a signal is sent to the CCAS . FWD SMK and AFT SMK red alerts are triggered on CAP. Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 324 of 764...
  • Page 353 TOILETS WASTE BIN FIRE EXTINGUISHING SYSTEM The system operates automatically when fire is detected (when the temperature is greater than 78°C (172°F). ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 325 of 764...
  • Page 354 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 326 of 764...
  • Page 355 Illuminates red in case of fire signal from associated engine. Extinguishes after CL is set at fuel shut off position or if fire detection signal terminates. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 356 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 328 of 764...
  • Page 357 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 329 of 764...
  • Page 358 SMK TEST pb Allows to test the 4 specific container smoke detectors working. R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 330 of 764...
  • Page 359 CONTAINER SMK local alert on overhead panel. PAX CONFIGURATION (CNTNR SMK pb is released) R Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 331 of 764...
  • Page 360 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 332 of 764...
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  • Page 362 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 334 of 764...
  • Page 363 - Smoke detected in the cargo bay (containers transportation only) • See CARGO BAY SMOKE" procedure in chapter 2.04.03. Mod : 4273 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 335 of 764...
  • Page 364 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 336 of 764...
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  • Page 369 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 341 of 764...
  • Page 370 LH aileron trim controlled tab travel : 6.7° up, 6.7° down. Full roll trim travel requires about 15s. Mod : 4372 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 342 of 764...
  • Page 371 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 343 of 764...
  • Page 372 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 344 of 764...
  • Page 373 In case of pitch uncoupling when the pusher triggering angle of attack is reached, only the captain control column is pushed forward. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 345 of 764...
  • Page 374 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 346 of 764...
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  • Page 386 Note : If EXT flag appears when flaps are extended, it means that there is a leak in the flaps hydraulic circuit. FLAP ASYM It Illuminates amber when flaps asymmetry exceeds 6,7°. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 358 of 764...
  • Page 387 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 359 of 764...
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  • Page 396 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 368 of 764...
  • Page 397 - Selection of STEEP APP" function. (It is impossible to select both functions at the same time). Mod. : 5262 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 369 of 764...
  • Page 398 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 370 of 764...
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  • Page 404 . "FLT CTL" amber light illuminates on CAP . Aural alert is Continuous Repetitive Chime (CRC) Mod : 4372 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 376 of 764...
  • Page 405 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 377 of 764...
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  • Page 408 These supply raw data directly to the standby airspeed ind. and the standby altimeter. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 380 of 764...
  • Page 409 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 381 of 764...
  • Page 410 Standby airspeed ind. and standby altimeter are directly supplied by raw data. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 411 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 383 of 764...
  • Page 412 These supply raw data directly to the standby airspeed ind. and the standby altimeter. R Mod : (3832 or 8259) + (3952 or 4890 or 5021 or 5022) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 413 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 385 of 764...
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  • Page 416 Note : Allowable deviation between normal altimeter indications and between normal and standby altimeter indications : FL (ft) NORM/NORM (ft) NORM/STBY (ft) 5.000 10.000 20.000 25.000 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 388 of 764...
  • Page 417 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 389 of 764...
  • Page 418 Note : Allowable deviation between normal altimeter indications and between normal and standby altimeter indications : FL (ft) NORM/NORM (ft) NORM/STBY (ft) 5.000 10.000 20.000 25.000 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 390 of 764...
  • Page 419 AviationLearning.net NOV 01 R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 391 of 764...
  • Page 420 Note : Allowable deviation between normal altimeter indications and between normal and standby altimeter indications : FL (ft) NORM/NORM (ft) NORM/STBY (ft) 5.000 10.000 20.000 25.000 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 392 of 764...
  • Page 421 - In that case, the vertical speed pointer disappears when V/S flag appears. Test When depressed, indicator will display a test pattern. Light sensort Not available Mod : 4541 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 393 of 764...
  • Page 422 AviationLearning.net NOV 01 R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 394 of 764...
  • Page 423 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 395 of 764...
  • Page 424 See ADC FAULT procedure in chapter 2.05.12. - Incorrect ADC switching • See ADC SW FAULT procedure in chapter 2.05.12. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 396 of 764...
  • Page 425 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 397 of 764...
  • Page 426 FLIGHT INSTRUMENTS 1.10 P 9/10 AIR DATA SYSTEM NOV 01 10.4 SCHEMATIC R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 398 of 764...
  • Page 427 AviationLearning.net NOV 00 Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 399 of 764...
  • Page 428 NOV 01 10.4 SCHEMATIC R Mod : (3832 or 8259) + (3952 or 4890 or 5021 or 5022) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 400 of 764...
  • Page 429 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 401 of 764...
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  • Page 435 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 407 of 764...
  • Page 436 Range of readable radio-altitude is from - 20 ft to 2500 ft. Above 2500 ft, radio altitude information is not displayed. See chapter 1.15.30. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 437 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 409 of 764...
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  • Page 443 To select green bearing pointer to VOR 2 or to ADF 2. On OFF position, green pointer disappears from EHSI. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 415 of 764...
  • Page 444 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 416 of 764...
  • Page 445 Note : RNV2 position is inoperative when MAP display is active. Refer to 1.15.60. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 417 of 764...
  • Page 446 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 418 of 764...
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  • Page 453 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 425 of 764...
  • Page 454 - the DFDR or QAR (if installed) electrical power is lost. - QAR (if installed) 80 % full. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 426 of 764...
  • Page 455 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 427 of 764...
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  • Page 463 Note : All the digits (on the FU counter as well as on the FUEL QTY ind.) may be tested by the overhead panel ANN LIGHT switch on TEST position. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 464 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 436 of 764...
  • Page 465 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 437 of 764...
  • Page 466 Green sector : 0ºC to 50ºC Yellow sector : 50ºc to 57ºC Red dash : -54ºC and +57ºC ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 438 of 764...
  • Page 467 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 439 of 764...
  • Page 468 Green sector : 0ºC to 50ºC Yellow sector : 50ºc to 57ºC Red dash : -54ºC and +57ºC ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 440 of 764...
  • Page 469 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 441 of 764...
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  • Page 476 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 448 of 764...
  • Page 477 The It illuminates amber and the CCAS is activated when associated tank compartment fluid quantity drops below 2.5 l (0.67 US gal). The X FEED automatically closes. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 449 of 764...
  • Page 478 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 450 of 764...
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  • Page 487 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 459 of 764...
  • Page 488 OFF. In this case, stall alarm threshold recovers the values defined for flight in normal conditions. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 489 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 461 of 764...
  • Page 490 OFF. In this case, stall alarm threshold recovers the values defined for flight in normal conditions. Mod : 5008 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 462 of 764...
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  • Page 493 Note : When de icing OVRD mode is selected, boots inflate according to a separate timer and MFC is totally by passed. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 494 - Associated distribution valve output has been controlled closed but a downstream pressure is detected. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 466 of 764...
  • Page 495 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 467 of 764...
  • Page 496 - Associated distribution valve output has been controlled closed but a downstream pressure is detected. Mod. : 1742 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 468 of 764...
  • Page 497 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 469 of 764...
  • Page 498 (pb pressed in) The DE-ICING MODE SEL pb (4) is operative and allows the crew to select the appropriate timing cycle depending on SAT. MAN illuminates white. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 470 of 764...
  • Page 499 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 471 of 764...
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  • Page 501 B(A) are not supplied 20 sec after eng. cycle beginning. • See DE ICING MODE SEL FAULT procedure in chapter 2.05.09 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 473 of 764...
  • Page 502 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 474 of 764...
  • Page 503 B(A) are not supplied 20 sec after eng. cycle beginning. • See DE ICING MODE SEL FAULT procedure in chapter 2.05.09. Mod : 1742 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 475 of 764...
  • Page 504 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 476 of 764...
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  • Page 510 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 482 of 764...
  • Page 511 (pb pressed in) The ANTI-ICING MODE SEL pb (2) is operative and allows the crew to select the appropriate timing cycle depending on SAT. MAN illuminates white. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 483 of 764...
  • Page 512 - MFC 1B or 2B and/or ADC failure, discrepancy between outputs. SSee MODE SEL AUTO FAULT procedure in chapter 2.05.09. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 484 of 764...
  • Page 513 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 485 of 764...
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  • Page 518 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 490 of 764...
  • Page 519 Captain wiper DC ESS BUS (on lateral panel CAPT) F/O wiper DC BUS 2 (on lateral panel F/O ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 491 of 764...
  • Page 520 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 492 of 764...
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  • Page 532 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 504 of 764...
  • Page 533 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 505 of 764...
  • Page 534 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 506 of 764...
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  • Page 536 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 508 of 764...
  • Page 537 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 509 of 764...
  • Page 538 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 510 of 764...
  • Page 539 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 511 of 764...
  • Page 540 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 512 of 764...
  • Page 541 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 513 of 764...
  • Page 542 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 514 of 764...
  • Page 543 WEIGHT AND LOADING 2.01.03 AIRSPEED AND OPERATIONAL PARAMETERS 2.01.04 POWER PLANT 2.01.05 SYSTEMS 2.01.06 TCAS 2.01.07 2.01.08 CABIN LIGHTING ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 515 of 764...
  • Page 544 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 516 of 764...
  • Page 545 For dispatch in the event of equipment failure or missing equipment refer to MEL/CDL. MAXIMUM NUMBER OF PASSENGER SEATS ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 517 of 764...
  • Page 546 The distance from station 0 to reference chord leading edge is 11.425 meters (449.803 in). CARGO COMPARTMENT LOADING LIMITATIONS See W.B.M. : 1.10.04 p 1 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 518 of 764...
  • Page 547 The distance from station 0 to reference chord leading edge is 11.425 meters (449.803 in.). CARGO COMPARTMENT LOADING LIMITATIONS See W.B.M. : 1.10.04 p 1 R Mod : 5150 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 519 of 764...
  • Page 548 The distance from station 0 to reference chord leading edge is 11.425 meters (449.803 in.). CARGO COMPARTMENT LOADING LIMITATIONS See W.B.M. : 1.10.04 p 1 Mod : 5150 + 5175 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 520 of 764...
  • Page 549 The distance from station 0 to reference chord leading edge is 11.425 meters (449.803 in). CARGO COMPARTMENT LOADING LIMITATIONS See W.B.M. : 1.10.04 p 1 ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 521 of 764...
  • Page 550 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 522 of 764...
  • Page 551 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 523 of 764...
  • Page 552 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 524 of 764...
  • Page 553 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 525 of 764...
  • Page 554 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 526 of 764...
  • Page 555 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 527 of 764...
  • Page 556 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 528 of 764...
  • Page 557 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 529 of 764...
  • Page 558 CAUTION : INCREASE BY 1.5 KT FOR TAKE-OFF BLEED ON –40 –30 –20 OUTSIDE AIR TEMPERATURE (DG.C) Eng. : PW127E ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 530 of 764...
  • Page 559 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 531 of 764...
  • Page 560 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 532 of 764...
  • Page 561 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 533 of 764...
  • Page 562 The maximum demonstrated cross wind on dry runway is 30 KT. MAXIMUM MEAN RUNWAY SLOPE : ± 2 % ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 534 of 764...
  • Page 563 Note : Flight with an engine running and the propeller feathered is not permitted. Eng. : PW127E ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 535 of 764...
  • Page 564 AviationLearning.net LIMITATIONS 2.01 POWER PLANT MAY 98 Eng. : PW127E ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 536 of 764...
  • Page 565 Note : Flight with an engine running and the propeller feathered is not permitted. Eng. : PW121A ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 537 of 764...
  • Page 566 AviationLearning.net LIMITATIONS 2.01 POWER PLANT MAY 98 Eng. : PW121A ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 538 of 764...
  • Page 567 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 539 of 764...
  • Page 568 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 540 of 764...
  • Page 569 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 541 of 764...
  • Page 570 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 542 of 764...
  • Page 571 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 543 of 764...
  • Page 572 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 544 of 764...
  • Page 573 BRAKED WHEELS EXCEPT IN CASE OF EMERGENCY TAKE OFF WITH MORE THAN ONE FAILED MFC MODULE IS PROHIBITED. ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 545 of 764...
  • Page 574 Provision is made to cover : - unusuable quantity - normal system leakage - Ref. Temp errors ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 546 of 764...
  • Page 575 BRAKED WHEELS EXCEPT IN CASE OF EMERGENCY TAKE OFF WITH MORE THAN ONE FAILED MFC MODULE IS PROHIBITED. ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 547 of 764...
  • Page 576 Provision is made to cover : - unusuable quantity - normal system leakage - Ref. Temp errors Mod. : 4292 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 548 of 764...
  • Page 577 BRAKED WHEELS EXCEPT IN CASE OF EMERGENCY TAKE OFF WITH MORE THAN ONE FAILED MFC MODULE IS PROHIBITED. ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 549 of 764...
  • Page 578 Provision is made to cover : - unusuable quantity - normal system leakage - Ref. Temp errors ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 550 of 764...
  • Page 579 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 551 of 764...
  • Page 580 AviationLearning.net LIMITATIONS 2.01 TCAS NOV 98 LEFT INTENTIONALLY BLANK ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 552 of 764...
  • Page 581 R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 553 of 764...
  • Page 582 RA command issued by the TCAS. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 554 of 764...
  • Page 583 6000 ft - Approach and landing 7000 ft Wings Level Assumed R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 555 of 764...
  • Page 584 Maneuvers based solely on information displayed on the traffic display are not authorized. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 556 of 764...
  • Page 585 -Errors or differences between independant air data sources PERFORMANCES The performances in Part 3 are applicable. R Mod : 3832 or 8259 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 557 of 764...
  • Page 586 -Errors or differences between independant air data sources PERFORMANCES The performances in Part 3 are applicable. Mod : (3832 or 8259) + 5205 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 558 of 764...
  • Page 587 AviationLearning.net LIMITATIONS 2.01 GLOBAL POSITIONING SYSTEM NOV 98 LEFT INTENTIONALLY BLANK ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 559 of 764...
  • Page 588 If RAIM warning appears, navigation must be crosschecked with usual means. Data base updating must be verified before each flight. Mod : 3952 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 560 of 764...
  • Page 589 AviationLearning.net LIMITATIONS 2.01 GLOBAL POSITIONING SYSTEM NOV 99 LEFT INTENTIONALLY BLANK Mod : 4597 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 561 of 764...
  • Page 590 Such an authorization must be obtained by the operator from the appropriate authorities. Mod. : 4654 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 562 of 764...
  • Page 591 GPS navigation capability. Mod. : 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 563 of 764...
  • Page 592 GPS navigation capability. R Mod. : (4654 + 4885) or 5020 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 564 of 764...
  • Page 593 GPS navigation capability. Mod. : 5176 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 565 of 764...
  • Page 594 GPS navigation capability. Mod. : (4890 + 5022) or 5021 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 566 of 764...
  • Page 595 AviationLearning.net LIMITATIONS 2.01 CABIN LIGHTING NOV 99 CABIN LIGHTING NOT APPLICABLE ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 567 of 764...
  • Page 596 The general cabin illumination system must be used during not less than 15 minutes before each flight. Mod : 5067 or 5171 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 568 of 764...
  • Page 597 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 569 of 764...
  • Page 598 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 570 of 764...
  • Page 599 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 571 of 764...
  • Page 600 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 572 of 764...
  • Page 601 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 573 of 764...
  • Page 602 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 574 of 764...
  • Page 603 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 575 of 764...
  • Page 604 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 576 of 764...
  • Page 605 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 577 of 764...
  • Page 606 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 578 of 764...
  • Page 607 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 579 of 764...
  • Page 608 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 580 of 764...
  • Page 609 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 581 of 764...
  • Page 610 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 582 of 764...
  • Page 611 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 583 of 764...
  • Page 612 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 584 of 764...
  • Page 613 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 585 of 764...
  • Page 614 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 586 of 764...
  • Page 615 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 587 of 764...
  • Page 616 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 588 of 764...
  • Page 617 DOB CD HOOKS ENGAGED MAINT IND DOB CD LATLK LKD MAINT IND DOB CD HOOKS DISENG MAINT IND F F F ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 589 of 764...
  • Page 618 AviationLearning.net 1.01 P 13 GENERAL NOV 01 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 590 of 764...
  • Page 619 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 591 of 764...
  • Page 620 AviationLearning.net 1.01 P 13 GENERAL NOV 01 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 592 of 764...
  • Page 621 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 593 of 764...
  • Page 622 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 594 of 764...
  • Page 623 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 595 of 764...
  • Page 624 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 596 of 764...
  • Page 625 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 597 of 764...
  • Page 626 60.2 CONTROLS 60.3 ELECTRICAL SUPPLY 60.4 SCHEMATIC R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 598 of 764...
  • Page 627 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 599 of 764...
  • Page 628 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 600 of 764...
  • Page 629 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 601 of 764...
  • Page 630 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 602 of 764...
  • Page 631 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 603 of 764...
  • Page 632 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 604 of 764...
  • Page 633 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 605 of 764...
  • Page 634 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 606 of 764...
  • Page 635 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 607 of 764...
  • Page 636 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 608 of 764...
  • Page 637 (on overhead panel ADF 1) ADF 2 (if installed) DC BUS 2 (on overhead panel ADF 2) ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 609 of 764...
  • Page 638 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 610 of 764...
  • Page 639 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 611 of 764...
  • Page 640 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 612 of 764...
  • Page 641 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 613 of 764...
  • Page 642 The system can be tested on ground and in flight above 1000 ft radio height by pressing one of the GPWS/GS lt. R Mod. : (4403 + 4404) or 5262 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 614 of 764...
  • Page 643 "TERRAIN-TERRAIN" aural message is heard until the aircraft pressure altitude has increased by 300 ft of altitude. R Mod. : (4403 + 4404) or 5262 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 615 of 764...
  • Page 644 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 616 of 764...
  • Page 645 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 617 of 764...
  • Page 646 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 618 of 764...
  • Page 647 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 619 of 764...
  • Page 648 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 620 of 764...
  • Page 649 STEEP APP PB Modifies the SINK RATE envelope, illuminates blue when pressed in. Mod. : 4403 + 4404 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 621 of 764...
  • Page 650 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 622 of 764...
  • Page 651 Each time the STEEP APP" pb is selected, the LDG FLAP 25" pb is released if already selected. It is impossible to select both functions at the same time. Mod. : 5262 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 623 of 764...
  • Page 652 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 624 of 764...
  • Page 653 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 625 of 764...
  • Page 654 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 626 of 764...
  • Page 655 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 627 of 764...
  • Page 656 System is controlled with the weather radar control panel. Modes selected on this panel are displayed on the EHSI. Mod : 5016 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 628 of 764...
  • Page 657 TST position : (TEST displayed on the EFIS) displays a test pattern to verify the system. Mod : 5016 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 629 of 764...
  • Page 658 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 630 of 764...
  • Page 659 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 631 of 764...
  • Page 660 Is used to select either the normal 12 looks/mn 120 scan or the faster update 24 looks/mn 60 sector scan. Mod : 5016 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 632 of 764...
  • Page 661 Appears as soon as ARC mode is selected on EHSI. Weather indication Is displayed in four colors. Mod : 5016 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 633 of 764...
  • Page 662 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 634 of 764...
  • Page 663 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 635 of 764...
  • Page 664 AviationLearning.net NAVIGATION SYSTEM 1.15 WEATHER RADAR NOV 99 LEFT INTENTIONALLY BLANK Mod : 5016 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 636 of 764...
  • Page 665 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 637 of 764...
  • Page 666 AviationLearning.net NAVIGATION SYSTEM 1.15 GLOBAL POSITIONING SYSTEM NOV 00 60.1 DESCRIPTION (See schematic P. 11/12) Using information provided by a constellation of 24 satellites (Bendix-King KLN 90 is able to track up to 8 satellites at a time), GPS is an automatic tridimensional (latitude, longitude, altitude) location and navigation means (KLN 90 is set for KLN 90A(s) or KLN 90B(s) depending on installed version).
  • Page 667 AviationLearning.net NAVIGATION SYSTEM 1.15 GLOBAL POSITIONING SYSTEM NOV 00 60.2 CONTROLS KLN 90 CONTROLS The screen is normally divided in two sides controlled by two sets of concentric knobs and two cursor buttons. Each can present a variety of information in a number of different page formats.
  • Page 668 To know all the functions available, refer to the table of contents of the HT 1000 pilot's guide. Mod : 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 640 of 764...
  • Page 669 R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 641 of 764...
  • Page 670 To know all the functions available, refer to the table of contents of the HT 1000 pilot's guide. Mod : (4654 or 4885 or 5020) + (4839 or 4656) ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 642 of 764...
  • Page 671 R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 643 of 764...
  • Page 672 To know all the functions available, refer to the table of contents of the HT 1000 pilot's guide. Mod 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 644 of 764...
  • Page 673 R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 645 of 764...
  • Page 674 Action on this pushbutton causes selection of the GPS mode. Refer to 1.10.30. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 646 of 764...
  • Page 675 ADF, an intersection or a user defined waypoint R Mod : 3952 or 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 647 of 764...
  • Page 676 Action on this pushbutton causes selection of the GPS mode. Refer to 1.10.30. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 648 of 764...
  • Page 677 ADF, an intersection or a user defined waypoint R Mod : 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 649 of 764...
  • Page 678 Action on this pushbutton causes selection of the GNSS mode. Refer to 1.10.30. R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 650 of 764...
  • Page 679 (white) f indicates an airport indicates a VOR R Mod : 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 651 of 764...
  • Page 680 Action on this pushbutton causes selection of the GNSS mode. Refer to 1.10.30. R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 652 of 764...
  • Page 681 Indicates the distance computed by GNSS to the next waypoint. Waypoints next waypoint (magenta) other waypoint (white) f indicates an airport indicates a VOR Mod : 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 653 of 764...
  • Page 682 Radar's range selector may be used to select the distance scale. R Mod : 3952 or 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 654 of 764...
  • Page 683 Lateral deviation to the track WPT alerting Illuminates amber when approaching a waypoint. TO/FROM annunciator R Mod : 3952 or 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 655 of 764...
  • Page 684 OFS (cyan) Indicates that a parallel offset has been activated. RADAR status R Mod 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 656 of 764...
  • Page 685 APP illuminates cyan when in approach phase. (Not applicable) OFS illuminates cyan when an offset has been activated. R Mod : 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 657 of 764...
  • Page 686 Radar's range selector may be used to select the distance scale. R Mod : 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 658 of 764...
  • Page 687 Lateral deviation to the track WPT alerting Illuminates amber when approaching a waypoint. TO/FROM annunciator R Mod : 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 659 of 764...
  • Page 688 OFS (cyan) Indicates that a parallel offset has been activated. RADAR status Vertical deviation Scale and index Mod 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 660 of 764...
  • Page 689 APP illuminates cyan when in approach phase. OFS illuminates cyan when an offset has been activated. Mod : 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 661 of 764...
  • Page 690 Lateral deviation to the track WPT alerting Illuminates amber when approaching a waypoint. TO/FROM annunciator R Mod : 3952 or 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 662 of 764...
  • Page 691 (RAIM = Receiver Autonomous Integrity Monitoring) FAULT illuminate amber when RAIM function is lost. Mod. : 3952 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 663 of 764...
  • Page 692 Lateral deviation to the track WPT alerting Illuminates amber when approaching a waypoint. TO/FROM annunciator R Mod : 3952 or 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 664 of 764...
  • Page 693 RNV MSG will extinguish when these cases are taken into account (MSG pb on GPS control panel). Mod. : 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 665 of 764...
  • Page 694 APP illuminates cyan when in approach phase. (Not applicable) OFS illuminates cyan when an offset has been activated. R Mod : 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 666 of 764...
  • Page 695 RNV MSG will extinguish when the associated MCDU message is cancelled. R Mod : 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 667 of 764...
  • Page 696 Lateral deviation to the track WPT alerting Illuminates amber when approaching a waypoint. TO/FROM annunciator R Mod : 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 668 of 764...
  • Page 697 RNV MSG will extinguish when these cases are taken into account (MSG pb on GPS control panel). R Mod. : 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 669 of 764...
  • Page 698 APP illuminates cyan when in approach phase. OFS illuminates cyan when an offset has been activated. Mod : 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 670 of 764...
  • Page 699 This message appears whenever the aircraft reaches the last altitude constraint on the descent path. Mod : 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 671 of 764...
  • Page 700 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 672 of 764...
  • Page 701 This jack enables to connect a computer to update the data base. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 702 DC BUS SUPPLY EQUIPMENT GNSS DC STBY BUS (on overhead panel GPS) R Mod : 4654 or 4885 or 5020 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 674 of 764...
  • Page 703 GLOBAL NAVIGATION SATELLITE SYSTEM GNSS NOV 00 LEFT INTENTIONALLY BLANK R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 675 of 764...
  • Page 704 ** In that case the crew has to use only usual means of navigation. Mod : 4890 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 676 of 764...
  • Page 705 This jack enables to connect a computer to update the data base. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 706 60.3 ELECTRICAL SUPPLY DC BUS SUPPLY EQUIPMENT GNSS DC STBY BUS (on overhead panel GPS) Mod : 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 678 of 764...
  • Page 707 GLOBAL NAVIGATION SATELLITE SYSTEM GNSS NOV 00 LEFT INTENTIONALLY BLANK R Mod : 4654 or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 679 of 764...
  • Page 708 ** In that case the crew has to use only usual means of navigation. R Mod : 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 680 of 764...
  • Page 709 This jack enables to connect a computer to update the data base. R Mod : 3952 or 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 710 AviationLearning.net NAVIGATION SYSTEM 1.15 GLOBAL POSITIONING SYSTEM P 11/12 (GPS) MAI 98 60.5 SCHEMATIC Mod. : 3952 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 682 of 764...
  • Page 711 GLOBAL NAVIGATION SATELLITE SYSTEM GNSS NOV 01 60.4 SCHEMATIC R Mod : 4654or 4885 or 5020 or 5176 ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 683 of 764...
  • Page 712 GLOBAL POSITIONING SYSTEM P 11/12 NOV 00 60.5 SCHEMATIC R Mod : 4890 or 5021 or 5022 ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 684 of 764...
  • Page 713 GLOBAL NAVIGATION SATELLITE SYSTEM GNSS NOV 01 60.4 SCHEMATIC Mod : (4654or 4885 or 5020 or 5176) + (4839 or 4656) ATR 42 Model 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 685 of 764...
  • Page 714 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 686 of 764...
  • Page 715 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 687 of 764...
  • Page 716 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 688 of 764...
  • Page 717 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 689 of 764...
  • Page 718 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 690 of 764...
  • Page 719 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 691 of 764...
  • Page 720 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 692 of 764...
  • Page 721 , that provides cooling of the lubricating system by using fuel system as cooling source. - A flow divider to the fuel nozzles. ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 693 of 764...
  • Page 722 Note : When EEC is deselected, exciters A + B can manually be activated, using the MAN IGN guarded push-button. ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 694 of 764...
  • Page 723 . to provide the HP motive flow required by the fuel tank jet pump through an engine valve - A fuel flowmeter - A flow divider to the fuel nozzles. ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 695 of 764...
  • Page 724 Note : When EEC is deselected, exciters A + B can manually be activated, using the MAN IGN guarded push-button. ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 696 of 764...
  • Page 725 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 697 of 764...
  • Page 726 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 698 of 764...
  • Page 727 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 699 of 764...
  • Page 728 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 700 of 764...
  • Page 729 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 701 of 764...
  • Page 730 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 702 of 764...
  • Page 731 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 703 of 764...
  • Page 732 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 704 of 764...
  • Page 733 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 705 of 764...
  • Page 734 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 706 of 764...
  • Page 735 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 707 of 764...
  • Page 736 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 708 of 764...
  • Page 737 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 709 of 764...
  • Page 738 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 710 of 764...
  • Page 739 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 711 of 764...
  • Page 740 Note : Operating line with EEC ON may be placed above or below the HMU BASE LAW depending on weather conditions. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 741 LINE C : CRZ1 or 2 Note : Sensible sector designed to allow fix throttle engine control ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 713 of 764...
  • Page 742 Thus, the torque which is the engine control parameter, is controlled (with PLA constant) in all ambient conditions. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 714 of 764...
  • Page 743 LINE C : CRZ Note : Sensible sector designed to allow fix throttle engine control Mod. : 4601 ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 715 of 764...
  • Page 744 Thus, the torque which is the engine control parameter, is controlled (with PLA constant) in all ambient conditions. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 716 of 764...
  • Page 745 LINE C : CLB or CRZ Note : Sensible sector designed to allow fix throttle engine control ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 717 of 764...
  • Page 746 Thus, the torque which is the engine control parameter, is controlled (with PLA constant) in all ambient conditions. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 718 of 764...
  • Page 747 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 719 of 764...
  • Page 748 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 720 of 764...
  • Page 749 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 721 of 764...
  • Page 750 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 722 of 764...
  • Page 751 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 723 of 764...
  • Page 752 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 724 of 764...
  • Page 753 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 725 of 764...
  • Page 754 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 726 of 764...
  • Page 755 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 727 of 764...
  • Page 756 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 728 of 764...
  • Page 757 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 729 of 764...
  • Page 758 CAUTION : If the engine is restarted, IT WILL BE NECESSARY TO SELECT PWR MGT to MCT position after relight in order to be able to UNFEATHER the propeller. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 730 of 764...
  • Page 759 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 731 of 764...
  • Page 760 CAUTION : If the engine is restarted, IT WILL BE NECESSARY TO SELECT PWR MGT to MCT position after relight in order to be able to UNFEATHER the propeller. ATR 42 Model : 400/500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 732 of 764...
  • Page 761 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 733 of 764...
  • Page 762 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 734 of 764...
  • Page 763 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 735 of 764...
  • Page 764 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 736 of 764...
  • Page 765 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 737 of 764...
  • Page 766 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 738 of 764...
  • Page 767 Allows to test the ind. During test, both counter and pointer will display 115 %. Note : A blue dot is provided on the ind. scale to identify 115 %. ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 768 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 740 of 764...
  • Page 769 Allows to test the ind. During test, both counter and pointer will display 115 %. Note : A blue dot is provided on the ind. scale to identify 115 %. ATR 42 Model : 400 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 770 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 742 of 764...
  • Page 771 Allows to test the ind. During test, both counter and pointer will displayed 1150°C. Note : A blue dot is provided on the ind. scale to identify 1150°C. ATR 42 Model : 500 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only...
  • Page 772 AviationLearning.net POWER PLANT 1.16 P 10 CONTROLS NOV 97 NH/NL IND Digital counter Actual NH is displayed. Pointer Actual NH is displayed. Green sector 62-102.7 % Red mark 102.7 % Pointer Actual NL is displayed. Green sector 62-104.2 % Red mark 104.2 % Test pb Allows to test the ind.
  • Page 773 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 745 of 764...
  • Page 774 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 746 of 764...
  • Page 775 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 747 of 764...
  • Page 776 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 748 of 764...
  • Page 777 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 749 of 764...
  • Page 778 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 750 of 764...
  • Page 779 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 751 of 764...
  • Page 780 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 752 of 764...
  • Page 781 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 753 of 764...
  • Page 782 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 754 of 764...
  • Page 783 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 755 of 764...
  • Page 784 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 756 of 764...
  • Page 785 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 757 of 764...
  • Page 786 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 758 of 764...
  • Page 787 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 759 of 764...
  • Page 788 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 760 of 764...
  • Page 789 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 761 of 764...
  • Page 790 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 762 of 764...
  • Page 791 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 763 of 764...
  • Page 792 AviationLearning.net 01/07//2018 REV 1 These notes are not revised after issue For Training Purposes Only Page 764 of 764...

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