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C F M 56-5B HIGHLIGHTS __________ REVISION NO. 54 May 01/08
Pages which have been revised are outlined below, together with the Highlig Revision
--------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIV PAGES --------------------------------------------------------------------------CHAPTER 76 __________
L.E.P. 1- 1 REVISED TO REFLECT THIS REVISION INDICATING NEW,REVISED, AND/OR DELETED PAGES T. OF C. REVISED TO REFLECT THIS REVISION 1 76-11-00 EFFECTIVITY UPDATED 5, 7, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 9, 1112 76-11-19 407, 411412
EFFECTIVITY UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
76-11-41 405, 411415, 419, 421
EFFECTIVITY UPDATED CONSUMABLE INGREDIENT DATA UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
201-225, 229-275 426-499, 503-549 701-749,
201-225, 227-227 426-455, 476-499 551-599, 701-749
ALL 201-225, 227-227 426-499, 503-549 701-749,
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C F M 56-5B CHAPTER __________ 76 ENGINE CONTROLS
LIST _______________________ OF EFFECTIVE PAGES N, R or D indicates pages which are New, Revised or Deleted respectively Remove and insert the affected pages and complete the Record of Revision Revisio the Record of Temporary Revisions as necessary
CH/SE/SU
C
PAGE
DATE
RECORD OF TEMP. REVISION L.E.P. T. of C. T. of C.
R 1- 1 May01/08 R 1 May01/08 2 Feb01/07
76-00-00 76-00-00 76-00-00 76-00-00 76-00-00
1 2 3 4 5
76-10-00 76-10-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00
Feb01/02 Feb01/96 Feb01/96 Feb01/96 Feb01/96
1 Feb01/96 2 Feb01/96
R R R R R
1 2 3 4 5 6 7 8 9 10 11 12
Feb01/96 Feb01/96 Feb01/96 Feb01/96 May01/08 Feb01/96 May01/08 Feb01/07 May01/08 Feb01/07 May01/08 May01/08
CH/SE/SU 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-00 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-17 76-11-19 76-11-19 76-11-19 76-11-19 76-11-19 76-11-19 76-11-19 76-11-19
C
PAGE
DATE
CH/SE/SU
C
510 May01/96 76-11-41 511 May01/96 76-11-41 512 Feb01/99 76-11-41 513 May01/99 76-11-41 514 May01/96 76-11-41 515 May01/96 76-11-41 401 Feb01/96 76-11-41 402 Feb01/99 76-11-41 403 Feb01/99 76-11-41 404 Feb01/96 76-11-41 405 Feb01/96 76-11-41 406 Feb01/96 76-11-41 407 Feb01/96 76-11-41 408 May01/99 76-11-41 409 Feb01/96 76-11-41 410 Feb01/99 76-11-41 411 May01/99 76-11-41 412 Feb01/96 76-11-41 413 Aug01/04 414 Feb01/99 76-12-00 415 Feb01/99 76-12-00 401 Feb01/97 76-12-00 402 Feb01/97 76-12-00 403 May01/96 404 May01/96 up to vote on this title 405Sign May01/96 Useful Not useful 406 May01/05 R 407 May01/08 408 May01/05
PAG
R R R R R
R R
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C F M 56-5B CHAPTER __________ 76 ENGINE CONTROLS
TABLE _________________ OF CONTENTS
SUBJECT _______ ENGINE _________________________ CONTROLS - GENERAL DESCRIPTION AND OPERATION General Throttle Control Lever ENG/MASTER Control Switch LP Fuel Shutoff Valve Control Component Location
________ CH/SE/SU 76-00-00
POWER _____________ CONTROL DESCRIPTION AND OPERATION General Manual Thrust Setting Mode (the autothrust function is not active) Automatic Thrust Setting Mode (the autothrust function is active)
76-10-00
THROTTLE CONTROL DESCRIPTION AND OPERATION General Throttle Control Mechanical Parts Throttle Control Lever Throttle Control Artificial Feel Unit Throttle Control Unit
Throttle Control Unit THROTTLE CONTROL
C _
PAGE ___________ ____ EFFECTIVITY 1 ALL 1 ALL 1 ALL 1 ALL 1 ALL 4 ALL 1 ALL 1 ALL 1 ALL 1
ALL
76-11-00 1 ALL 1 ALL 1 ALL 1 ALL 5 ALL 5
201-225, 279-299, 503-549, 701-749, Sign up to vote on this title 13 227-227,
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C F M 56-5B CHAPTER __________ 76 ENGINE CONTROLS
TABLE _________________ OF CONTENTS _______ SUBJECT REMOVAL/INSTALLATION REMOVAL/INSTALLATI ON Removal of the Throttle Control Unit (8KS1, 8KS2) Installation of the Throttle Control Unit (8KS1, 8KS2) LEVER ASSEMBLY - THROTTLE CONTROL REMOVAL/INSTALLATION REMOVAL/INSTALLATI ON Removal of the Throttle Control Lever Assembly Installation of the Throttle Control Lever Assembly
CH/SE/SU ________
ENGINE MASTER CONTROL DESCRIPTION AND OPERATION HP Fuel Shut OFF Valve Control General Valve Operation LP Fuel Shut Off Valve Control General Valve Operation
76-12-00
C _
____ ___________ PAGE EFFECTIVITY 401 ALL 401 ALL 406
ALL
401 401
ALL ALL
415
ALL
1 1 1 1 4 4 4
ALL ALL ALL ALL ALL ALL ALL
76-11-41
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C F M 56-5B ENGINE _____________________________________________________ CONTROLS - GENERAL - DESCRIPTION AND OPERATION
1. General _______ The engine control system consist of : - the throttle control - the HP fuel shutoff valve control - the LP fuel control.
A. Throttle Control Lever (Ref. Fig. 001) The throttle control system is fully electrical. The throttle con lever drives the position detectors. The position detectors are under the cockpit center pedestal. Two of the resolvers are dedica the FADEC system. Each channel of the Electronic Control Unit rec the position signal from one resolver in the analog form.
R
B. ENG/MASTER Control Switch (Ref. Fig. 002) The MASTER control switch interfaces with the HP fuel shutoff val the Engine Interface Unit (EIU). It controls directly the closure of the fuel shutoff valve : it the valve solenoid. An analog signal informs the EIU of the position of the MASTER switch. The EIU transmits then the information to the ECU in digital form. The ECU uses this information to initiate the automatic and manual starting sequences. The MASTER control switches are part of the panel 115VU, switch replacement requires removal of panel 115VU. C. LP Fuel Shutoff Valve Control The LP fuel shutoff valve is electrically controlled : - either by the ENG/MASTER control switch on the ENG panel - or by the ENG FIRE pushbutton switch. Sign up to vote on this title
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C F M 56-5B 2. Component __________________ Location (Ref. Fig. 003)
----------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I I I I I DOOR I ----------------------------------------------------------------------2KC CTL SW-ENG/MASTER 2 115VU 210 3KC CTL SW-ENG/MASTER 1 115VU 210 4000KC SOLENOID-HP FUEL SOV 437 437AL 447 447AL 8KS1 CTL UNIT-THROTTLE, ENG1 11VU 210 8KS2 CTL UNIT-THROTTLE, ENG2 11VU 210
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C F M 56-5B POWER _________________________________________ CONTROL - DESCRIPTION AND OPERATION
1. General _______ (Ref. Fig. 001)
A. Manual Thrust Setting Mode (the autothrust function is not active) active The throttle control lever in the cockpit center pedestal controls - the engine level of thrust - the thrust limit mode. The Electronic Control Unit (ECU): - receives the throttle lever angle - computes the engine thrust limit parameter and adjusts the actua engine thrust parameter accordingly.
B. Automatic Thrust Setting Mode (the autothrust function is active) The throttle control lever controls : - the actual thrust limit - the thrust limit mode. The FMGC computes the target thrust parameter and sends it to the The ECU adjusts the actual engine thrust parameter according to value (Ref. 73-20-00). The top limit value of the target thrust parameter is the actual of the throttle control lever (this is applicable when the alpha protection is not activated).
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C F M 56-5B THROTTLE ____________________________________________ CONTROL - DESCRIPTION AND OPERATION
1. General _______ (Ref. Fig. 001) The throttle control system consist of : - the throttle control lever - the throttle control artificial feel unit - the throttle control unit - the electrical harness. In addition each throttle control lever is fitted with an instinctive pushbutton switch. This pushbutton switch serves for the de-activation and disengagement autothrust function. The design of the throttle control is based upon a fixed throttle this means that the throttle control levers are not servo motorized. 2. Throttle _________________________________ Control Mechanical Parts
A. Throttle Control Lever (Ref. Fig. 002, 003) The throttle control handle comprises : - a throttle control lever which incorporates stop devices and instinctive disconnect pushbutton switch - a graduated fixed sector - a reverse latching lever. The throttle control lever moves over a range from : - -20 deg. TLA (Reverser Full Throttle stop) to 45 deg. TLA (Forwa Throttle stop). An intermediate mechanical stop is fitted at 0 deg. TLA. This stop is overriden when the reverse latching lever is pulled selection of the reverse power. This idle stop is reset as soon as the lever is selected back to thrust area. In the forward thrust area, there are two detent points : - MAX CLIMB detent point set at 25 deg. TLA - MAX CONTINUOUS/FLEX TAKE OFF detent point set at 35 deg. TLA. up tois voteone on this title point In the reverse thrust throttle range, Sign there detent Not useful - -6 deg. TLA, this position corresponds to the of the Useful selection reverser command and the Reverse Idle setting. From -20 deg. TLA to 0 deg. TLA, the autothrust function cannot
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C F M 56-5B In the forward range (35 deg. to 45 deg. TLA), the autothrust fun cannot be activated (except in alpha floor condition). This range corresponds to the selection of FLEX TAKE OFF/MAX TAKE AROUND) mode. The throttle control lever is linked to a mechanical rod. This the input lever of the throttle control artificial feel unit.
B. Throttle Control Artificial Feel Unit (Ref. Fig. 004) The Throttle control artificial feel unit is located below the center pedestal. this artificial feel unit is connected to engine throttle control lever and to the engine 1(2) throttle control means of rods. The artificial feel unit is a friction system wich provides a load feedback to the throttle control lever. This artificial feel unit comprises two symetrical casings, one one right. Each casing contains an identical and independent mecha Each mechanism is composed of: - a friction brake assembly - a gear assembly - a lever assembly - a bellcrank assembly Throttle control lever travel is transmitted to the artificial unit and to the throttle control unit. The linear movement of the throttle control levers is transforme a rotary movement at the bellcrank which turns around the fricti brake assembly shaft. This movement rotates a toothed quadrant with the shaft. This toothed quadrant causes inverse rotation of a gear equipped disk which has four detent notches. Each notch corresponds to throttle control lever setting and is felt as a friction point throttle control levers. R
**ON A/C 201-225, 229-275, 279-299, 426-499, 503-549, 551-599, 701-749,
C. Throttle Control Unit Sign up to vote on this title (Ref. Fig. 005, 006, 007) Not useful A mechanical rod transmits the throttle control movement. Useful lever It connects the throttle control artificial feel unit to the input of the throttle control unit.
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C F M 56-5B
Thrust Control Power Supplies Figure 007 R EFF : 201-225, 229-275, 279-299, 426-499, 503-549, 551-599, 701-749, SROS
76-11-00
Page 11/12 May 01/08
C F M 56-5B - a device which drives the resolver and the potentiometer Sign and up to vote on this title - a pin device for rigging the resolvers potentiometers Not useful - 1 switch whose signal is dedicated to Useful the EIU. - a safety device which leads the resolvers outside the normal range in case of failure of the driving device
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C F M 56-5B - a device which drives the resolver and the potentiometer - a pin device for rigging the resolvers and potentiometers - 1 switch whose signal is dedicated to the EIU. - a safety device which leads the resolvers outside the normal range in case of failure of the driving device - two output electrical connectors. The input lever drives two gear sectors assembled face to face. sector drives itself a set of one resolver and three potentiometer The relationship between the throttle lever angle and throttle angle (TRA) is linear and : 1 deg. TLA = 1.9 TRA. The accuracy of the throttle control unit (error between the input position and the resolver angle) is 0.5 deg. TRA. The maximum discrepancy between the signals generated by the two resolvers is 0.25 deg. TRA. The TLA resolver operates in two quadr the first quadrant serves for positive angles and the fourth quadr negative angles. Each resolver is dedicated to one channel of the ECU and receives electrical excitation from the ECU. The ECU considers a throttle resolver angle value : - less than -47.5 deg. TRA or - greater than 98.8 deg. TRA as resolver position signal failure. The ECU incorporates a resolver fault accomodation logic. This allows engine operation after a failure or a complete loss of the throttle resolver position signal. **ON A/C 227-227, 276-278,
C. Throttle Control Unit (Ref. Fig. 005A, 006A, 007A) A mechanical rod transmits the throttle control lever movement. It connects the throttle control artificial feel unit to the input of the throttle control unit. The throttle control unit comprises : - an input lever - mechanical stops which limit the angular range Sign upto to vote this (one title resolver - 2 resolvers whose signals are dedicated the onECU channel of the ECU) Useful Not useful - 6 potentiometers fitted three by three. Their signals are used flight control system
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C F M 56-5B The relationship between the throttle lever angle and throttle angle (TRA) is linear and : 1 deg. TLA = 1.9 TRA. The accuracy of the throttle control unit (error between the input position and the resolver angle) is 0.5 deg. TRA. The maximum discrepancy between the signals generated by the two resolvers is 0.25 deg. TRA. The TLA resolver operates in two quadr the first quadrant serves for positive angles and the fourth quadr negative angles. Each resolver is dedicated to one channel of the ECU and receives electrical excitation from the ECU. The ECU considers a throttle resolver angle value : - less than -47.5 deg. TRA or - greater than 98.8 deg. TRA as resolver position signal failure. The ECU incorporates a resolver fault accomodation logic. This allows engine operation after a failure or a complete loss of the throttle resolver position signal.
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C F M 56-5B
Thrust Control Power Supplies Figure 007A R EFF : 227-227, 276-278, SROS
76-11-00
Page 15/16 Feb 01/07
C F M 56-5B THROTTLE __________________________________ CONTROL - ADJUSTMENT/TEST
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TASK 76-11-00-820-044 Adjustment of the Mechanical Linkage
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C F M 56-5B THROTTLE __________________________________ CONTROL - ADJUSTMENT/TEST TASK 76-11-00-820-044 Adjustment of the Mechanical Linkage
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION -----------------------------------------------------------------------
R
No specific No specific No specific 98DNSA20206080 98DNSA20208080
blanking caps circuit breaker(s) safety clip(s) warning notice 2 RIGGING PIN 1 RIGGING PIN
B. Consumable Materials
----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------No specific No specific
lockwire 0.032 in. (0.8 mm) dia. lockwire 0.032 in. (0.8mm) dia.
C. Referenced Information
---------------------------------------------------------------------- Sign up to vote on this title REFERENCE DESIGNATION ---------------------------------------------------------------------- Useful Not useful 22-82-12-000-001
Removal of the MCDU (3CA1,3CA2,3CA3)
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C F M 56-5B ----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------23-51-12-400-001 34-41-12-000-001 34-41-12-400-001 34-52-12-000-001 34-52-12-400-001 76-11-00-991-910 76-11-00-991-911 76-11-00-991-912
Installation of the Audio Control Panel (ACP) 2RN2, 2RN3, 2RN4, 2RN5) Removal of the Weather Radar Control Unit (3SQ Installation of the Weather Radar Control Unit Removal of the ATC/TCAS Control Unit (3SH) Installation of the ATC/TCAS Control Unit (3SH Fig. 501 Fig. 502 Fig. 503
3. Job __________ Set-up Subtask 76-11-00-865-059 A. Open, safety and tag this(these) circuit breaker(s):
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 49VU LIGHTING/EMER LT/CKPT/DOME 1LE 105VU FLT CTL/SEC1/STBY SPLY 22CE 121VU ENGINE/IGN/ENG2/SYS B 3JH2 121VU ENGINE/IGN/ENG1/SYS B 3JH1 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF 122VU LIGHTING/FLOOD/CTR INST/PNL 2LE Subtask 76-11-00-941-056 B. Safety Precautions
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C F M 56-5B (3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the 1(2). Subtask 76-11-00-010-055 C. Open the access door 811.
4. Procedure _________ Subtask 76-11-00-869-060
A. Put the throttle control lever in the IDLE STOP position and hold this position (Ref. Fig. 501/TASK 76-11-00-991-910) detail A. (1) Adjust the length of the rod.
R R
CAUTION _______ : DO NOT APPLY FORCE TO PUSH IN OR PUSH OUT THE RIGGIN IN THE RIGGING HOLES. IF THE RIGGING PINS ARE DIFFIC PUSH IN, YOU MUST ADJUST THE RODS UNTIL THEY GO IN
(a) Make sure that you can easily install and remove the RIGGI (98DNSA20208080) (5) in the artificial feel unit (1). (b) If you can not do this, adjust the length of the rod (6). Subtask 76-11-00-820-058 B. Remove for access
SignDisplay up to vote Units on this title (1) Remove the Multipurpose Control and 3CA1 and (Ref. TASK 22-82-12-000-001) Useful Not useful
(2) Remove the Radio Management Panels 1RG1 and 1RG2 (Ref. TASK
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C F M 56-5B
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C F M 56-5B (4) Remove the Weather Radar Control Unit 3SQ (Ref. TASK 34-41-12001)
(5) Remove the ATC/TCAS Control Unit 3SH (Ref. TASK 34-52-12-000-0 (6) Remove the FLOOD LT/INTEG LT panel 111VU and FLOOD LT panel (Ref. Fig. 502/TASK 76-11-00-991-911)
NOTE ____ : The removal procedure is the same for the FLOOD LT/INTE panel 111VU and FLOOD LT panel 112VU. (a) Release the fasteners of the panel (1) and disengage the (1) from its housing. (b) Disconnect the connector (3) from the panel (1). (c) Remove the panel (1). (d) Put blanking caps on the connectors (2) and (3). (7) Remove the screws (14). (8) Remove the ventilation plates (15). (9) Disconnect the clamps (16). (10) Remove the screws (10) and the washers (11). (Ref. Fig. 503/TASK 76-11-00-991-912) (11) Remove the plates (12) and (13).
(12) Cut and remove the lockwire and adjust the length of the adjus rod (6) (Ref. Fig. 501/TASK 76-11-00-991-910) detail B.
Signand up tothe vote adjustable on this title (13) Tighten and safety the hinge points rod lockwire 0.032 in. (0.8 mm) dia.. Useful Not useful
Subtask 76-11-00-869-061
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C F M 56-5B
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C F M 56-5B
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C F M 56-5B (3) Install the pin again. (4) Make sure that you can: (a) Easily install the RIGGING PIN (98DNSA20206080) (3) in throttle control unit (4) and in the input lever, (b) Easily remove this pin from these components. (c) If you can not do this, adjust the length of the rod (2). Subtask 76-11-00-820-057
D. Cut and remove the lockwire and adjust the length of the adjustabl (2). (Ref. Fig. 501/TASK 76-11-00-991-910) detail B.
(1) Disconnect the rod (2) from the throttle control unit and the artificial feel unit to install the lockwire 0.032 in. (0.8mm) Tighten and safety the hinge points and the adjustable rod (2) Install the rod (2). Subtask 76-11-00-869-062 E. Remove the pin (5). With the throttle control lever in the IDLE position make sure that you can : (1) Easily remove the pin (3) from the throttle control unit. (2) Easily install this pin in this unit. Remove this pin. 5. Close-up ________ Subtask 76-11-00-869-063
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A. Make sure that all the pins are removed. Useful (1) Install the plates (12) and (13).
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C F M 56-5B (5) Install the screws (14).
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(6) Install the FLOOD LT/INTEG LT panel 111VU and FLOOD LT panel (Ref. Fig. 502/TASK 76-11-00-991-911)
NOTE ____ : The installation procedure is the same for the FLOOD LT panel 111VU and FLOOD LT panel 112VU. (a) Remove the blanking caps from the connectors (2) and (3). (b) Install the connector (2) on the panel (1). (c) Install the panel (1) on the structure. (d) Fully tighten the fasteners on the panel (1). (7) Install the Multipurpose Control and Display Units (3CA1 and (Ref. TASK 22-82-12-400-002)
(8) Install the Radio Management Panels (1RG1 and 1RG2) (Ref. TAS 13-400-001)
(9) Install the Audio Control Panels (2RN1 and 2RN2) (Ref. TASK 400-001)
(10) Install the Weather Radar Control Unit (3SQ) (Ref. TASK 34-41001)
(11) Install the ATC/TCAS Control Unit (3SH) (Ref. TASK 34-52-12-40
(12) Make sure that the work area is clean and clear of tool(s) items. Subtask 76-11-00-410-055 B. Close Access (1) Close the access door 811. (2) Remove the access platform(s).
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C F M 56-5B Subtask 76-11-00-865-060 C. Remove the safety clip(s) and the tag(s) and close this(these) breaker(s): 1JH, 2JH1, 2JH2, 3JH1, 3JH2, 21CE1, 21CE2, 22CE, 21CE3. Subtask 76-11-00-869-064 D. With the throttle control lever in the IDLE STOP position, make you can: (1) easily install the pin (5) in the artificial feel unit (1) (2) easily remove this pin from the artificial feel unit (1) (3) install the pin again. (4) Make sure that you can : (5) easily install the RIGGING PIN (98DNSA20206080) (3) in the control unit (4) and in the input lever, (6) easily remove this pin from these components. (a) If you can not do this, adjust the length of the rod (2). Subtask 76-11-00-710-053
E. Do an operational test of the FLOOD LT/ING LT panel 111VU and FLO panel 112VU : (1) Operate the light adjustment knobs of the FLOOD LT/INTEG LT 11VU and FLOOD LT panel 112VU.
(2) Make sure that the light intensity of the glareshield 13VU, glareshield panel 130VU, CAPT glareshield panel 131VU and over Sign up to vote on this title control & indicating panel 48VU changes.
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C F M 56-5B TASK 76-11-00-820-045 Adjustment of the Artificial Feel Unit
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------------No specific No specific No specific 98D76103000000
circuit breaker(s) safety clip(s) warning notice access platform 1.8 m (5 ft. 11 in.) 1 THROTTLE LEVER LOAD MEASURE
B. Consumable Materials
----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------No specific
lockwire 0.032 in. (0.8mm) dia.
C. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------76-11-00-991-913
Fig. 504
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C F M 56-5B 3. Job __________ Set-up Subtask 76-11-00-865-061 A. Open, safety and tag this(these) circuit breaker(s): R R
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 105VU FLT CTL/SEC1/STBY SPLY 22CE 121VU 121VU 121VU 121VU 121VU 121VU
ENGINE/IGN/ENG2/SYS B ENGINE/IGN/ENG1/SYS B ENGINE/IGN/ENG2/SYS A BAT ENGINE/IGN/ENG1/SYS A BAT FLIGHT CONTROLS/SEC3/SPLY FLIGHT CONTROLS/SEC2/SPLY
3JH2 3JH1 2JH2 2JH1 21CE3 21CE2
Subtask 76-11-00-941-057 B. Safety Precautions (1) On the center pedestal, on the ENG panel 115VU:
(a) Put a warning notice to tell persons not to start the engi
(2) Make sure that the engine 1(2) shutdown occurred not less tha minutes before you do this procedure. (3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
Sign up to vote title (b) Put a warning notice to tell persons not ontothisenergize the 1(2). Useful Not useful
Subtask 76-11-00-480-052
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C F M 56-5B Subtask 76-11-00-941-058 D. Put an access platform below the forward avionics compartment. Subtask 76-11-00-010-056 E. Open the access door 811.
4. Procedure _________ (Ref. Fig. 504/TASK 76-11-00-991-913) Subtask 76-11-00-020-052 A. Loosen the three screws (3). Remove the guard (7).
(1) Cut and remove the lockwire from the lock nut (6). Loosen the nut. Subtask 76-11-00-820-059
R R
B. Hold the adjusting rod (5) then turn the nut (4) to get a load +0.1 -0 daN (1.8 +0.22 -0.0000 lbf) on the related throttle contro lever.
NOTE ____ : Measure this value in the IDLE STOP/MAX CLIMB range. Do measure this value at the detent points where the load incr suddenly.
(1) Tighten the lock nut (6) to block the adjustment system. Measu load again to make sure that it is the same. Subtask 76-11-00-420-052 C. Safety the lock nut (6) with lockwire 0.032 in. (0.8mm) dia.. Subtask 76-11-00-020-053
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D. Cut and remove the lockwire from the lock nut (2). Loosen the loc
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C F M 56-5B
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C F M 56-5B (1) Block the adjustment system. Measure the load again to make it is the same as the value given in the paragraph E. Subtask 76-11-00-420-053 F. Safety the lock nut (2) with lockwire 0.032 in. (0.8mm) dia. (1) Install the guard (7). Tighten the three screws (3).
5. Close-up ________ Subtask 76-11-00-410-056 A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) items. (2) Close the access door 811. (3) Remove the access platform(s). (4) Remove the warning notice(s). Subtask 76-11-00-865-062
B. Remove the safety clip(s) and the tag(s) and close this(these) breaker(s): 1JH, 2JH1, 2JH2, 3JH1, 3JH2, 21CE1, 21CE2, 21CE3, 22CE Subtask 76-11-00-080-052 C. Remove the tool from the throttle control levers.
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C F M 56-5B ARTIFICIAL ______________________________________________________________ FEEL UNIT - THROTTLE CONTROL - REMOVAL/INSTALLATION REMOVAL/INSTALLATI ON TASK 76-11-17-000-042 Removal of the Throttle Control Artificial Feel Unit
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------------No specific No specific No specific No specific 98DNSA20206080
blanking caps circuit breaker(s) safety clip(s) warning notice access platform 1.8 m (5 ft. 11 in.) 1 RIGGING PIN
B. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------22-82-12-000-001 23-13-13-000-001 23-51-12-000-001 34-41-12-000-001 34-52-12-000-001 76-11-17-991-908 76-11-17-991-909 76-11-17-991-910
Removal of the MCDU (3CA1,3CA2,3CA3) Removal of the Radio Management Panel (CRMP) 1RG2, 1RG3) Removal of the Audio Control Panel (ACP) (2RN1 2RN3, 2RN4, 2RN5) Removal of the Weather Radar Control Unit (3SQ Sign up to vote on this title Removal of the ATC/TCAS Control Unit (3SH) Fig. 401 Useful Not useful Fig. 402 Fig. 403
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C F M 56-5B 3. Job __________ Set-up Subtask 76-11-17-865-056 A. Open, safety and tag this(these) circuit breaker(s):
R R
R
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 49VU LIGHTING/EMER LT/CKPT/DOME 1LE 105VU FLT CTL/SEC1/STBY SPLY 22CE 121VU 121VU 121VU 121VU 121VU 121VU 122VU 122VU
ENGINE/IGN/ENG2/SYS B ENGINE/IGN/ENG1/SYS B ENGINE/IGN/ENG2/SYS A BAT ENGINE/IGN/ENG1/SYS A BAT FLIGHT CONTROLS/SEC3/SPLY FLIGHT CONTROLS/SEC2/SPLY LIGHTING/INSTL LT/MAIN INST/PNL AND/PED LIGHTING/FLOOD/CTR INST/PNL
3JH2 3JH1 2JH2 2JH1 21CE3 21CE2 4LF 2LE
Subtask 76-11-17-869-052
B. Make sure that the throttle control levers are at idle (0 degree). Subtask 76-11-17-941-053 C. Safety Precautions (1) Put a warning notice in the cockpit to tell persons not to - the throttle control levers - the slat and flap control levers. (2) On the panel 50VU: to vote on thisGND title PWR/1(2) - Make sure that the ON legend of Sign the upENG/FADEC pushbutton switch is off. Useful Not useful - Install a warning notice.
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C F M 56-5B Subtask 76-11-17-010-052 D. Get Access (1) Open the access door 811. (2) Put an access platform. Subtask 76-11-17-010-055 E. Get Access (1) Remove the Multipurpose Control and Display Units 3CA1 and (Ref. TASK 22-82-12-000-001).
(2) Remove the Radio Management Panels 1RG1 and 1RG2 (Ref. TASK 000-001).
(3) Remove the Audio Control Panels 2RN1 and 2RN2 (Ref. TASK 23-51 000-001).
(4) Remove the Weather Radar Control Unit 3SQ (Ref. TASK 34-41-12001). (5) Remove the ATC Control Unit 3SH (Ref. TASK 34-52-12-000-001). (6) Remove the FLOOD LT/INTEG LT panel 111VU and FLOOD LT panel (Ref. Fig. 401/TASK 76-11-17-991-908)
NOTE ____ : The removal procedure is the same for the FLOOD LT/INTE panel 111VU and FLOOD LT panel 112VU. (a) Release the fasteners of the panel (1) and disengage the (1) from its housing. (b) Disconnect the connector (3) from the panel (1). Sign up to vote on this title
(c) Remove the panel (1).
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(d) Put blanking caps on the connectors (2) and (3).
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C F M 56-5B
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C F M 56-5B (9) Disconnect the clamps (9). (10) Remove the screws (6) and the washers (5). (Ref. Fig. 402/TASK 76-11-17-991-909) (11) Remove the plates (4) and (10).
4. Procedure _________ Subtask 76-11-17-480-052
A. Install the RIGGING PIN (98DNSA20206080) (11) in the throttle con unit (Ref. Fig. 402/TASK 76-11-17-991-909) Subtask 76-11-17-020-051 B. Remove the Throttle Control Artificial Feel Unit as follows: (1) Remove and discard the 4 cotter pins (13) (Ref. Fig. 403/TASK 76-11-17-991-910) (2) Remove the 4 nuts (14), the 4 washers (15) and the 4 bolts sure that the 4 bushes (16) stay bonded. (3) Remove the rods (27). (4) Remove and discard the 4 cotter pins (18). (5) Remove the 2 nuts (19), the 2 washers (20) and the 2 bolts sure that the 2 bushes (25) stay bonded. (6) Remove the 2 nuts (21), the 2 washers (22) and the 2 bolts (7) Remove the throttle control artificial feel unit (23). Sign up to vote on this title
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C F M 56-5B
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C F M 56-5B
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C F M 56-5B TASK 76-11-17-400-042 Installation of the Throttle Control Feel Unit
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
R
----------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------------No specific No specific 98DNSA20206080 98DNSA20208080 98D76103000000
warning notice access platform 1.8 m (5 ft. 11 in.) 1 RIGGING PIN 1 RIGGING PIN 1 THROTTLE LEVER LOAD MEASURE
B. Consumable Materials
----------------------------------------------------------------------REFERENCE DESIGNATION -----------------------------------------------------------------------
Material No.
CP2188
* loctite 675 (Ref. 70-30-00)
C. Expendable Parts
----------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ---------------------------------------------------------------------- Sign up to vote on this title
13 18
cotter pins cotter pins
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C F M 56-5B D. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION -----------------------------------------------------------------------
22-82-12-000-001 22-82-12-400-002 22- 82-12-400-002 23-13-13-000-001 23-13-13-400-001 23-51-12-000-001 23-51-12-400-001 34-41-12-000-001 34-41-12-400-001 34-52-12-000-001 34-52-12-400-001 76-11-00-820-044 76-11-00-820-045 76-11-17-991-908 76-11-17-991-909 76-11-17-991-910 76-11-17-991-911
Removal of the MCDU (3CA1,3CA2,3CA3) Installation of the MCDU (3CA1,3CA2,3CA3) Removal of the Radio Management Panel (CRMP) 1RG2, 1RG3) Installation of the Radio Management Panel (1RG1, 1RG2, 1RG3) Removal of the Audio Control Panel (ACP) (2RN1 2RN3, 2RN4, 2RN5) Installation of the Audio Control Panel (ACP) 2RN2, 2RN3, 2RN4, 2RN5) Removal of the Weather Radar Control Unit (3SQ Installation of the Weather Radar Control Unit Removal of the ATC/TCAS Control Unit (3SH) Installation of the ATC/TCAS Control Unit (3SH Adjustment of the Mechanical Linkage Adjustment of the Artificial Feel Unit Fig. 401 Fig. 402 Fig. 403 Fig. 404
3. Job __________ Set-up Subtask 76-11-17-860-051 A. Aircraft Maintenance Configuration
(1) In the cockpit, make sure that the warning notice is in positi tell persons not to move: - the trottle control levers - the slat and flap control leversSign up to vote on this title
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(2) On the center pedestal, on the ENG panel 115VU, make sure tha warning notice is in position to tell persons not to start
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C F M 56-5B (4) Make sure that the access platform is in position. (5) Make sure that the MCDU 3CA1 and 3CA2 are removed (Ref. TASK 12-000-001). (6) Make sure that the Radio Management Panels 1RG1 and 1RG2 are (Ref. TASK 23-13-13-000-001).
(7) Make sure that the Audio Control Panels 2RN1 and 2RN2 are rem (Ref. TASK 23-51-12-000-001). (8) Make sure that the Weather Radar Control Unit 3SQ is removed (Ref. TASK 34-41-12-000-001).
(9) Make sure that the ATC Control Unit 3SH is removed (Ref. TASK 12-000-001). (10) Make sure that the FLOOD LT/INTEG LT panel 111VU and FLOOD 112VU are removed. (11) Make sure that the plates are removed. Subtask 76-11-17-010-056 B. Make sure that the access door 811 is open. Subtask 76-11-17-865-057
R R
C. Make sure that this(these) circuit breaker(s) is(are) open, safeti safet tagged
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 Sign up to vote on this title 49VU LIGHTING/EMER LT/CKPT/DOME 1LE 105VU FLT CTL/SEC1/STBY SPLY Useful Not useful 22CE 121VU ENGINE/IGN/ENG2/SYS B
3JH2
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C F M 56-5B 4. Procedure _________ (Ref. Fig. 404/TASK 76-11-17-991-911) Subtask 76-11-17-420-051 A. Install the Throttle Control Artificial Feel Unit as follows: (1) Install the throttle control artificial feel unit (23). (2) Install the 2 bolts (24), 2 washers (22) and 2 nuts (21).
(3) If necessary bond the bushes (25) on the bolts (26) with locti (Material No. CP2188).
(4) Install the 2 bolt assemblies (26), the 2 washers (20) and (19). (5) Tighten the 4 nuts. (6) Install 4 new cotter pins (18). (7) Install the 4 rods (27). (8) If necessary bond the 4 bushes (16) on the 4 bolts (17) with 675 (Material No. CP2188).
(9) Install the 4 bolt assemblies (17), the 4 washers (15) and (14). (10) Tighten the 4 nuts. Subtask 76-11-17-820-052 B. Adjustment of the mechanical linkage:
R
Sign upand to vote on this the title rigging (1) Make sure that you can easily install remove RIGGING PIN (98DNSA20208080) (12) inUseful the artificial Not useful feel unit (Ref. Fig. 403/TASK 76-11-17-991-910)
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C F M 56-5B
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C F M 56-5B (2) Make sure that you can easily install and remove the rigging RIGGING PIN (98DNSA20206080) (11) in the throttle control unit (Ref. Fig. 403/TASK 76-11-17-991-910) (a) If you cannot do this, adjust the length of the rod (Ref. 76-11-00-820-044). Subtask 76-11-17-420-054 C. Install 4 news cotter pins (13). Subtask 76-11-17-080-052
D. Remove the rigging pin (12) from the artificial feel unit and the pin (11) from the throttle control unit. Subtask 76-11-17-480-053 E. Install the THROTTLE LEVER LOAD MEASURE (98D76103000000) on the control levers. Subtask 76-11-17-820-053 F. Adjustment of the Artificial Feel Unit:
(1) Measure the value necessary to move the throttle control lever between the IDLE STOP and the MAX CLIMB. (a) This value must be 0.8 +0.1 -0 daN (1.8 +0.2 -0 lbf).
R
NOTE ____ : Measure this value in the IDLE STOP to MAX CLIMB not measure this value at the hard point where the increases suddenly. (2) Measure the value necessary to move to more than MAX CLIMB point. Sign up to vote on this title
Useful useful-0 lbf). (a) This value must be 2.5 +0.1 -0 (5.62 +0.22 daN Not
(3) If you do not get these values, adjust the artificial feel
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C F M 56-5B 5. Close-up ________ Subtask 76-11-17-410-052 A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) items. (2) Install the plates (4) and (10). (Ref. Fig. 402/TASK 76-11-17-991-909) (3) Install the washers (5) and the screws (6). (4) Install the clamps (9). (5) Install the ventilation plates (8). (6) Install the screws (7). (7) Install the FLOOD LT/INTEG LT panel 111VU and FLOOD LT panel (Ref. Fig. 401/TASK 76-11-17-991-908)
NOTE ____ : The installation procedure is the same for the FLOOD LT panel 111VU and FLOOD LT panel 112VU. (a) Remove the blanking caps from the connectors (2) and (3). (b) Install the connector (2) on the panel (1). (c) Install the panel (1) on the structure. (d) Fully tighten the fasteners on the panel (1). (8) Install the Multipurpose Control and Display Units (3CA1 and (Ref. TASK 22-82-12-400-002). Sign up to vote on this title
useful (Ref. TAS (9) Install the Radio Management Panels (1RG1 andNot 1RG2) Useful 13-400-001).
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C F M 56-5B Subtask 76-11-17-410-053 B. Close Access (1) Remove the access platform(s). (2) Close the access door 811 (3) Remove the warning notice(s). Subtask 76-11-17-865-058
C. Remove the safety clip(s) and the tag(s) and close this(these) breaker(s): 1JH, 2JH1, 2JH2, 3JH1, 3JH2, 21CE1, 21CE2, 21CE3, 22CE, 1LE, 2LE, Subtask 76-11-17-710-052 D. Do an operational test of the panels FLOOD LT/INTEG LT PNL 111VU FLOOD LT PNL 112VU:
(1) operate the light adjustment knobs of the panels FLOOD LT/INTE PNL 111VU and FLOOD LT PNL 112VU. (2) Make sure that the light intensity of the glareshield panels F/O glareshield panel 130VU, captain glareshield panel 131VU, overhead CTL & IND panel 48VU changes.
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C F M 56-5B CONTROL __________________________________________________________ UNIT - THROTTLE (8KS1,8KS2) - REMOVAL/INSTALLATION REMOVAL/INSTALLAT ION TASK 76-11-19-000-042 Removal of the Throttle Control Unit (8KS1, 8KS2)
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION -----------------------------------------------------------------------
R
No specific No specific 98DNSA20208080
blanking caps access platform 1.5 m (4 ft. 11 in.) 1 RIGGING PIN
B. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------76-11-19-991-908 76-11-19-991-909 76-11-19-991-910
Fig. 401 Fig. 402 Fig. 403
3. Job __________ Set-up Subtask 76-11-19-865-057
Sign up to vote on this title A. Make sure that this(these) circuit breaker(s) is(are) closed:
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----------------------------------------------------------------------PANEL DESIGNATION IDENT.
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C F M 56-5B Subtask 76-11-19-010-051 B. Get Access (1) Put the access platform (2) Open the access door 811 Subtask 76-11-19-869-056
C. Make sure that the throttle control levers are set to idle (0 deg TLA).
4. Procedure _________
(Ref. Fig. 401/TASK 76-11-19-991-908, 402/TASK 76-11-19-991-909, 403 76-11-19-991-910) Subtask 76-11-19-020-055 A. Disconnect Connectors (1) Disconnect the four connectors (12). (2) Put blanking caps on the disconnected electrical connectors. Subtask 76-11-19-480-052
R
B. Install the RIGGING PIN (98DNSA20208080) (13) in the artificial of the throttle control. Subtask 76-11-19-020-051 C. Removal of the Throttle Control Unit. (1) Remove and discard the cotter pin (5).
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Useful Not useful (2) Remove the nut (6), the washer (7) the bolt (2). Make sur and the bush (3) stays bonded to the bolt (2).
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C F M 56-5B
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C F M 56-5B
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Airbus A320 Operation
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C F M 56-5B
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C F M 56-5B TASK 76-11-19-400-042 Installation of the Throttle Control Unit (8KS1, 8KS2)
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------------No specific 98DNSA20206080
access platform 1.5 m (4 ft. 11 in.) 1 RIGGING PIN
B. Consumable Materials
----------------------------------------------------------------------REFERENCE DESIGNATION -----------------------------------------------------------------------
Material No.
CP2188
* Loctite 675 (Ref. 70-30-00)
C. Expendable Parts
----------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ----------------------------------------------------------------------5 8
cotter pin cotter pins
76-11-01 76-11-01
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C F M 56-5B D. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------24-41-00-861-002 24-41-00-862-002 27-96-00-740-001 31-60-00-860-001 31-60-00-860-002 76-11-00-820-044 76-11-19-991-908 76-11-19-991-909 76-11-19-991-910
R R
29-HYDRAULIC
Energize the Aircraft Electrical Circuits from External Power De-energize the Aircraft Electrical Circuits from the External Power BITE Test of the EFCS (Ground Scanning) EIS Start Procedure EIS Stop Procedure Adjustment of the Mechanical Linkage Fig. 401 Fig. 402 Fig. 403
**ON A/C 201-225, 227-227, 229-299, 426-455, 476-499, 503-549, 551-599, 701-749, 76-11-19-991-911
Fig. 404
**ON A/C 456-475, 76-11-19-991-911-A
Fig. 404A
**ON A/C ALL 3. Job __________ Set-up Subtask 76-11-19-860-052 A. Aircraft Maintenance Configuration
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Useful (1) Make sure that the access platform in position. is Not useful
(2) Make sure that the throttle control levers are set to idle
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C F M 56-5B
INTENTIONALLY BLANK
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C F M 56-5B Subtask 76-11-19-865-058
C. Make sure that this(these) circuit breaker(s) is(are) open, safeti safet tagged
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 105VU FLT CTL/SEC1/STBY SPLY 22CE 121VU FLIGHT CONTROLS/SEC3/SPLY 121VU FLIGHT CONTROLS/SEC2/SPLY
21CE3 21CE2
Subtask 76-11-19-869-057 D. Inspection of the bolt (1) Make sure that the bush (3) is correctly bonded to the bolt (2) If necessary, bond the bush (3) to the bolt (2) with Loctite (Material No. CP2188) 4. Procedure _________
(Ref. Fig. 401/TASK 76-11-19-991-908, 402/TASK 76-11-19-991-909, 403 76-11-19-991-910) Subtask 76-11-19-420-051 A. Installation of the Throttle Control Unit. (1) Remove all the blanking caps from the connectors.
(2) Install the throttle control unit 8KS1 (8KS2) (11) on its sup
Sign washers up to vote on this title (3) Install the three bolts (1) with the (10) and the nut Tighten the bolts (1). Useful Not useful
(4) Install the three new cotter pins (8)
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C F M 56-5B Subtask 76-11-19-820-052 B. Make sure that you can easily install and remove the rigging pin PIN (98DNSA20206080) (14). If not adjust the rod (12) (Ref. TASK 00-820-044) Subtask 76-11-19-420-055 C. Install cotter pin and connectors (1) Install a new cotter pin (5).
(2) Connect the four electrical connectors (12). Tighten electrica connector fingertight plus one-eight turn using soft nose plie Subtask 76-11-19-080-052 D. Remove the rigging pin (13) from the artificial feel unit. Subtask 76-11-19-865-060
E. Remove the safety clip(s) and the tag(s) and close this(these) breaker(s): 21CE1, 21CE2, 21CE3, 22CE Subtask 76-11-19-861-051
F. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861Subtask 76-11-19-869-058 G. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (upper ECAM DU only) (Ref. TASK 860-001).
to vote on thisGND title PWR 1 and (2) On the panel 50VU, make sure that Sign theupENG FADEC useful pushbutton switches are released (ONUseful LEGENDS COME ON). Not
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C F M 56-5B Subtask 76-11-19-865-059 H. Make sure that this(these) circuit breaker(s) is(are) closed:
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------FOR 8KS1 49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 FOR 8KS2 49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 121VU ENGINE/ENG2/FADEC B 4KS2 Subtask 76-11-19-710-052 J. Do this test
R R
**ON A/C 201-225, 227-227, 229-299, 426-455, 476-499, 503-549, 551-599, 701-749, (Ref. Fig. 404/TASK 76-11-19-991-911) **ON A/C 456-475, (Ref. Fig. 404A/TASK 76-11-19-991-911-A) 76-11-19-991-911-A ) **ON A/C ALL (1) Open circuit breakers 2KS1, 2KS2
(2) Move the throttle control lever ENG1(2) and make sure that white circle on N1 indication follows the throttle control position. Sign up to vote on this title
(3) Close circuits breakers 2KS1, 2KS2 Useful (4) Open circuit breakers 4KS1, 4KS2
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C F M 56-5B
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C F M 56-5B
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C F M 56-5B (7) Move throttle control lever ENG1(2) and make sure that the white circle on N1 indication follows the throttle control position. Make sure that no warning message shows on the upper DU.
(8) Do the BITE test of the EFCS (Ref. TASK 27-96-00-740-001) and sure that no message related to the throttle control unit 8KS1 shown.
5. Close-up ________ Subtask 76-11-19-869-059 A. Put the aircraft back to its initial configuration.
(1) On the panel 50VU, release the ENG FADEC GND PWR 1 and 2 pushb switches (ON legends goes off). (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002). Subtask 76-11-19-862-051
B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-8 002). Subtask 76-11-19-410-051 C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) items. (2) Close the access door 811 (3) Remove the access platform(s).
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C F M 56-5B LEVER ________________________________________________________ ASSEMBLY - THROTTLE CONTROL - REMOVAL/INSTALLATION REMOVAL/INSTALLATI ON TASK 76-11-41-000-042 Removal of the Throttle Control Lever Assembly
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------------No specific No specific No specific No specific 98DNSA20208120
blanking caps circuit breaker(s) safety clip(s) warning notice access platform 1.8 m (5 ft. 11 in.) 1 RIGGING PIN
B. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION -----------------------------------------------------------------------
R
22-82-12-000-001 23-13-13-000-001 23-51-12-000-001 27-41-41-000-001 34-41-12-000-001 34-52-12-000-001 76-11-41-991-914 76-11-41-991-915
Removal of the MCDU (3CA1,3CA2,3CA3) Removal of the Radio Management Panel (RMP) 1RG2, 1RG3) Removal of the Audio Control Panel (ACP) (2RN1 2RN3, 2RN4, 2RN5) Removal of the Control Mechanism-Pitch Trim Sign up Radar to vote on this title Unit (3SQ Removal of the Weather Control Removal of the ATC/TCAS Unit (3SH) Useful Control Not useful Fig. 401 Fig. 402
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C F M 56-5B 3. Job __________ Set-up Subtask 76-11-41-865-056 A. Open, safety and tag this(these) circuit breaker(s):
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 49VU AUTO FLT/FMGC/1 10CA1 49VU LIGHTING/EMER LT/CKPT/DOME 1LE 105VU FLT CTL/SEC1/STBY SPLY 22CE 121VU AUTO FLT/FMGC/2 10CA2 121VU ENGINE/IGN/ENG2/SYS B 3JH2 121VU ENGINE/IGN/ENG1/SYS B 3JH1 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF 122VU LIGHTING/FLOOD/CTR INST/PNL 2LE Subtask 76-11-41-869-053 B. Make sure that the throttle control levers are at idle (0 degree Subtask 76-11-41-941-053 C. Safety Precautions (1) Put a warning notice in the cockpit to tell persons not to slat and flap control lever. (2) On the center pedestal, on the ENG panel 115VU:
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Useful not (a) Put a warning notice to tell persons to useful start the engi Not
(3) Make sure that the engine 1(2) shutdown occurred not less tha
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C F M 56-5B (b) Put a warning notice to tell persons not to energize the 1(2). Subtask 76-11-41-010-054 D. Get Access (1) Open the access door 811. (2) Put the access platform in position. Subtask 76-11-41-010-055 E. Removal for Access (1) Remove the Multipurpose Control and Display Units 3CA1 and (Ref. TASK 22-82-12-000-001).
(2) Remove the Radio Management Panels 1RG1 and 1RG2 (Ref. TASK 000-001).
(3) Remove the Audio Control Panels 2RN1 and 2RN2 (Ref. TASK 23-51 000-001).
(4) Remove the Weather Radar Control Unit 3SQ (Ref. TASK 34-41-12001). (5) Remove the ATC Control Unit 3SH (Ref. TASK 34-52-12-000-001). (6) Remove the FLOOD LT/INTEG LT panel 111VU and FLOOD LT panel (Ref. Fig. 401/TASK 76-11-41-991-914)
NOTE ____ : The removal procedure is the same for the FLOOD LT/INTE panel 111VU and FLOOD LT panel 112VU. (a) Release the fasteners of the panel (1) and disengage the Sign up to vote on this title (1) from its housing.
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(b) Disconnect the connector (3) from the panel (1).
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C F M 56-5B
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C F M 56-5B (9) Disconnect the clamps (9). (10) Remove the screws (6) and the washers (5). (Ref. Fig. 402/TASK 76-11-41-991-915) (11) Remove the plates (4) and (10).
(12) Remove the pitch trim control mechanism (Ref. TASK 27-41-41-00 4. Procedure _________
(Ref. Fig. 402/TASK 76-11-41-991-915, 403/TASK 76-11-41-991-916, 404 76-11-41-991-917, 405/TASK 76-11-41-991-918, 406/TASK 76-11-41-991-91 Subtask 76-11-41-480-052 A. Install the rigging pin RIGGING PIN (98DNSA20208120) (11) in the artificial feel unit. R
**ON A/C 201-205, 227-227, 229-237, 276-281, 476-478, Subtask 76-11-41-020-051 B. Removal of the Throttle Control Lever Assembly (1) Remove and discard the 2 cotter pins (30). (2) Remove the 2 nuts (31), 2 washers (32) and 2 bolts (34). Make that the 2 bushes (33) stay bonded. (3) Remove the links. (4) Remove the 2 screws (23) and the index (22). (5) Remove the 2 screws (14) and the index (16).
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(6) Remove the screw (28) and the hollow pin (24). Useful Not useful (7) Drive out the pin (26). Remove the link (25) and the trigger
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C F M 56-5B (11) Remove the 5 screws (85).
(12) Lift the lighted label (86) and disconnect the connector 21LFA (13) Remove the lighted label (86). (14) Remove the 3 screws (17) and the 3 screws (20). (15) Remove the housing (18). (16) Remove and discard the 8 cotter pins (43). (17) Remove the 8 nuts (44), the 8 washers (45) and the 8 screws (18) Remove 2 forward covers (63) and the 2 aft covers (42). (19) Remove and discard the cotter pin (72).
(20) Remove the washer (73), the nut (74), the bearing (60) the (61), the screw (64), the bushing (66), the bearing (65) and (25). (21) Drive out the pin (59) and remove the rocker (57).
(22) Remove the screw (76), the washers (78) and (79) and the 2 (77).
(23) Remove the screws (80), the washers (81) and (83) and the cla (82). (24) Disconnect the connectors 2145VC and 2146VC. (25) Put blanking caps on the disconnected electrical connectors. (26) Cut and remove the lockwire. up to vote on this title (27) Remove the nut (37) and the washerSign (38).
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(28) Pull smoothly the shaft (54) to remove:
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C F M 56-5B (e) the bushing (53), (29) Remove the shaft (54).
(30) On the bellcrank (41), remove the ball bearing (40), the space and the bearing (48).
(31) On the bellcrank (55) remove the bearing (50), the spacer (51 the bearing (52). R R R
**ON A/C 201-204, 206-225, 227-227, 229-299, 426-499, 503-549, 551-599, 701-749, Post SB 76-1004 For A/C 201-204,227-227,229-237,276-281,476-4 201-204,227-227,2 29-237,276-281,476-478, 78, Subtask 76-11-41-020-051-A B. Removal of the Throttle Control Lever Assembly (1) Remove and discard the 2 cotter pins (30). (2) Remove the 2 nuts (31), 2 washers (32) and 2 bolts (34). Make that the 2 bushes (33) stay bonded. (3) Remove the links. (4) Remove the 2 screws (23) and the index (22). (5) Remove the 2 screws (14) and the index (16). (6) Remove the screw (28) and the hollow pin (24). (7) Drive out the pin (26). Remove the link (25) and the trigger (8) Remove the 2 screws (15) and the 2 hollow pins (13).
(9) Remove the lever (29): pull the lever to disconnect the connec Sign up to vote on this title located inside, at the lever-to-bellcrank junction.
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(10) Remove the lever (12): do the same procedure as for the lever
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C F M 56-5B (15) Remove the housing (18).
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(16) Remove and discard the 8 cotter pins (43). (17) Remove the 8 nuts (44), the 8 washers (45) and the 8 screws (18) Remove 2 forward covers (63) and the 2 aft covers (42). (19) Remove and discard the cotter pin (72).
(20) Remove the washer (73), the nut (74), the roller (60) the bus (61), the screw (64), the bushing (66), the roller (65) and (25). (21) Drive out the pin (59) and remove the rocker (57).
(22) Remove the screw (76), the washers (78) and (79) and the 2 (77).
(23) Remove the screws (80), the washers (81) and (83) and the cla (82). (24) Disconnect the connectors 2145VC and 2146VC. (25) Put blanking caps on the disconnected electrical connectors. (26) Cut and remove the lockwire. (27) Remove the nut (37) and the washer (38). (28) Pull smoothly the shaft (54) to remove: (a) the bushing (39), (b) the bellcrank (41), (c) the adjustment bushing (49), Sign up to vote on this title
(d) the bellcrank (55),
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C F M 56-5B (31) On the bellcrank (55) remove the bearing (50), the spacer (51 the bearing (52).
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C F M 56-5B **ON A/C ALL TASK 76-11-41-400-042 Installation of the Throttle Control Lever Assembly
1. Reason __________________ for the Job Self Explanatory 2. Job ______________________ Set-up Information A. Fixtures, Tools, Test and Support Equipment
----------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------------No specific No specific No specific
warning notice access platform 1.8 m (5 ft. 11 in.) Torque Wrench : range 1.00 to 10.00 m.daN (8.00 to 75.00 lbf.f 1 RIGGING PIN
98DNSA20208120
B. Consumable Materials
----------------------------------------------------------------------REFERENCE DESIGNATION -----------------------------------------------------------------------
Material No.
CP8001
Material No.
CP8002
Material No. 08-007A R R
Material No. 08-029
* lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-0 * lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-0
Sign up to vote on this title SEALANT, HIGH TEMP. (Ref. 20-31-00) Not useful USA ASTM D 5363 Useful GROUP 4 2 GRADE 1 CLASS THREADLOCKER (Ref. 20-31-00)
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C F M 56-5B C. Expendable Parts
----------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN ----------------------------------------------------------------------30 30 40 40 43 43 48 48 49 49 50 50 72 72
cotter pins cotter pins bearing bearing cotter pins cotter pins bearing bearing adjustment bushing adjustment bushing bearing bearing cotter pins cotter pins
76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01 76-11-01
D. Referenced Information
----------------------------------------------------------------------REFERENCE DESIGNATION -----------------------------------------------------------------------
22-82-12-000-001 22-82-12-400-002 22- 82-12-400-002 22-96-00-710-001 22-97-00-710-001 R 23-13-13-000-001 R
23-13-13-400-001 23-51-12-000-001 23-51-12-400-001 24-41-00-861-002
Removal of the MCDU (3CA1,3CA2,3CA3) Installation of the MCDU (3CA1,3CA2,3CA3) Operational Test of the AFS Operational Test of the LAND CAT III Capabilit Removal of the Radio Management Panel (RMP) 1RG2, 1RG3) Installation of the Radio Management Panel (1RG1, 1RG2, 1RG3) Removal of the Audio Control Panel (ACP) (2RN1 Sign up to vote on this title 2RN3, 2RN4, 2RN5) Installation of the Audio Control Panel (ACP) Useful Not useful 2RN2, 2RN3, 2RN4, 2RN5) Energize the Aircraft Electrical Circuits from
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C F M 56-5B ----------------------------------------------------------------------REFERENCE DESIGNATION ----------------------------------------------------------------------34-41-12-000-001 34-41-12-400-001 34-52-12-000-001 34-52-12-400-001 76-11-41-991-914 76-11-41-991-915 76-11-41-991-916 76-11-41-991-917 76-11-41-991-918 76-11-41-991-919 76-11-41-991-920
Removal of the Weather Radar Control Unit (3SQ Installation of the Weather Radar Control Unit Removal of the ATC/TCAS Control Unit (3SH) Installation of the ATC/TCAS Control Unit (3SH Fig. 401 Fig. 402 Fig. 403 Fig. 404 Fig. 405 Fig. 406 Fig. 407
3. Job __________ Set-up Subtask 76-11-41-865-057
A. Make sure that this(these) circuit breaker(s) is(are) open, safeti safet tagged
----------------------------------------------------------------------PANEL DESIGNATION IDENT. ----------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY CONTROLS/SEC1/NORM /SPLY 21CE1 49VU AUTO FLT/FMGC/1 10CA1 49VU LIGHTING/EMER LT/CKPT/DOME 1LE 105VU FLT CTL/SEC1/STBY SPLY 22CE 121VU AUTO FLT/FMGC/2 10CA2 121VU ENGINE/IGN/ENG2/SYS B 3JH2 121VU ENGINE/IGN/ENG1/SYS B 3JH1 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 Sign up to vote on this title 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 121VU FLIGHT CONTROLS/SEC2/SPLY Useful Not useful 21CE2 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF 122VU LIGHTING/FLOOD/CTR INST/PNL 2LE
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C F M 56-5B Subtask 76-11-41-860-051 B. Aircraft Maintenance Configuration
(1) Make sure that a warning notice is in the cockpit to tell per to move the slat and flap control lever.
(2) On the center pedestal, on the ENG panel 115VU, make sure tha warning notice is in position to tell persons not to start engine. (3) On the overhead maintenance panel 50VU, make sure that the of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make that a warning notice is in position to tell persons not to the FADEC 1(2). (4) Make sure that the access platform is in position. Subtask 76-11-41-010-057 C. Get Access (1) Make sure that the access door 811 is open.
(2) Make sure that the Multipurpose Control and Display Units 3CA 3CA2 are removed (Ref. TASK 22-82-12-000-001). 22-82-12-000-001) . (3) Make sure that the Radio Management Panels 1RG1 and 1RG2 are (Ref. TASK 23-13-13-000-001).
(4) Make sure that the Audio Control Panels 2RN1 and 2RN2 are rem (Ref. TASK 23-51-12-000-001). (5) Make sure that the Weather Radar Control Unit 3SQ is removed (Ref. TASK 34-41-12-000-001).
Sign3SH up tois vote on this title(Ref. TASK (6) Make sure that the ATC Control Unit removed 12-000-001). Useful Not useful
(7) Make sure that the FLOOD LT/INTEG LT panel 111VU and FLOOD
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C F M 56-5B (9) Make sure that the RIGGING PIN (98DNSA20208120) (11) is instal the artificial feel unit. (Ref. Fig. 403/TASK 76-11-41-991-916)
4. Procedure _________
(Ref. Fig. 402/TASK 76-11-41-991-915, 403/TASK 76-11-41-991-916, 404 76-11-41-991-917, 405/TASK 76-11-41-991-918, 406/TASK 76-11-41-991-91 407/TASK 76-11-41-991-920) R
**ON A/C 201-205, 227-227, 229-237, 276-281, 476-478, Subtask 76-11-41-420-056
A. Preparation before Installation of the Throttle Control Lever Ass (1) On the bellcrank (55), install a new bearing (50). (2) On the bellcrank (41), install a new bearing (40), the spacer and a new bearing (48). (3) Engage the shaft (54) and push it. At the same time install: (a) the bushing (53), (b) the bellcrank (55), (c) the adjustment bushing (49), (d) the bellcrank (41), (e) the bushing (39). (4) Push the shaft (54) and install the washer (38) and the nut
Sign 4 up m.daN to vote on this title and 29.49 (5) TORQUE the nut (37) to between 3 and (22.12 lbf.ft). Useful Not useful
(6) Wirelock the nut (37) with lockwire 0.032 in. (0.8 mm) dia.
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C F M 56-5B
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C F M 56-5B (9) Install the clamps (82), the washers (81) and (83) and the (80).
(10) Install the clamps (77), the washers (78) and (79) and the (76).
(11) Install the rocker (57) and the pin (59).
(12) Install the link (25), the bearing (65), the bushing (66), (64), the bushing (61), the bearing (60), the washer (73) and (74). (13) Install 2 new cotter pins (72). (14) Install the 2 forward covers (63) and the 2 aft covers (42). (15) Install the 8 screws (46), the 8 washers (45) and the 8 nuts (16) Install 8 new cotter pins (43).
R R R
**ON A/C 201-204, 206-225, 227-227, 229-299, 426-499, 503-549, 551-599, 701-749, Post SB 76-1004 For A/C 201-204,227-227,229-237,276-281,476-4 201-204,227-227,2 29-237,276-281,476-478, 78, Subtask 76-11-41-420-056-A
A. Preparation before Installation of the Throttle Control Lever Ass (1) On the bellcrank (55), install a new bearing (50). (2) On the bellcrank (41), install a new bearing (40), the spacer and a new bearing (48). (3) Engage the shaft (54) and push it. At the same time install: (a) the bushing (53), (b) the bellcrank (55), (c) the adjustment bushing (49),
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C F M 56-5B (6) Wirelock the nut (37) with lockwire 0.032 in. (0.8 mm) dia. No. CP8001) or lockwire 0.032 in. (0.8 mm) dia. (Material No. CP8002).
(7) Remove the blanking caps from the connectors 2145VC and 2146VC (8) Connect the connectors 2145VC and 2146VC.
(9) Install the clamps (82), the washers (81) and (83) and the (80).
(10) Install the clamps (77), the washers (78) and (79) and the (76). (11) Install the rocker (57) and the pin (59).
(12) Install the link (25), the roller (65), the bushing (66), the (64), the bushing (61), the roller (60), the washer (73) and (74). (13) Install 2 new cotter pins (72). (14) Install the 2 forward covers (63) and the 2 aft covers (42). (15) Install the 8 screws (46), the 8 washers (45) and the 8 nuts (16) Install 8 new cotter pins (43). **ON A/C ALL Subtask 76-11-41-220-052
B. Make sure there is a minimum clearance of 3 mm (0.12 in.) between screws (64) and the 8 screws (46). If not, install a new adjustmen bushing (49). Sign up to vote on this title
Subtask 76-11-41-420-052
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C. Installation of the Throttle Control Lever Assembly
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C F M 56-5B (6) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-007A) screws (15).
R
(7) Install the 2 screws (15) and the 2 hollow pins (13).
R
(8) Assemble the trigger (27) and the link (25) with the pin (26).
R
(9) Engage the trigger (27) in the lever (29) and install the hol (24) and the screw (28).
R
(10) Install the index (16) and the 2 screws (14).
R
(11) Install the index (22) and the 2 screws (23).
R
(12) Put the two control levers in the idle position (0 degree TLA engage the two links.
R
(13) If necessary install 2 new bushings (33) on the screws (34) them with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-029)
R
(14) Install the 2 screws (34), the 2 washers (32) and the 2 nuts
R
(15) Install 2 new cotter pins (30). Subtask 76-11-41-080-052 D. Remove the rigging pin (11) from the artificial feel unit.
5. Close-up ________ Subtask 76-11-41-410-054 A. Close Access
(1) Install the pitch trim control mechanism (Ref. TASK 27-41-41-4 001). Sign up to vote on this title
(2) Install the plates (4) and (10). Useful (Ref. Fig. 402/TASK 76-11-41-991-915)
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C F M 56-5B (7) Install the FLOOD LT/INTEG LT panel 111VU and FLOOD LT panel (Ref. Fig. 401/TASK 76-11-41-991-914) NOTE ____ : The installation procedure is the same for the panels LT/INTEG LT panel 111VU and FLOOD LT panel 112VU. (a) Remove the blanking caps from the connectors (2) and (3). (b) Install the connector (3) on the panel (1). (c) Install the panel (1) on the structure. (d) Fully tighten the fasteners on the panel (1). (8) Install the Multipurpose Control and Display Units (3CA1 and (Ref. TASK 22-82-12-400-002).
(9) Install the Radio Management Panels (1RG1 and 1RG2) (Ref. TAS 13-400-001).
(10) Install the Audio Control Panels (2RN1 and 2RN2) (Ref. TASK 400-001).
(11) Install the Weather Radar Control Unit (3SQ) (Ref. TASK 34-41001).
(12) Install the ATC Control Unit (3SH) (Ref. TASK 34-52-12-400-001 Subtask 76-11-41-410-055 B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) items. (2) Close the access door 811. (3) Remove the access platform(s). (4) Remove the warning notice(s).
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C F M 56-5B Subtask 76-11-41-861-051
D. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861Subtask 76-11-41-710-052 E. Do an operational test of the FLOOD LT/INTEG LT panel 111VU and panel 112VU: (1) Operate the light adjustment knobs of the FLOOD LT/INTEG LT 111VU and FLOOD LT panel 112VU.
(2) Make sure that the light intensity of the glareshield panel glareshield panel 130VU, CAPT glareshield panel 131VU and over control and indicating panel 48VU changes. Subtask 76-11-41-869-057 F. DO the EIS start procedure (Ref. TASK 31-60-00-860-001). Subtask 76-11-41-710-054 G. Do the test that follows:
(1) Move the ENG1 and ENG2 throttle control levers from MAX REV T/O.
(a) On the upper ECAM DU, make sure that the small white circl the N1 indication follows the throttle control lever posit (b) Make sure that the movement is smooth, without friction
(2) Do an operational test of the AFS (Ref. TASK 22-96-00-710-001) R R
NOTE ____ : If the aircraft is operated in cat 3 conditions, do CAT 3 capability test (Ref. TASK 22-97-00-710-001). Sign up to vote on this title
Subtask 76-11-41-869-058
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H. DO the EIS stop procedure (Ref. TASK 31-60-00-860-002).
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C F M 56-5B ENGINE _________________________________________________ MASTER CONTROL - DESCRIPTION AND OPERATION
1. HP ______________________________ Fuel Shut OFF Valve Control
A. General (Ref. Fig. 001) The HP fuel shutoff valve control is fully electrical (the HP shu valve is a part of the HMU described in Ref. 73-20-00). It is per from the engine panel in the cockpit as follows : - opening of the HP fuel SOV : it is controlled by the ECU : the ECU receives the commands from ENG/MASTER control switch and ENG/MODE/CRANK/NORM/IGN ENG/MODE/CRANK/NO RM/IGN START sele switch. - closure of the HP fuel SOV : it is controlled directly from the ENG/MASTER control switch position (Ref. 73-20-00 and 80-00-00). B. Valve Operation (Ref. Fig. 002) The FADEC control system contains two fuel shut-off means, which through pilot valves to close the pressurizing valve :
(1) A fuel shutoff which is directly hardwired to the ENG/MASTER switch. This solenoid operated pilot valve is powered by the 28VDC. It is closed when powered.
(2) When the main metering valve is positioned below a minimum position : a mechanically operated pilot valve in the HMU clos pressurizing valve. This function is software logic inhibited prevent operation at and above idle operation. The fuel shutoff valve meets the following concepts. - The pressurizing valve does not actuate open with boost pres (even if both pilot valves call for ON) until the HP fuel provides sufficient pressure to open it. - Loss of power supply does not lead to change the selected Sign up to vote on this title shutoff valve position. - When HP fuel shutoff valve is selected (open) a spuri Useful closed Not useful transient voltage to open (close) does not lead to a permane opening (closure) of the fuel valve.
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28-FUEL
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Airbus A320 Operation
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C F M 56-5B
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28-FUEL
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C F M 56-5B
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C F M 56-5B 2. LP ______________________________ Fuel Shut Off Valve Control (Ref. ATA 28)
A. General The function of the LP fuel shutoff valve is to control the fuel at engine-to-pylon interface. The valve is located on the engine supply system in the wing leadi edge.
B. Valve Operation (Ref. Fig. 001) The LP fuel shutoff valve is controlled : - From the cockpit overhead panel by means of the ENG FIRE pushbut switch - From the cockpit center pedestal by means of the ENG/MASTER con switch on engine control panel.
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