767飞行手册

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767飞行手册
BOEING 767 TABLE OF CONTENTS THE AIRCRAFT….11 BASIC FLIGHT INSTRUMENTS AND CONTROLS..................7 AIRSPEED INDICATOR ALTIMETER TAPE RADIO ALTIMETER....... VERTICAL SPEED… ,非非非非 ELECTRONIC ATTITUDE DIRECTOR INDICATOR THROTTLES FLAPS L∧ NDING GEAR… SPOILERS…, LAVIGATION SYSTEMS 垂看。。。。。。。。。。。。。D。D。D。。·。·。。。。。看。看。。。。看 RMI AFDS STATUS ATERAL MODES VERTICAL MODES............... RADAR ALTITUDE SPEED DEVIATION SCALE.... 90000 RUNWAY CLOSURE INDICATOR OURSE DEVIATION INDICATION (CDI)AND GLIDESLOPE SCALES FLIGHT DIRECTOR ELECTRONIC HORIZONTAL SITUATION INDICATOR OSE MODE ARC MODE∴.. OFF MODE 111 ““““+“+“ +“ ““““ OMMUNICATIONS. av 1 RECEIVER RADIOS...... 13 AUTOPILOT FLIGHT DIRECTOR SYSTEM(AFDS)…,,,,,,,,,,,,,,,,…,……14 AUTOTHROTTLE MODES 14 LTITUDE MANAGEMENT MODES . HEADING MODES 16 NAVAID TRACKING MODES 1 16 APPROACII MODE................. 17 AUTOLAND MODE NGINE INDICATION AND CREW ALERTING SYSTEM( EICAS).…...,…,…,…,……,……18 AS MESSAGE CONTROL ENTER PANEL INSTRUMENTS..m.. m..m..2 PWS/WARNINg liGhtS GROUND PROXIMITY WARNING SYSTEM.. WARNING ANNUNCIATORS 2 STANDBY ENGINE GAUGE...... AUTOBRAKES STANDBY FLIGHT INSTRUMENTS.... Boeing 767 LOCK Ⅴ ERHEAD SYSTEMS PANEL∴24 ELECTRICAL SYSTEMS....24 BATTERY POWER 24 EXTERNAL POWER APU POWER… AC BUS 25 ENEratorS UEL SYSTEM AND STARTING SYSTEMS. FUEL PANEL 26 START PANEL FUEL CONTROL SWITCHES... NORMAL ENGINE STARTING PROCEDURE……1 QUICK ENGINE STARTING PROCEDURE PNEUMATIC SYSTEM. OLD STARTUP SOLATION VALVES… AIR CONDITIONING SYSTEM MISCELLANEOUS ······· 30 ASSENGER SIGNS∴ ANTI-ICE YAW DAMPER... ···················+·+:·;·:· FORWARD OVERHEAD PERFORMANCE CHARTS B-767-200 OPERATING SPEEDS.... TWO ENGINE 300 KNOT CRUISE........ TWO ENGINE MACH &0 CRUISE WO ENGINE LONG RANGE CRUISE TWO ENGINE HOLDING SPEEDS AND FUEL FLOW 67 NORMAL PROCEDURES CHECKLIST . OCKPIT INITIAL PREPARATION COCKPIT FINAL PREPARATION BEFORE STARTING ENGINES BEFORE BRAKE RELEASE TAXI BEFORE TAKE-OFF FTER TAKE-OFF DESCENT DESCENDING THRU FL180 OR LEAVING CRUISE BEFORE LANDING AFTER LANDING.. PARKING...... IF LEAVING AIRCRAFT. 自自非 .40 OPERATING LIMITATIONS 鲁看鲁鲁春垂 ISTRUCTURAL WEIGHT LIMITATIONS MAXIMUM TIRE SPEED 41 BOEING 767 Ⅴ ERWEIGHT LANDING MAXIMUM OPERATING LIMIT SPEEDS(VMO/MMo).. DESIGN MANEUVERING SPEEDS (VA) 41 MAXIMUM FLAP EXTENDED SPEEDS (V 41 LANDING GEAR LIMIT SPEEDS (VLOLE). ··“·“;;·:“;·········“········“·“·““;“;“;“““;“· TALL SPEEDS - KIAS MINIMUM V, SPEED (ALL TAKEOFF FLAPS). REDITS AND OTHER THINGS . LEGAL STUFF ·· Created by Terry Yingling Roaminganetzero. net 15July1999 Boeing 767 THE AIRCRAFT The 767 is a large, two-aisle twinjet, airplane and is miles; and the 767-300 Freighter, with 16,020 cubic feet of currently in service in five versions: the 767-200 and- cargo volume and a range of 3, 765 miles 200ER (extended range), with seating for 224 passengers in two classes or 181 passengers in a three- In 1997, Boeing launched a higher-capacity version of the f up to 7, 665 miles; the 767- 767, called the 767-400ER. Thi 300 and -300ER, with seating for 269 in two classes seating for 304 passengers in two classes or 245 ind 218 in three classes and a range capability of 7, 080 passengers in a three-class arrangement with a range capability of 6, 475 miles Seat Basic Max to Weight 767-200ER 181 passengers in three classes 767-200ER 345,000 pounds 767-300ER 218 passengers in three classes 767-300ER 380,000 pounds 767-300 Freighter 767-300 Freighter 408,000 pounds 767-400ER 245 passengers in three classes 767400ER 400,000 pounds Configurations Fuel 24, 140US galle Seating ranges from five-to seven-abreast with two maximum range 767-200ER 6,650Nm Length 767-300ER 6,150N 767-300 Freighter 3,270 767-200ER 159 feet 2 inches 767400ER 5.625Nm 767-300ER 180 feet 3 inches 767-300 Freighter 180 feet 3 inches Altitude capability 767-400ER 201 feet 4 inches 767-200ER 37,900feet Wingspan 767-300ER 35,200feet 767-300 Freighte 1g 35,000feet 767-200/-300/-300 freighter 156 feet 1 inches 767-400ER 34,700feet 767-400ER 70 feet 4 inches Cruise speed Mach 0.80 (530 mph Tail height Cargo cal 767-200300-300 Freighter 52 feet 0 inches 767-400ER 55feet I inches 767-20ER 3070 cubic feet 767-300ER 4030 cubic feet EI engines 767-300 Freighter 16020 cubic feet 767400ER 4.580 cubic feet 767-200/-300/-400ER/-300 Freighter Pratt Whitney Pw4000 Airplane model Price(millions $) 767-300/-300 Freighter 767-200ER 89.0-100.0 Rolls royce rb211-524 767-300ER 105.0-117.0 767-400ER 115.0-127.0 767-200/-300/-40ER/-300 Freighter General electric CF6-80C2B 1999 Monthly Production Rate is 4 per qtr BOEING 757/767 BASIC FLIGHT INSTRUMENTS AND CONTROLS NOSE RETRACT SK OFF VERTICA SPEED N0020 10 6 二5 101329 o■o 5 AIRSPEED INDICATOR The orange altimeter bug is a selectable Decision Height () bug. Clicking over the left or right side of the dh It has both rotating analog airspeed digits and bug knob will cause the diI bug to rotate around the rotating analog Mach number digits. The Mach altimeter. Additionally, there is a dh number window does not become active until 400 Mach DH Bug Mach window N0020 的p/ DH Bug Kn0b Airspeed bugs Baro Knob 000 Command Airspeed Bug window in the EADi just above the digital Radio Altitude readout. The digital Dhi readout responds to movement of the altimeter dh bug and indicates the Also incorporated into the gauge are airspeed same value. When the aircraft reaches the radio height reference bugs and an autopilot set airspeed bug. The indicated in the dh window the radio altitude readout airspeed bugs are moveable using mouse click areas will change to orange and the gpws system will call out near the right edge of the gauge. They ha I Minimums. Minimums" ave a memory"so that every time the panel is loaded they will be in their last assigned position. Additionally, TAPE RADIO ALTIMETER when moving an airspeed bug and bumping into another airspeed bug they will all move along There are two radio altimeters. The digital together. The autopilot airspeed bug is set using the readout located in the upper right corner of AFDS IAS/MACH display window EADI and the tape radio altimeter. The radio altimeter only reads out to 1, 400ft. The ALTIMETER digital readout displays altitude up to 2,500 feet above the ground The altimeter setting is shown in both Millibars and Inches of Hg. The altimeter setting is adjusted by Ⅴ ERTICAL SPEED clicking on the left or right side of the baro knob Both Mb and hg readouts will respond to the A Vertical speed indicator is available VERTICAL SPEED baRO knob movement and is calibrated to show assent or decent in thousands fpm Boeing 767 ELECTRONIC ATTITUDE LANDING GEAR NOSE DIRECTOR INDICATOR LEFT RIGHT Looking at the picture at left you RETRACT Artificial horizon Angle bank Indicator will see outlined the mouse click 270K areas. Box 1is where you click H200 fo GS250 r gear down Is where you click for gear up. Box 3 is OFF 10 something new called the OFF position Once the gear have retracted and you are climbing out the procedure is to put the gear VNAV handle in the off position. This cuts power to the NAv/ hydraulic systems feeding the landing gear assembly. So p Indicator Pitch bar indicator clicking on will bring the handle down to OFF (as shown). Box4 is normally an override switch but we The eadi combines many functions into one are using it as a test switch. Pressing it will test all the instrument. Basic flight guidance is provided by an landing gear indicator lights artificial horizon for pitch and roll control. At the bottom of the EADI is a slip indicator for yaw a note about the Tail Skid light. Even though it control. Description of the other functions of the illuminates during the test, it is non operational. This EADI is provided in the navigation Systems section light only illuminates if the tail skid is out of position and of this manual the warning is suppressed during normal operations THROTTLES SPOILERS The two throttles may be operated Just click and drag the spoiler handle to extend or retract together or when dragged with the the spoilers mou dently. Reverse thrust is available FLAPS RET Flaps are operated by clicking on the gauge a plus sign shown will lower the flaps and a minus sign will raise them EXT FLAP 220K 210K 15 FLAPS 20 /195K 8 BOEING 767 NAVIGATION SYSTEMS RMII A significant feature of the rmi is the ability to DME 1 DME 2 elect the nav source for each course needle 002.8002 Clicking over each knob will change position to DME 1 l/// DME 2 indicate the Nav source and the corresponding needle VOR 2 VOR 1 will point accordingly. VOR 1 is the dashed arrow, vor 2 is the outlined arrow 少 VORI. VOR2 and Adf are the allowable Nay Source sources. However, since there is only one ADF Selection √AADF ADF possible in Fs98 both pointers will point to the same ADF. DME I and dMe 2 correspond to Nav I and Nay 2 information Ground Speed DH AIt Speed Deviation Scale GS250 DH200 Radar alt 1750 Glideslope Auto Throttle mode 10 Runway Closure SPD FL CH 10 aFDs Status FD CMD s囗AT FD Vertical modes PD Lateral modes (upper) o。 IOO LO0c↓ ower TO LNAV (lower) (upper) SPD HDG HLD LOC LOC ALT HOLD G/S FLARE HDG SEL R OUT L NAV FLARE VNAV L NAV B/CRS VNAV GA Course deviation GA B/CRS ROUT AFDS STATUS different lateral and vertical modes would be selected to continue the flight. The same is true for a go Indicates the status of the autopilot if the autopilot is around. ga would be annunciated for both modes engaged the green CMD annunciator will show. If and would be cleared on climbout through selection the autopilot is not engaged but the flight director is of different modes in use a green Fd would show If the aFds is in FD mode then the flight director bars will command your LATERAL MODES flight based on autopilot inputs. Therefore, the pilot can manually fly the aircraft and still have complete The lateral mode selected on the autopilot is control of the flight director through the autopilot annunciated in the lower right corner of the EaDI The upper position(white)shows the armed mode When the Fd is engaged on the ground the AFDS For example, if in heading hold(HDG HOLD)mode goes into takeoff mode and the TO annunciators are and the localizer LoC) is selected to capture the indicated for both lateral and vertical modes The white LOC and the green HDG HOLD would show flight director commands runway heading and a pitch When the aircraft intercepts the localizer the white attitude for positive rate of climb. After takeoff a LOC will disappear and a green LoC will appear in Boeing 767 place of HDG HOLD. This indicates the autopilot is altitude is below the selected dh the digits turn now tracking the localizer. orange. The Roll out annunciator is associated with the autoland capability of the aircraft. When in a Cat ll SPEED DEVIATION SCALE or cat Iii situation and using the autoland's land 2 or Land 3 function(explained later) a ROLL OUT Commonly known as the fast/slow gauge, this annunciation will be seen which indicates the aircraft display will show how far off the aircraft is from the is ready to(white)or is performing (green) the autopilot selected airspeed. If too fast the pointer runway rollout procedure. B goes to the F side. If too slow the pointer moves spacc toward the S side. It is calibrated at +/-10 kias constraints the RolL OUT annunciator appears as R UT RUNWAY CLOSURE VERTICAL MODES INDICATOR The vertical mode selected on the autopilot is When in the Approach mode and below 200ft AGL, a annunciated in the lower left corner of the eadi small runway symbol will appear in the EADI and The upper position(white) shows the armed mode ill gradually rise up into the pitch bar as you close For example, if in altitude hold(ALt HOlD) mode in on the ground. This is a nice backup in low and the approach mode(app) is engaged there would visibility to give you yet another indication that be a white g/s annunciator to indicate arming for ground contact is coming. This symbol we have here glideslope capture on top of the green ALT HOLD is not 100% accurate for the 767 but it does the job annunciator. Then upon glideslope intercept the white Gis will disappear and the green G/'s will COURSE DEVIATION appear in place of the ALT HOLd annunciator. This indicates the autopilot is now tracking the glideslope INDICATION (CDD AND path GLIDESLOPE SCALES The Flare annunciator is associated with the When tuned to a vor there will be a course autoland capability of the aircraft. When in a Cat ll deviation scale. The Glideslope scale is only present or cat iii situation and using the autoland's land 2 when a valid ils is tuned in or land 3 function the flare annunciation which indicates the aircraft is ready to (white) or is FLIGHT DIRECTOR performing (green) the FLARE maneuver, will illuminate. additionally the autothrottle will The flight director only requires to be turned on/off annunciate Idle during the flare with the fd switch on the afds panel. when turned on a horizontal and vertical pink bar will appear on RADAR ALTITUDE the face of the eadl a digital radar altitude displays actual height above The flight director uses a double cue with 2 bars The the ground up to 2, 500 feet. Between 500 and 2, 500 basic idea is to adjust aircraft pitch and roll so that feet the display is calibrated at 50 foot increments the pink Pitch Bar (horizontal line) and pink Roll Bar Below 500 feet the calibration becomes 10 feet (vertical line) are al ways centered. Pitch towards the There is a dh window that is adjusted using the bars to center them altimeter Dh bug adjustment. When the radio

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