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De Havilland DASH8 100 Series, Руководство по обслуживанию

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De Havilland DASH8 100 Series Скачать руководство пользователя страница 32

REFER TO INTERNAL DOCUMENT 

REFER TO INTERNAL DOCUMENT 

 

dam01_7710000_001.cgm, cg, 10/07/03

PRE MOD 8/0886

D

SERIES 100

AIRCRAFT MAINTENANCE MANUAL

TORQUE INDICATING SYSTEM

Figure 1 (Sheet 1 of 2)

MASTER
EFFECTIVITY: See Pageblock 77−10−00 page 1

77−10−00

Page 4

Dec 20/2004

Содержание DASH8 100 Series

Страница 1: ...is by means of a transmitter sensing fuel flow to the engine fuel manifold connected by electrical wiring to an indicator on the engine instrument panel Fuel temperature indicating is by means of a t...

Страница 2: ......

Страница 3: ...in the caution lights panel in the flight compartment For details of the caution lights system refer to Chapter 33 3 Operation Refer to Figure 2 The switch is provided with one contact set The switch...

Страница 4: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL FUEL LOW PRESSURE WARNING Figure 1 MASTER EFFECTIVITY See Pageblock 73 31 00 page 1 73 31 00 Page 2 Dec 20 2004...

Страница 5: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL FUEL LOW PRESSURE WARNING Figure 2 MASTER EFFECTIVITY See Pageblock 73 31 00 page 1 73 31 00 Page 3 Dec 20 2004...

Страница 6: ......

Страница 7: ...g impeller type and is connected to the associated indicator by electrical wiring B Fuel Flow Indicators Refer to Figure 2 and Figure 3 The fuel flow indicators are located on the engine instrument pa...

Страница 8: ...gital display is blanked Mod 8 1738 introduces fuel flow indicators with specification changes as follows 1 FF fuel flow of 1200 PPH 550 KG H and higher beyond indicator range shall read 1200 PPH 550...

Страница 9: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL FUEL FLOW TRANSMITTER INSTALLATION Figure 1 MASTER EFFECTIVITY See Pageblock 73 32 00 page 1 73 32 00 Page 3 Dec 20 2004...

Страница 10: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL FUEL FLOW FF INDICATING SYSTEM SCHEMATIC Figure 2 MASTER EFFECTIVITY See Pageblock 73 32 00 page 1 73 32 00 Page 4 Dec 20 2004...

Страница 11: ...F FUEL USED PULSE 2 1 0 3 4 5 FUEL FLOW KG H x 100 dam01_7332000_003 dg gw 31 10 01 1 Engine No 1 indicating system shown engine No 2 system similar 2 Identification code is 7331 NOTE INDICATOR FUEL F...

Страница 12: ......

Страница 13: ...HTR S2 b On the right DC circuit breaker panel FUEL FLOW IND ENG 2 Q5 IND LCD HTR A1 3 Remove the fuel flow indicator 1 as follows a Loosen the top right and lower left screws 3 that attach the indic...

Страница 14: ...t access to the transmitter refer to AMM 06 40 10 3 For the No 2 fuel flow transmitter open the access panel 424AR to get access to the transmitter refer to AMM 06 40 10 4 Remove the fuel flow transmi...

Страница 15: ...ttom fuel line 4 Connect the bottom fuel line 4 to the fuel flow transmitter 1 f Remove the protective cap from the top fuel line 3 Connect the top fuel line 3 to the fuel flow transmitter 1 g Remove...

Страница 16: ...nstrument panel LEGEND 0 2 4 6 8 10 12 PPH x 100 FF 4 3 2 1 3 dam01_7332004_002 dg gw aug14 2008 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL Fuel Flow Indicator Removal and Installation Figure 201 MASTER...

Страница 17: ...1 Fuel flow transmitter 2 Electrical connector 3 Fuel line 4 Fuel line 5 Bolt 6 Washer 7 Bracket LEGEND D SERIES 100 AIRCRAFT MAINTENANCE MANUAL FUEL FLOW TRANSMITTER REMOVAL INSTALLATION Figure 202...

Страница 18: ...USE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT 1 Apply electrical power to the aircraft refer to AMM 12 00 05 2 Push and hold the test button on the indicator Make sure that The pointer moves to the b...

Страница 19: ...y 5 ampere FUEL TEMP ENG 1 N4 left secondary bus and FUEL TEMP ENG 2 E4 right secondary bus circuit breakers Lighting for the indicator is from the 5V dc lighting system refer to Chapter 33 The indica...

Страница 20: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL FUEL TEMPERATURE INDICATING SCHEMATIC Figure 1 MASTER EFFECTIVITY See Pageblock 73 33 00 page 1 73 33 00 Page 2 Dec 20 2004...

Страница 21: ...Loosen the indicator top right securing screw approximately five turns b Push in the securing screws to disengage the clamping mechanism c Slide out the fuel temperature indicator d Disconnect the co...

Страница 22: ...fuel temperature indicator is unserviceable or there is no power supply to the indicator the pointer on the indicator will move off the scale below 40 C 40 F 6 If the fuel temperature indicator is ser...

Страница 23: ...ND 1 2 3 dam01_7333004_001 dg kmw aug14 2008 FUEL TEMP 80 40 0 40 C o 1 2 80 40 0 40 C o D SERIES 100 AIRCRAFT MAINTENANCE MANUAL Fuel Temperature Dual Indicator Removal and Installation Figure 201 MA...

Страница 24: ......

Страница 25: ...F propeller RPM PROP RPM and high pressure compressor NH indicators are each provided with liquid crystal display LCD for digital readouts Pre mod 8 1 1101 aircraft indicators incorporate temperature...

Страница 26: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL ENGINE INSTRUMENT PANEL Figure 1 MASTER EFFECTIVITY See Pageblock 77 00 00 page 1 77 00 00 Page 2 Dec 20 2004...

Страница 27: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL ENGINE INDICATING SENSING COMPONENTS ON ENGINE Figure 2 MASTER EFFECTIVITY See Pageblock 77 00 00 page 1 77 00 00 Page 3 Dec 20 2004...

Страница 28: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL PRE MOD 8 1 1101 LIQUID CRYSTAL DISPLAY LCD HEATERS ELECTRICAL SCHEMATIC Figure 3 MASTER EFFECTIVITY See Pageblock 77 00 00 page 1 77 00 00 Page 4 Dec 20 2004...

Страница 29: ...nit SCU are described in the Engine Maintenance Manual For location of SCU and sensor refer to ENGINE INDICATING GENERAL Figure 2 The SCUs of both engines are interconnected by electrical circuits to...

Страница 30: ...r from the associated ECU opp engine uptrim discrete which initiates engine uptrim A press to test pushbutton on the front of the indicator can be used to verify operation of indicator internal circui...

Страница 31: ...pointer and digital display indicate zero and PWR UPTRIM light goes out 7 Repeat steps 4 5 and 6 for the right torque indicator press to test switch NOTE Operation of PWR UPTRIM light confirms functio...

Страница 32: ...O INTERNAL DOCUMENT dam01_7710000_001 cgm cg 10 07 03 PRE MOD 8 0886 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL TORQUE INDICATING SYSTEM Figure 1 Sheet 1 of 2 MASTER EFFECTIVITY See Pageblock 77 10 00 p...

Страница 33: ...TO INTERNAL DOCUMENT MOD 8 0886 dam01_7710000_002 cgm cg 10 07 03 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL TORQUE INDICATING SYSTEM Figure 1 Sheet 2 of 2 MASTER EFFECTIVITY See Pageblock 77 10 00 pag...

Страница 34: ...REFER TO INTERNAL DOCUMENT REFER TO INTERNAL DOCUMENT D SERIES 100 AIRCRAFT MAINTENANCE MANUAL TORQUE INDICATOR Figure 2 MASTER EFFECTIVITY See Pageblock 77 10 00 page 1 77 10 00 Page 6 Dec 20 2004...

Страница 35: ...NICS M1 TORQUE IND BUG RIGHT DC R3 ENGR INSTR 3 Loosen the torque TRQ indicator top right and lower left securing screws approximately five turns 4 Push in the torque TRQ indicator top right and lower...

Страница 36: ...e unlit blue dot at 105 and the digital display shows 105 0 8 Release the PRESS TO TEST push button on the torque TRQ indicator Check that the analog pointer and digital display show 0 9 On the overhe...

Страница 37: ...em b Power to engine electronic control unit ECU ECU ENG 1 K4 on 28V dc left essential bus circuit breaker panel and ECU ENG 1 J7 Mod 8 0488 on right 28V dc essential bus circuit breaker panel When ch...

Страница 38: ...epeat step 7 to obtain digital readings for indicator and voltage output to Flight Data Recorder FDR within limits of Figure 202 9 Disconnect power supplies Reconnect connectors 7700 P1 at ECU 7700 P7...

Страница 39: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL TORQUE SYSTEM CALIBRATION CHECK DETAILS Figure 201 MASTER EFFECTIVITY See Pageblock 77 10 11 page 201 77 10 11 Page 203 Dec 20 2004...

Страница 40: ...The tesyt values in the table apply only when 5 volts reference volts is applied to pin 5 of electrical connector 7700 P7 during calibration check Should reference voltage other than 5 volts be usedd...

Страница 41: ...mpute the ac signal from its associated speed sensor and provide an equivalent readout of NH speed by means of a moving pointer against a fixed dial and an equivalent digital display A 0 to 5 V dc sig...

Страница 42: ...or 0 5 switch S1 opens and igniter operation is inhibited Ref Chapter 74 Engine Ignition System Do an operational test of the NH speed indicator auto relight system after replacement of a NH speed ind...

Страница 43: ...4 S1 NO 28VDC TO AUTO RELIGHT CTRL RELAY dam10_771200_001 NOTE Circuits shown for engine No 1 Engine No 2 circuits similar Ident code is 7711 unless otherwise indicated Refer to chapter 33 Refer to ch...

Страница 44: ......

Страница 45: ...R 3 Loosen the NH indicator top right and lower left securing screws approximately five turns 4 Push in the NH indicator top right and lower left securing screws to disengage the clamping mechanism 5...

Страница 46: ...S TO TEST push button on the NH indicator Check that the analog pointer and digital display show 0 9 On the overhead console rotate the ENGINE PANEL lighting selector from OFF to BRT Check that the NH...

Страница 47: ...el behind avionics rack 5 Connect signal generator across pins 1 and 2 of sensor electrical connector 7711 P5 6 Close ENG 1 NH IND engine No 1 circuit breaker or ENG 2 NH IND engine No 2 circuit break...

Страница 48: ...O FLIGHT DATA RECORDER Circuits shown for engine no 1 Engine no 2 circuits similar Ident code is 7711 unless otherwise indicated NOTE NH SENSOR MAGNETIC PICK UP P5 B A B D POWER GROUND 5 28VDCL SEC BU...

Страница 49: ...596 3 798 100 80 60 40 20 4 55 3 64 2 73 1 82 0 91 TOLERANCES POINTER OR 1 0 DIGITS OR 0 3 RECORDER OR 0 03 Volts D SERIES 100 AIRCRAFT MAINTENANCE MANUAL NH CALIBRATION CHECK VALUES Figure 202 MASTE...

Страница 50: ...ide 425AL Nacelle right side 424AR WARNING MAKE SURE THAT ALL PERSONS IN THE AREA OF THE AIRCRAFT ARE TOLD BEFORE THE ELECTRICAL SYSTEM IS ENERGIZED IF YOU DO NOT DO THIS YOU CAN CAUSE INJURIES TO PER...

Страница 51: ...displays 0 Audible firing of both ignitors at Engine 2 e On the center console set the PROP 2 Lever to FUEL OFF and observe the following No audible firing of both ignitors at Engine 2 f On the ENGIN...

Страница 52: ...measured at 9811 TB19 Pin 3C h Move engine ignition switch 1 to the AUTO position Check that 28 VDC cannot be measured at 9811 TB19 Pin 3C i Slowly move the Condition Lever 1 on the center console to...

Страница 53: ...QUIPMENT d Apply electrical power to the aircraft e Close engine 2 ignition CB f Check the Condition Lever 2 on the center console is at the FUEL OFF position g Check that 28 VDC cannot be measured at...

Страница 54: ...03L18 to 2A r Disconnect 9811 P48 and check that continuity exist between Pin M and Pin K when the Condition Lever 2 is in the FUEL OFF position s Move the Condition Lever 2 to the START FEATHER posit...

Страница 55: ...rcuits and indicating mechanisms for engine No 1 and engine No 2 which receive separate inputs from the associated speed sensor The circuits are separately powered from the 28 V dc essential buses cir...

Страница 56: ...ERIES 100 AIRCRAFT MAINTENANCE MANUAL ENGINE LOW PRESSURE COMPRESSOR ROTOR SPEED NL INDICATING SYSTEM WIRING DIAGRAM Figure 1 MASTER EFFECTIVITY See Pageblock 77 14 00 page 1 77 14 00 Page 2 Jun 20 20...

Страница 57: ...he securing screws to disengage the clamping mechanism 5 Slide out the NL indicator 6 Disconnect the connector and remove the NL indicator B Installation of the NL Indicator 1 Make sure the aircraft i...

Страница 58: ...t the NL indicator back lighting varies from off to bright 8 Do an engine start refer to Chapter 71 00 00 9 Check for correct operation of the NL indicator s 10 Shut down engine refer to Chapter 71 00...

Страница 59: ...circuit breaker F5 and engine No 2 from the right bus protected by the ENG 2 ITT IND circuit breaker F5 Indicator lighting is white powered from the 5 V dc lighting system refer to Chapter 33 The ind...

Страница 60: ...dial a blue dot on the face of the indicator dial and an equivalent digital display Releasing the test pushbutton causes the indicator pointer to return to its original setting with an equivalent dig...

Страница 61: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL INTER TURBINE TEMPERATURE ITT INDICATING SYSTEM Figure 1 MASTER EFFECTIVITY See Pageblock 77 20 00 page 1 77 20 00 Page 3 Dec 20 2004...

Страница 62: ......

Страница 63: ...R 3 Loosen the ITT indicator top right and lower left securing screws approximately five turns 4 Push in the ITT indicator top right and lower left securing screws to disengage the clamping mechanism...

Страница 64: ...ws 1050 and the overtemperature advisory light is ON 8 Release the PRESS TO TEST push button on the ITT indicator Check that the analog pointer and digital display shows current engine temperature 9 O...

Страница 65: ...1 5 Press test pushbutton on indicator and check overtemperature warning light on at 810 degrees C pointer positions opposite blue dot at 1050 degrees C and equivalent digital reading Release pushbutt...

Страница 66: ...leads to terminal block and torque alumel nut large diameter to 25 to 30 pound inches and chromel nut small diameter to 20 to 25 pound inches refer to Figure 203 13 Close circuit breakers refer to st...

Страница 67: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL MILLIVOLT SETTINGS CORRECTED FOR AMB TEMP Figure 201 Sheet 1 of 2 MASTER EFFECTIVITY See Pageblock 77 20 11 page 201 77 20 11 Page 203 Dec 20 2004...

Страница 68: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL MILLIVOLT SETTINGS CORRECTED FOR AMB TEMP Figure 201 Sheet 2 of 2 MASTER EFFECTIVITY See Pageblock 77 20 11 page 201 77 20 11 Page 204 Dec 20 2004...

Страница 69: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL INTER TURBINE TEMPERATURE ITT INDICATING SYSTEM CALIBRATION DETAILS Figure 202 MASTER EFFECTIVITY See Pageblock 77 20 11 page 201 77 20 11 Page 205 Dec 20 2004...

Страница 70: ...T D SERIES 100 AIRCRAFT MAINTENANCE MANUAL INTER TURBINE TEMPERATURE ITT INDICATING SYSTEM CALIBRATION DETAILS Figure 203 MASTER EFFECTIVITY See Pageblock 77 20 11 page 201 77 20 11 Page 206 Dec 20 20...

Страница 71: ...OR 9 DEG C OR 9 DEG C OR 5 DEG C OR 5 DEG C OR 5 DEG C OR 5 DEG C OVERTEMPERATURE WARNING LIGHT IS SET TO COME ON AT APPROXIMATELY 810 oC 2 5 C 0 C D SERIES 100 AIRCRAFT MAINTENANCE MANUAL ITT CALIBR...

Страница 72: ......

Страница 73: ...eft side of the engine Access to the sight glass is by means of a hinged access door in the engine left side cowl Components shown are oil pressure transmitter and low oil pressure switch both connect...

Страница 74: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OIL INDICATING COMPONENTS Figure 1 MASTER EFFECTIVITY See Pageblock 79 30 00 page 1 79 30 00 Page 2 Dec 20 2004...

Страница 75: ...ter deflects the diaphragm and unbalances the bridge to produce an output signal of 0 to 100 milivolts proportional to 0 to 100 psi corrected for reference pressure The signal is applied to the oil pr...

Страница 76: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OIL PRESSURE INDICATING AND ELECTRICAL SCHEMATIC Figure 1 MASTER EFFECTIVITY See Pageblock 79 32 00 page 1 79 32 00 Page 2 Dec 20 2004...

Страница 77: ...screws to disengage the clamping mechanism 5 Slide out the OIL PRESS TEMP dual indicator 6 Disconnect the connector and remove the OIL PRESS TEMP dual indicator B Installation of the OIL PRESSURE TEM...

Страница 78: ...to Chapter 71 00 00 8 Check for correct operation of the OIL PRESS TEMP dual indicator 9 Shut down the engine Refer to Chapter 71 00 00 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL MASTER EFFECTIVITY 79...

Страница 79: ...oil pressure and temperature dual indicator is marked ENG OIL and has two scales and pointers one scale marked PSI and the other degrees C On aircraft incorporating Mod 8 1050 the oil pressure temper...

Страница 80: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OIL TEMPERATURE INDICATING AND ELECTRICAL SCHEMATIC Figure 1 MASTER EFFECTIVITY See Pageblock 79 34 00 page 1 79 34 00 Page 2 Dec 20 2004...

Страница 81: ...ronic safety precautions refer to AMM 24 00 00 5 Disconnect the electrical connector 2 from the oil temperature bulb 1 6 Put the protective cap on the electrical connector 2 WARNING YOU MUST WEAR EYE...

Страница 82: ...ngine instrument panel in the flight compartment 12 Do the engine shutdown for the related engine refer to AMM 71 00 00 13 Install the left side center panel 413 AL engine No 1 or 423 AL engine No 2 r...

Страница 83: ...b 2 Electrical connector 3 Packing 4 Adapter LEGEND dam01_7934032_001 dg cs apr04 2012 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OIL TEMPERATURE BULB REMOVAL INSTALLATION Figure 201 MASTER EFFECTIVITY...

Страница 84: ......

Страница 85: ...bomachinery accessory gearbox cavity pressure The switches are each provided with two contact sets the normally closed contact of one set in each switch is connected to and controls the operation of t...

Страница 86: ...ES 100 AIRCRAFT MAINTENANCE MANUAL ENGINE OIL PRESSURE LOW WARNING SYSTEM PRE MOD 8 0235 AND 8 0446 ELECTRICAL SCHEMATIC Figure 1 MASTER EFFECTIVITY See Pageblock 79 36 00 page 1 79 36 00 Page 2 Dec 2...

Страница 87: ...RIES 100 AIRCRAFT MAINTENANCE MANUAL ENGINE OIL PRESSURE LOW WARNING SYSTEM MOD 8 0235 AND 8 0446 ELECTRICAL SCHEMATIC Figure 2 MASTER EFFECTIVITY See Pageblock 79 36 00 page 1 79 36 00 Page 3 Dec 20...

Страница 88: ......

Страница 89: ...ical connector 1 7 Put a container below the tubes 3 and 4 to collect the oil drain 8 Disconnect the tubes 3 and 4 from the oil pressure switch 2 9 Put the protective caps on the open ends of the tube...

Страница 90: ...panel 413 AL engine No 1 or 423 AL engine No 2 Refer to Chapter 71 10 00 12 Install the lower forward nacelle cowl Refer to Chapter 71 10 00 13 Remove main gear doors lock pin and close the doors ref...

Страница 91: ...7 4 1 Electrical connector 2 Oil pressure switch 3 Tube 4 Tube 5 Nut 6 Washer 7 Screw 8 Bracket LEGEND D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OIL PRESSURE SWITCH REMOVAL INSTALLATION Figure 201 MAS...

Страница 92: ...5 6 1 Electrical connector 2 Oil pressure switch 3 Tube 4 Tube 5 Nut 6 Washer 7 Screw 8 Bracket LEGEND D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OIL PRESSURE SWITCH REMOVAL INSTALLATION Figure 202 MAS...

Страница 93: ...E EQUIPMENT 4 Obey all the electrical electronic safety precautions refer to AMM 24 00 00 5 Disconnect the electrical connector 2 from the oil pressure transmitter 1 6 Put the protective caps on the e...

Страница 94: ...same specification and install it to the union 5 13 Install the union 5 to the oil pressure transmitter 1 14 Remove the protective cap from the tube 3 15 Connect the tube 3 to the union 5 refer to AMM...

Страница 95: ...tainer 9 Packing 10 Clamp 11 Screw LEGEND 12 Washer 13 Nut 14 Bracket 7 8 9 15 16 15 Tube 16 Tube dam01_7936032_001 dg hp mar26 2012 OIL PRESSURE SWITCH REF D SERIES 100 AIRCRAFT MAINTENANCE MANUAL OI...

Страница 96: ...11 Screw LEGEND 12 Washer 13 Nut 14 Bracket 15 Tube 16 Tube dam01_7936032_002 dg hp mar26 2012 2 1 4 5 6 10 11 7 8 9 15 16 13 12 OIL PRESSURE SWITCH REF 14 3 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL...

Страница 97: ...he mounting bracket is attached to the propeller shaft seal housing of the engine reduction gearbox at 5 o clock view on front of propeller shaft The synchrophase control unit located on electrical eq...

Страница 98: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL PROPELLER SYNCHROPHASING SYSTEM ELECTRICAL SCHEMATIC Figure 1 MASTER EFFECTIVITY See Pageblock 61 29 00 page 1 61 29 00 Page 2 Dec 20 2004...

Страница 99: ...ignal from engine No 1 propeller pulse generator as the reference or master signal relay a correction signal as required to the torque motor of engine No 2 PCU The torque motor operates through the PC...

Страница 100: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL SYNCHROPHASER PULSE GENERATOR DETAILS Figure 2 MASTER EFFECTIVITY See Pageblock 61 29 00 page 1 61 29 00 Page 4 Dec 20 2004...

Страница 101: ...ns of moving pointer against a fixed dial and an equivalent digital display A 0 to 5 V dc signal proportional to propeller RPM is relayed to the flight data recorder refer to Chapter 31 The indicator...

Страница 102: ...Beta Lockout System Installed CR873CH00011 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL MASTER EFFECTIVITY See Pageblock 61 44 00 page 1 61 44 00 Page 2 Dec 20 2004...

Страница 103: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL PROPELLER SPEED NP INDICATING Figure 1 MASTER EFFECTIVITY See Pageblock 61 44 00 page 1 61 44 00 Page 3 Dec 20 2004...

Страница 104: ......

Страница 105: ...sen the propeller PROP RPM indicator top right and lower left securing screws approximately five turns 4 Push in the propeller PROP RPM indicator top right and lower left securing screws to disengage...

Страница 106: ...eck 1 With dc power on press test pushbutton on indicator Check pointer moves opposite blue dot at 1050 RPM and equivalent digital reading Check that on release of pushbutton indicator returns to orig...

Страница 107: ...nd repeat step 7 to obtain digital readings for indicator and voltage output to Flight Data Recorder FDR within limits of Figure 201 9 Open circuit breakers step 2 a or b and remove signal generator 1...

Страница 108: ...DIGITAL FLIGHT DATA RECORDER VOLTS 3 400 2 720 1 813 907 453 1500 1200 800 400 200 5 00 4 00 2 67 1 33 0 67 D SERIES 100 AIRCRAFT MAINTENANCE MANUAL NP CALIBRATION CHECK VALUES Figure 201 MASTER EFFEC...

Страница 109: ...D SERIES 100 AIRCRAFT MAINTENANCE MANUAL NP INDICATING SYSTEM CALIBRATION DETAILS Figure 202 MASTER EFFECTIVITY See Pageblock 61 44 00 page 201 61 44 00 Page 205 Jun 20 2005...

Страница 110: ......

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