設備與裝飾防火燃油液壓防冰防雨

1、CHAPTER26Fire737-600/700/800/900 AIRCRAFT MAINTENANCE MANUALCHAPTER 26FireSubject/PageDateCOCSubject/PageDateCOCEFFECTIVE PAGES26-11-00 (cont.)1 thru 5Oct 15/20135Feb 10/20036BLANK6Oct 10/200226-CONTENTS7Feb 10/20031Oct 15/20098Feb 10/20072Jun 15/20099Feb 10/20033Jun 15/200910Oct 10/20024Jun 15/2009

2、11Oct 10/20025Jun 15/200912Feb 15/20116BLANK13Jun 10/200726-00-0014BLANK1Oct 10/200226-14-002Oct 10/20061Oct 10/20023Jun 15/20122Oct 10/20024Feb 15/20133Feb 10/20035Jun 10/20064Jun 15/20126Jun 10/20065Feb 15/20137Jun 10/20076Jun 15/20128BLANK7Feb 15/201326-11-008Feb 15/20131Oct 10/20029Feb 15/20132O

3、ct 10/200210Feb 15/20133Feb 10/200311Feb 15/20134Oct 10/200212Jun 15/2012A = Added, R = Revised, D = Deleted, O = Overflow, C = Customer Originated Change26-EFFECTIVE PAGESPage 5D633A101-XIABOEING PROPRIETARY - Copyright #- Unpublished Work - See title page forOct 15/2013s.Subject/PageDateCOCSubject

4、/PageDateCOC26-14-00 (cont.)26-16-00 (cont.)13Feb 15/20134Feb 15/201314Oct 15/20095Jun 10/200615Feb 15/20136Jun 10/200616Feb 15/20137Jun 10/2006R17Oct 15/20138Jun 10/200618Jun 15/20129Jun 10/2006A19Oct 15/201310Jun 10/2006A20BLANK11Jun 10/200626-15-0012Jun 10/20061Oct 10/200213Jun 10/20062Oct 10/200

5、214Jun 10/20063Jun 10/200715Jun 10/20064Oct 15/201016Jun 10/20065Jun 10/200717Jun 10/20066Oct 10/200618Feb 15/20137Feb 10/200319Jun 10/20068Oct 10/200620Feb 15/20139Feb 10/200321Jun 10/200610BLANK22Jun 10/200626-16-0023Jun 10/20061Oct 10/200224BLANK2Oct 10/200226-17-003Jun 15/20121Oct 10/2002Subject

6、/PageDateCOCSubject/PageDateCOC26-17-00 (cont.)26-18-00 (cont.)2Oct 10/200212Jun 10/20063Feb 10/200313Jun 15/20124Oct 10/200214Feb 15/20135Feb 10/200726-21-006Oct 10/20021Oct 10/20027Feb 10/20032Oct 10/20028Oct 10/20023Feb 10/20079Feb 10/20034Oct 10/200210Oct 10/20025Feb 10/200311Feb 10/20036Oct 10/

7、200212BLANK7Feb 10/200726-18-008Oct 10/20021Oct 10/20029Feb 10/20032Oct 10/200210Oct 10/20023Feb 10/200311Oct 10/20024Oct 10/200212Oct 10/20025Jun 15/201213Feb 10/20036Feb 15/201314Oct 10/20027Jun 10/200615Feb 10/20038Jun 10/200616Oct 10/20029Jun 10/200617Feb 10/200310Feb 10/200718Oct 10/200211Jun 1

8、0/200619Feb 10/2003Subject/PageDateCOCSubject/PageDateCOC26-21-00 (cont.)26-22-00 (cont.)20BLANK22BLANK26-22-0026-23-001Oct 10/20021Oct 10/20022Oct 10/20062Oct 10/20043Feb 15/20133Jun 15/20124Jun 10/20074Feb 15/20135Feb 10/20055Jun 10/20066Oct 10/20066Jun 10/20067Feb 15/20137Jun 10/20068Jun 10/20078

9、Jun 10/20069Feb 15/20139Jun 15/201210Feb 10/200510Feb 15/201311Feb 15/201311Jun 10/200612Feb 10/200512Jun 10/200613Feb 10/200513Jun 10/200614Feb 10/200514Jun 10/200615Feb 15/201315Jun 15/201216Feb 10/200516Feb 15/201317Feb 10/200517Feb 10/200718Oct 10/200618Jun 15/200819Oct 10/200619Feb 10/200720Oct

10、 10/200620Feb 10/200721Jun 10/200721Feb 10/2007Subject/PageDateCOCSubject/PageDateCOC26-23-00 (cont.)22BLANK26-24-001Oct 10/20022Oct 10/20023Feb 15/20104BLANK26-26-001Oct 10/20022Oct 10/20023Feb 10/20034BLANK737-600/700/800/900 AIRCRAFT MAINTENANCE MANUALCHAPTER 26FireCH-SC-SUSubjectPageEffectivity2

11、6-00-00FIRE- INTRODUCTION2XIA ALL26-00-00FIRE- FIRE ALARMS - FUNCTIONAL DESCRIPTION6XIA ALL26-11-00FIRE- ENGINE FIRE DETECTION - INTRODUCTION2XIA ALL26-11-00FIRE DESCRIPTION- ENGINE FIRE DETECTION - GENERAL4XIA ALL26-11-00FIRE DETECTORS- ENGINE FIRE DETECTION - ENGINE FIRE6XIA ALL26-11-00FIRE- ENGIN

12、E FIRE DETECTION - ENGINE AND APU8XIA ALLFIRE DETECTION MODULE26-11-00FIRE DESCRIPTION- ENGINE FIRE DETECTION - FUNCTIONAL11XIA ALL26-14-00FIRE INTRODUCTION- LAVATORY SMOKE DETECTION -2XIA ALL26-14-00FIRE DESCRIPTION- LAVATORY SMOKE DETECTION - GENERAL4XIA ALL26-14-00FIRE- LAVATORY SMOKE DETECTION -

13、 LAVATORY8XIA ALLSMOKE DETECTOR26-14-00FIRE DESCRIPTION- LAVATORY SMOKE DETECTION - FUNCTIONAL15XIA ALL26-15-00FIRE- APU FIRE DETECTION - INTRODUCTION2XIA ALL26-15-00FIRE- APU FIRE DETECTION - GENERAL DESCRIPTION4XIA ALL26-15-00FIRE- APU FIRE DETECTION - APU FIRE DETECTOR6XIA ALL26-CONTENTSPage 2 Ju

14、n 15/2009D633A101-XIABOEING PROPRIETARY - Copyright #- Unpublished Work - See title page fors.D633A101-XIA26-CONTENTSPage 1 Oct 15/2009CH-SC-SUSubjectPageEffectivity26-15-00FIRE - APU FIRE DETECTION - FUNCTIONAL DESCRIPTION26-16-00FIRE - CARGO COMPARTMENT SMOKE DETECTION - INTRODUCTION26-16-00FIRE -

15、 CARGO COMPARTMENT SMOKE DETECTION - GENERAL DESCRIPTION26-16-00FIRE - CARGO COMPARTMENT SMOKE DETECTION - COMPONENT LOCATION26-16-00FIRE - LWR CARGO COMPARTMENT SMOKE DETECTION - SMOKE DETECTOR26-16-00FIRE - LWR CARGO COMPARTMENT SMOKE DETECTION - CARGO ELECTRONIC UNIT26-16-00FIRE - CARGO COMPARTME

16、NT SMOKE DETECTION - CARGO FIRE CONTROL PANEL26-16-00FIRE - CARGO COMPARTMENT SMOKE DETECTION - FUNCTIONAL DESCRIPTION - LOWER DECK26-16-00FIRE - CARGO COMPARTMENT SMOKE DETECTION - SMOKE DETECTOR TEST26-17-00FIRE - WHEEL WELL OVERHEAT DETECTION - INTRODUCTION26-17-00FIRE - WHEEL WELL OVERHEAT DETEC

17、TION - GENERAL DESCRIPTION26-17-00FIRE - WHEEL WELL OVERHEAT DETECTION - OVERHEAT DETECTOR ELEMENT8XIA ALL2XIA ALL6XIA ALL8XIA ALL10XIA ALL12XIA ALL15XIA ALL18XIA ALL22XIA ALL2XIA ALL4XIA ALL6XIA ALL737-600/700/800/900 AIRCRAFT MAINTENANCE MANUALCHAPTER 26FireCH-SC-SUSubjectPageEffectivity26-CONTENT

18、SPage 5 Jun 15/2009D633A101-XIABOEING PROPRIETARY - Copyright #- Unpublished Work - See title page fors.26-17-00FIRE - WHEEL WELL OVERHEAT DETECTION - COMPARTMENT OVERHEAT DETECTION CONTROLLER26-17-00FIRE - WHEEL WELL OVERHEAT DETECTION - FUNCTIONAL DESCRIPTION26-18-00FIRE - WING AND BODY OVERHEAT D

19、ETECTION - INTRODUCTION26-18-00FIRE - WING AND BODY OVERHEAT DETECTION - GENERAL DESCRIPTION26-18-00FIRE - WING AND BODY OVERHEAT DETECTION - COMPARTMENT OVERHEAT DETECTION CONTROLLER26-18-00FIRE - WING AND BODY OVERHEAT DETECTION - FUNCTIONAL DESCRIPTION26-18-00FIRE - WING AND BODY OVERHEAT DETECTI

20、ON - FUNCTIONAL DESCRIPTION8XIA ALL10XIA ALL2XIA ALL4XIA ALL8XIA ALL10XIA ALL12XIA ALL26-21-00FIRE- ENGINE FIRE EXTINGUISHING - INTRODUCTION2XIA ALL26-21-00FIRE- ENGINE FIRE EXTINGUISHING - OPERATION4XIA ALL26-21-00FIRE BOTTLE- ENGINE FIRE EXTINGUISHING - EXTINGUISHER6XIA ALL26-21-00FIREBOTTLE SQUIB

21、- ENGINE FIRE EXTINGUISHING - EXTINGUISHER8XIA ALL26-21-00FIRE- ENGINE FIRE EXTINGUISHING - OVERHEAT/FIRE11XIA ALLPANEL26-21-00FIRE - ENGINE FIRE EXTINGUISHING - FUNCTIONAL DESCRIPTION14XIA ALLCH-SC-SUSubjectPageEffectivity26-21-00FIRE- ENGINE FIRE EXTINGUISHING - ENGINE AND16XIA ALLAPU FIRE EXTINGU

22、ISHER TEST26-21-00FIRE- ENGINE FIRE EXTINGUISHING - ENGINE EXTIN18XIA ALLTEST - FUNCTIONAL DESCRIPTION26-22-00FIRE - APU FIRE EXTINGUISHING - INTRODUCTION2XIA ALL26-22-00FIRE - APU FIRE EXTINGUISHING - OPERATION6XIA ALL26-22-00FIRE - APU FIRE EXTINGUISHING - APU FIRE EXTINGUISHING BOTTLE9XIA ALL26-2

23、2-00FIRE- APU FIRE EXTINGUISHING - APU FIRE14XIA ALLEXTINGUISHER BOTTLE SQUIB26-22-00FIRECONTROL PANEL- APU FIRE EXTINGUISHING - APU GROUND18XIA ALL26-22-00FIRE DESCRIPTION- APU FIRE EXTINGUISHING - FUNCTIONAL20XIA ALL26-23-00FIRE INTRODUCTION- CARGO COMPT FIRE EXTINGUISHING -2XIA ALL26-23-00FIRE OP

24、ERATION- CARGO COMPT FIRE EXTINGUISHING -6XIA ALL26-23-00FIRE- CARGO COMPT FIRE EXTINGUISHING -8XIA ALLCOMPONENT LOCATION26-23-00FIRE- CARGO COMPT FIRE EXTINGUISHING - FIRE12XIA ALLEXTINGUISHING BOTTLECH-SC-SUSubjectPageEffectivity26-23-00FIRE - CARGO COMPT FIRE EXTINGUISHING - FILTER DRIER26-23-00F

25、IRE - CARGO COMPT FIRE EXTINGUISHING - FUNCTIONAL DESCRIPTION26-23-00FIRE - CARGO COMPT FIRE EXTINGUISHING - CARGO FIRE CONTROL PANEL - SQUIB TEST26-24-00FIRE - LAVATORY FIRE EXTINGUISHING - LAV FIRE EXTING BOTTLE AND TEMP INDICATOR14XIA ALL18XIA ALL20XIA ALL2XIA ALL26-26-00FIRE - PORTABLE FIRE EXTI

26、NGUISHING2XIA ALL737-600/700/800/900 AIRCRAFT MAINTENANCE MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANKBOEING PROPRIETARY - Copyright #- Unpublished Work - See title page fors.D633A101-XIA26-00-00Page 1 Oct 10/2002FIRE - INTRODUCTIONPurposeThe fire systems monitor the airplane for these conditions:* F

27、ire* Smoke* Overheat* Pneumatic duct leaks.Fire/Overheat DetectionThe airplane has these fire/overheat detection systems:* Engine overheat detection* Engine fire detection* APU fire detection* Wheel well fire detection* Wing/Body overheat detection* Cargo compartment smoke detection* Lavatory smoke

28、detection.ExtinguishingThe airplane has these fire extinguishing systems:* Engine* APU* Lavatory* Cargo compartment* Portable fire extinguishers.Abbreviations and Acronyms* adv - advisory* APU - auxiliary power unit* BITE - built in test equipment* det - detector* DV - Distinguished Visitor* E/E - e

29、lectronic equipment* ENG - engine* ext - extinguish* HMU - hydro-mechanical unit* hyd - hydraulic* inop - inoperable* LED - light emitting diodes* LOC - local* lts - lights* maint - maintenance* MD&T - master dim and test* mem - memory* MLG - main landing gear* ovht - overheat* PA - passenger ad

30、dress* ref - reference* rev - reverser* typ - typical* vlv - valve* warn - warning* W/W - wheel well26-00-00-001EFXIA ALLFECTIVITYD633A101-XIA26-00-00Page 2 Oct 10/200626-00-00-001EFFECTIVITYXIA 001-006, 009-011FIRE - INTRODUCTIOND633A101-XIA26-00-00Page 3 Jun 15/201226-00-00-001EFFECTIVITYXIA 012-0

31、15, 801-810, 812-838, 840-999FIRE - INTRODUCTIOND633A101-XIA26-00-00Page 4 Feb 15/2013THIS PAGE IS INTENTIONALLY LEFT BLANKD633A101-XIA26-00-00Page 5 Jun 10/2006FIRE - FIRE ALARMS - FUNCTIONAL DESCRIPTIONPurposeThe fire alarms provide visual and aural indication to the flight crew about a fire in an

32、y of these systems:* Engine 1* Engine 2* APU* Forward cargo compartment* Aft cargo compartment* Main wheel well.Visual and Aural IndicationsWhen there is a fire, these are the visual and aural indications:* Two red FIRE WARN lights on the P7 panel come on* Bell in the aural warning unit comes on* Re

33、d light and horn on alternatly in the right main wheel well come on (APU fire only). (The horn does not come on in flight.)Functional DescriptionWhen there is a fire in the engine, the engine and APU fire detection module provides a ground for the two red FIRE WARN lights and the bell.When there is

34、a fire in the main wheel well, the compartment overheat detection controller provides a ground for the two red FIRE WARN lights and the bell.When there is smoke in the forward or aft cargo compartment, the cargo electronic unit provides a ground for the two red FIRE WARN lights and the bell.The two

35、red FIRE WARN lights, bell, and horn are reset by removal of the ground. The reset is done by a momentary push on one of these:* Left FIRE WARN light* Right FIRE WARN light* Bell cutout switch on P8* Horn cutout switch on the P28 panel.26-00-00-002When there is a fire in the APU, the engine and APU

36、fire detection module provides a ground for the two red FIRE WARN lights and the bell. The same module provides power for the red light and horn on the P28 panel.EFXIA ALLFECTIVITYD633A101-XIA26-00-00Page 6 Jun 10/200626-00-00-002EFXIA ALLFECTIVITYFIRE - FIRE ALARMS - FUNCTIONAL DESCRIPTION26-00-00D

37、633A101-XIAPage 7 Jun 10/2007737-600/700/800/900 AIRCRAFT MAINTENANCE MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANKBOEING PROPRIETARY - Copyright #- Unpublished Work - See title page fors.D633A101-XIA26-11-00Page 1 Oct 10/2002FIRE - ENGINE FIRE DETECTION - INTRODUCTIONPurposeThe engine overheat and fi

38、re detection system uses detectors on the engine. The detectors monitor engines for overheat and fire conditions. When the system senses an overheat or a fire condition, alarm indications operate in the flight compartment. The indications are on the P7 glareshield panel and on the engine and APU fir

39、e control panel. A bell also operates in the flight compartment for an engine fire.EFXIA ALL26-11-00-001FECTIVITYD633A101-XIA26-11-00Page 2 Oct 10/200226-11-00-001EFXIA ALLFECTIVITYFIRE - ENGINE FIRE DETECTION - INTRODUCTION26-11-00D633A101-XIAPage 3 Feb 10/2003FIRE - ENGINE FIRE DETECTION - GENERAL

40、 DESCRIPTIONGeneral DescriptionThese are the components for engine overheat and fire:* Engine overheat/fire detector (loop A and loop B)* Engine and APU fire detection module* Glareshield, P7 panel* Engine and APU fire control panel* Aural warning unit.Overheat/fire detectors on the engind signals t

41、o the engine and APU fire detection module. This module will supply aural and visual indications in the flight compartment.The engine and APU fire detection module gives visual indications for detector faults on the module and the engine and APU fire control panel panel.Overheat/fire testYou use the

42、 TEST switch on the engine and APU fire control panel. In the OVHT/FIRE position, the indications in the flight compartment are the same as for the real fire condition. If the test fails, use the engine and APU fire detection module to isolate the fault.NOTE: During the engine overheat/fire test, th

43、e APU fire and wheel well fire circuits are also tested.Fault/inop testYou use the TEST switch on the engine and APU fire control panel. In the FAULT/INOP position, the indications in the flight compartment are the same as a real fault condition. If the test fails, use the engine and APU fire detect

44、ion module to isolate the fault.NOTE: During engine fault test, the APU fire detector fault circuit is tested.Single Loop OperationIf an engine overheat/fire detector fails to operate, the engine and APU fire detection module automatically changes to single loop operation. In the single loop mode, o

45、nly one loop must detect an overheat or fire condition for the engine and APU fire detection module to give the alarm condition.There is no indication in the flight compartment of single loop operation until you do the OVHT/FIRE test.EFXIA ALL26-11-00-006FECTIVITYD633A101-XIA26-11-00Page 4 Oct 10/20

46、0226-11-00-006EFXIA ALLFECTIVITYFIRE - ENGINE FIRE DETECTION - GENERAL DESCRIPTION26-11-00D633A101-XIAPage 5 Feb 10/2003FIRE - ENGINE FIRE DETECTION - ENGINE FIRE DETECTORSPurposeThe engine fire detectors monitor for high temperatures in the engine area.General DescriptionEach engine has eight detec

47、tors. The detectors monitor four sections of the engine. In each section, two detectors attach to a support tube and make an assembly. An assembly has one detector from loop A and one from loop B.Physical DescriptionThe engine fire detectors have these parts:* Overheat, fire, and fault pressure swit

48、ches* Resistors* Terminal stud* A stainless steel, gas charged tube.LocationThese are the locations of the engine fire detectors:* Two on the upper fan case section* Two on the lower fan case section* Two on the left core section* Two on the right core section.EFXIA ALLFECTIVITYDetector Characterist

49、icsThis table shows the temperature characteristics of the detectors.Detector LocationOverheatFireUpper Fan Case345F (174C)580F (304C)Lower Fan Case345F (174C)580F (304C)Left Core Section650F (343C)850F (454C)Right Core section650F (343C)850F (454C)OperationThe three pressure switches sense these co

50、nditions:* Overheat* Fire* Fault (loss of gas pressure).Gas pressure in the sense tube holds the fault pressure switch in the d position. The other two pressure switcheswhen the gas pressure increases because of an overheat or fire condition.The overheat and fire signals go to the engine and the APU fire detection module. This module s overheat or fire indication in the flight compartment.If the pressure in the sense tube decreases, the fault switch opens. This switch sends the fault signal to the engine and APU fire detection module.26-11-0026-11-00-003D633A101-