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Super 80 Professional – AOM

LANDING GEAR

Section 18 Page 3

Super 80 Professional – Aircraft Operating Manual

Coolsky, 2018

Main Gear Doors

The main gear doors consist of a

hydraulically operated main door and a

mechanically operated outboard door. The

main gear doors are mechanically latched

when closed. The main gear doors cycle to

the closed position when the gear is

approaching the extended position.

Visual/aural Indicating and Warning

System

The landing gear position and status is

indicated by annunciator lights on the

upper main instrument panel. Three landing

gear position lights come on green to

indicate that the landing gear is down and

locked. The lights will come on red when the

landing gear is in any intermediate position.

The landing gear door annunciator will

come one anytime either of the main

landing gear doors are not closed and

latched.

The landing gear warning horn and vocal

warning will sound when the airplane is at or

below 210 KTS and either one of the throttles

are closed and the landing gear handle is

not in the down position. The landing gear

warning horn and vocal warning will also

sound whenever the flaps are extended to

beyond 26 degrees and the landing gear

handle is not in the down position.

Reference markings on each main gear

landing gear over-center linkage provide

visual confirmation that the landing gear is

down and locked. Nose gear verification is

provided by a green indicator pin on the

pedestal just behind the throttle quadrant.

Brakes

Each main gear wheel is fitted with a dual

system, disc-type power brake. Each brake

contains two independent cylinder and

passageway systems. Each system contains

four hydraulic cylinders, one bleed port and

one hydraulic pressure port.

The wheel brakes are controlled by two

completely independent hydraulic brake

systems. Each system is capable of supplying

reserve brake pressure in the event of a

hydraulic pressure failure in the other system.

The airplane wheel brakes may be

mechanically applied by depressing the

brake pedals.

A fully automatic anti-skid system is installed

to obtain a more effective braking

application, through control of wheel

rotation at the point of maximum braking

efficiency. The system is deactivated

whenever the landing gear handle is not in

the down detent, parking brakes set, arm

switch at OFF, or airplane is at low taxi

speeds.

Both main landing gear wheels and nose

gear wheel are fitted with spin brakes. The

purpose of the spin brake is to stop the tire

rotation after take-off.

A gauge and annunciator light proved

visual indication of brake temperature.

The parking brakes are set by pulling up the

park brake control knob (located on the

captain’s left console). Park brake on is

indicated by an annunciator light on the

overhead panel. If the throttles are

advanced to a take-off setting with the

parking brake set, the aural/vocal warning

system will be activated.

Содержание Super 80 Professional

Страница 1: ...Super 80 Professional Aircraft Operating Manual By Coolsky 2018 Version 2 0...

Страница 2: ...ng Techniques 4 Emergency Procedures 5 Air Conditioning and Pressurization 6 Anti Ice and Rain Protection 7 Auto Flight 8 APU 9 Communications 10 Electrical 11 Fire Protection 12 Flight Controls 13 Fl...

Страница 3: ...TAIN S INSTRUMENT PANEL 11 CENTER INSTRUMENT PANEL 12 PEDESTAL FORWARD 13 PEDESTAL AFT 14 SECTION 2 LIMITATIONS 0 TABLE OF CONTENTS 1 GENERAL 2 AIRSPEEDS 3 WEIGHTS 3 SECTION 3 NORMAL PROCEDURES 0 TABL...

Страница 4: ...SCHEMATIC PNEUMATICS 3 CONTROLS AND INDICATORS 4 AIR CONDITIONING 5 PRESSURIZATION 7 WARNING AND CAUTION INDICATORS 9 SECTION 7 ANTI ICE AND RAIN PROTECTION 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AN...

Страница 5: ...ORS 3 SECTION 11 ELECTRICAL 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 4 WARNING AND CAUTION INDICATORS 7 SECTION 12 FIRE PROTECTION 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATOR...

Страница 6: ...ISPLAY 11 PFD FAIL LEGENDS 13 PFD COMPACTED MODE 14 SECTION 15 FLIGHT MANAGEMENT 0 TABLE OF CONTENTS 1 GENERAL 2 IRS MODE SELECT PANEL 6 FMS FLIGHT GUIDANCE MODES 7 MCDU PAGE DESCRIPTION 11 FMS OPERAT...

Страница 7: ...ION DISPLAY ROSE MODE 5 NAVIGATION DISPLAY ARC MODE 6 NAVIGATION DISPLAY MAP MODE 8 NAVIGATION DISPLAY PLAN MODE 9 MODE SELECTOR CONTROL PANEL MAG TRUE LIGHT 10 SECTION 21 OXYGEN 0 TABLE OF CONTENTS 1...

Страница 8: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 1 DESCRIPTION...

Страница 9: ...CONTENTS SECTION 1 DESCRIPTION 0 TABLE OF CONTENTS 1 DIMENSIONS 2 TURNING RADIUS 4 COMPARTMENTS 5 INTERIOR ARRANGEMENT 6 COCKPIT ARRANGEMENT 7 OVERHEAD PANEL AFT 8 OVERHEAD PANEL FORWARD 9 GLARESHIEL...

Страница 10: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 2 Super 80 Professional Aircraft Operating Manual Coolsky 2018 DIMENSIONS...

Страница 11: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 3 Super 80 Professional Aircraft Operating Manual Coolsky 2018...

Страница 12: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 4 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TURNING RADIUS...

Страница 13: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 5 Super 80 Professional Aircraft Operating Manual Coolsky 2018 COMPARTMENTS...

Страница 14: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 6 Super 80 Professional Aircraft Operating Manual Coolsky 2018 INTERIOR ARRANGEMENT...

Страница 15: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 7 Super 80 Professional Aircraft Operating Manual Coolsky 2018 COCKPIT ARRANGEMENT...

Страница 16: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 8 Super 80 Professional Aircraft Operating Manual Coolsky 2018 OVERHEAD PANEL AFT...

Страница 17: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 9 Super 80 Professional Aircraft Operating Manual Coolsky 2018 OVERHEAD PANEL FORWARD...

Страница 18: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 10 Super 80 Professional Aircraft Operating Manual Coolsky 2018 GLARESHIELD AND UPPER INSTRUMENT PANEL...

Страница 19: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 11 Super 80 Professional Aircraft Operating Manual Coolsky 2018 CAPTAIN S INSTRUMENT PANEL...

Страница 20: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 12 Super 80 Professional Aircraft Operating Manual Coolsky 2018 CENTER INSTRUMENT PANEL...

Страница 21: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 13 Super 80 Professional Aircraft Operating Manual Coolsky 2018 PEDESTAL FORWARD...

Страница 22: ...Super 80 Professional AOM DESCRIPTION Section 1 Page 14 Super 80 Professional Aircraft Operating Manual Coolsky 2018 PEDESTAL AFT...

Страница 23: ...Super 80 Professional AOM LIMITATIONS Section 2 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 2 LIMITATIONS...

Страница 24: ...80 Professional AOM LIMITATIONS Section 2 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 2 LIMITATIONS 0 TABLE OF CONTENTS 1 GENERAL 2 AIRSPEEDS 3 WEIGH...

Страница 25: ...nd Component 10 knots Crosswind Values Take Off and Landing Maximum demonstrated crosswind component is 30kts This is not a limitation However components at or near 30 knots with higher gusts should b...

Страница 26: ...s 57M 31 40 195kts 57M Slats Extended SLATS POSITION LIMITING SPEED Mid position 280kts 57M Full extended 240kts 57M Turbulence Penetration Speed 275 285kts or 75 79M whichever is lower WEIGHTS Maximu...

Страница 27: ...Super 80 Professional AOM NORMAL PROCEDURES Section 3 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 3 NORMAL PROCEDURES...

Страница 28: ...OF CONTENTS 1 GENERAL 2 NORMAL PROCEDURE CHECKLIST 3 ORIGINATION PRE FLIGHT INSPECTION 5 COCKPIT CLEAN UP INSPECTION 13 BEFORE STARTING ENGINES 16 PRIOR TO ENGINE START OR PUSHOUT 20 APU START 21 ENGI...

Страница 29: ...lot flying will normally call for changes to be made to the Flight Guidance panel by the pilot not flying Both pilots should be aware of all communications traffic and clearances Traffic Watch Both cr...

Страница 30: ...UT GALLEY POWER OFF ENGINE IGNITION CONTIN FUEL PUMPS ON AUX HYDRAULIC PUMP ON ANTI COLLITION EXTERIOR LIGHTS ON AS REQUIRED DOOR ANNUNCIATOR OUT AIR CONDITIONING SUPPLY SWITCHES OFF TAXI BEFORE TAXI...

Страница 31: ...POILER LEVER ARMED AUTO BRAKES AS REQUIRED FLAPS SLATS LAND ANNUNCIATOR LIGHTS CHECKED AFTER LANDING TAXI AUTOPILOT AND AUTOTHROTTLE SWITCHES OFF LANDING LIGHTS OFF SPOILER LEVER RET AUTO BRAKES OFF D...

Страница 32: ...n on the Instrument Panel Digital lights 6 Turn on the Flight Guidance Control Panel Digital lights HYDRAULIC PANEL CHECK 7 Set the Transfer Pump switch to OFF 8 Set both Engine Pump switches to HI 9...

Страница 33: ...Set the AIR COND SHUTOFF switch to AUTO 27 Set the RAM AIR switch to OFF EXTERIOR LIGHTS CHECK LIGHTS 28 Check the exterior lights of the aircraft Not simulated in the panel FLAP HANDLE INDICATOR AGRE...

Страница 34: ...the FLIGHT RECORDER OFF light stays off the Flight Recorder operates properly 49 Set the Flight Recorder Test switch back to NORM and put the guard back on FD CMD NORMAL 50 Set the FD CMD switch to N...

Страница 35: ...f Note The Start Pump should be off 66 Turn back on fuel pump used for APU operation IGNITION OFF 67 Set the Ignition switch to OFF FUEL HEAT OFF 68 Set both FUEL HEAT switches to OFF START SWITCHES L...

Страница 36: ...o OFF COCKPIT FLOOD LIGHT AS REQUIRED 84 Set the CKPT FLOOD switch to OFF or as required OVERHEAD CONSOLE LIGHTS AS REQUIRED 85 Set the OVHD CONSOLE LTS knobs to OFF or as required STALL WARNING TEST...

Страница 37: ...LAND PRE FLIGHT TEST ACCOMPLISH 106 Set both VHF radios to the same ILS frequency any frequency will do such as for example 110 90 Click the lower left number to switch between the two VHF radios 107...

Страница 38: ...MODE light should come on All Mode Selector lights should be out 125 Press TO to turn the NO MODE light off FUEL QUANTITY TEST 126 Push the Fuel Quantity Test button to test the Fuel Quantity Indicat...

Страница 39: ...that the LONG TRIM indicator moves in the appropriate direction SPOILER LEVER RET 141 The spoiler lever should be in the RET position forward down position RUDDER HYDRAULIC CONTROL PWR 142 The RUD HY...

Страница 40: ...OGBOOK CHECK 5 Check the aircraft papers Not simulated CIRCUIT BREAKERS CHECK 6 Not simulated BATTERY SWITCH ON 7 Set the battery switch to the ON position EMERGENCY POWER OFF 8 Set the Emergency Powe...

Страница 41: ...OPEN PNEUMATICS AND AIR CONDITIONING ESTABLISHED 24 Set Pneumatic X Feed handles to the OPEN up position 25 Check that the APU AIR switch is set to ON or COLDER 26 Set both Air Conditioning Supply swi...

Страница 42: ...ch to RESET Momentary to reset the fuel used counters GEAR HANDLE DOWN 46 Confirm that the gear handle is down and that all the three green gear lights are on FLAP HANDLE INDICATOR AGREE 47 Make sure...

Страница 43: ...Check and set the levers on the Audio Panel For normal operation set VHF 1 and 2 and the MKR lever to ON up Leave the rest in the OFF off position EMERGENCY LIGHTS ARMED 8 Set the emergency lights swi...

Страница 44: ...BARO knob You can also reset the barometric pressure setting by pressing the B key on your keyboard 31 Also set and check the Standby Altimeter 32 Check the Radio Distance Magnetic Indicator No flags...

Страница 45: ...the LONG TRIM handle SPOILER LEVER RET 53 The spoiler lever should be in the RET position forward position THROTTLES CLOSED 54 Both throttles should be closed and the reverse levers down TAKE OFF WARN...

Страница 46: ...fessional Aircraft Operating Manual Coolsky 2018 FLIGHT FORMS CHECKED 64 Have you done your paperwork NO SMOKING SIGNS ON 65 Set the No Smoking switch to ON FIVE MINUTES PRIOR TO DEPARTURE SEAT BELT S...

Страница 47: ...fuel leave them OFF AUX HYDRAULIC PUMP ON 4 Set the Auxiliary Hydraulic Pump switch to ON Also check that both engine hydraulic pumps are in the LOW position ANTI COLLITION EXTERIOR LIGHTS ON AS REQUI...

Страница 48: ...d or engine s running set the RH Aft Fuel Boost Pump switch to ON Note that you do not need to have both the Start Pump and a Fuel Boost Pump running simultaneously only one of them is required APU MA...

Страница 49: ...Section 3 Page 22 Super 80 Professional Aircraft Operating Manual Coolsky 2018 PNEUMATIC PRESSURE NORMAL 15 The Pneumatic Pressure Gauge should indicate about 35 PSI PNEUMATIC X FEED VALVES OPEN 16 Op...

Страница 50: ...for the engine you are about to start must be set to OPEN Set the left Pneumatic X Feed handle to OPEN up 6 Check the Pneumatic Pressure Gauge Optimum starting pressure is about 30 38 PSI 7 Open the g...

Страница 51: ...should be out 21 EXT PWR L Power In Use Light should be out 22 L CSD OIL PRESS LOW light should be out 23 L OIL PRESS LOW light should be out 24 L HYD PRESS LOW light should be out 25 EGT should indi...

Страница 52: ...the brakes to stop the forward motion and simultaneously set both engines to reverse idle thrust 8 When both blue ENG REVERSE THRUST lights come on release the brakes and drop both feet to the floor 9...

Страница 53: ...pump failure TAXI The second part of the TAXI checklist is normally performed while the aircraft is taxiing Note that one engine taxi is only necessary when extended taxi is expected Otherwise taxi w...

Страница 54: ...cking for freedom of movement and normal control forces 8 Check that the SPOILER DEPLOYED light comes on during aileron check 9 Check that the ELEVATOR POWER ON light comes on when the control column...

Страница 55: ...be erect and have no flags visible 10 Make sure the ART switch is in the AUTO position guarded position ANTI ICE AS REQUIRED 11 Set the Air Foil Anti Ice switch to OFF Turn the Air Foil Anti ice swit...

Страница 56: ...cabin by pressing the ATTENDANT CALL button once Press the Attendant Call Reset light below to extinguish the light 25 Set the Air Conditioning Supply switches to AUTO ANNUNCIATOR LIGHTS CHECKED 26 Ch...

Страница 57: ...l needles should be within normal range 8 Callouts for 80 knots V1 rotate V2 and V2 10 should be made 9 When the aircraft has reached a positive rate of climb 10 select gear up and verify that the gea...

Страница 58: ...e out on the Slats Advisory Lights panel PRESSURIZATION AND AIR COND CHECKED 8 Check that the Cabin Altitude indicator is indicating normally rising altitude 9 Check that the Differential Pressure ind...

Страница 59: ...rd HYDRAULIC PUMPS LOW OFF 17 Set both Engine Pump switches to LOW 18 Set the Auxiliary Pump switch to OFF 19 Set the TRANS Pump switch to OFF if on 20 Not on the checklist On the Annunciator Panel ch...

Страница 60: ...After the center tank is empty as indicated by the quantity gauge 4 set the center tank Fuel Pump switches to OFF FIRST FLIGHT OF DAY ITEMS CHECKED 5 During the airplane s first flight of the day vari...

Страница 61: ...DSHIELD ANTI FOG AS REQUIRED 9 If you expect to descend into an area with high humidity or rain turn on windshield anti fog Note that this system should be used for anti fogging rather than defogging...

Страница 62: ...witch to ON 17 Check the Hydraulic Quantity gauges Both gauges should read above the red band 18 Check the Brake Pressure gauge Both needles should indicate minimum above the red band but normally wit...

Страница 63: ...T AND CROSSCHECKED 3 Check that none of the flight instruments have any flags visible Crosscheck all standby flight instruments against the primary flight instruments SEAT BELT NO SMK ON 4 Set the Sea...

Страница 64: ...h the blue Engine Reverse Thrust lights come on when applying reverse thrust If only one reverser deploys use caution when applying reverse power on remaining engine 3 Since reversing is more effectiv...

Страница 65: ...he Spoiler Lever to RET AUTO BRAKES OFF DISARM 5 Set the AUTO BRAKE Selector to OFF 6 Set the AUTO BRAKE ARM DISARM switch to DISARM PNEU XFEED One engine taxi R OPEN L CLOSED 7 For one engine taxi op...

Страница 66: ...e refer to the STARTING APU procedure guide on how to start the APU 16 Before shutting down the right engine set the APU Air switch to ON 17 and set the right Pneumatic X Feed Valve Lever to OPEN up R...

Страница 67: ...d be turned off Set the APU Master switch to OFF 7 Set the APU AIR switch to OFF 8 Set the APU DOORS switch to OFF and put the guard back on FUEL LEVERS OFF 9 Check that External power or APU power is...

Страница 68: ...te entries in the Flight Crew and aircraft logbooks FD SWITCHES OFF OFF 28 Set the Flight Director switch to OFF O2 PANEL SUPPLY LEVERS OFF 29 Set the DILUTER DEMAND CONTROL switch to NORMAL OXYGEN 30...

Страница 69: ...OFF 38 If the aircraft has ground power connected or the APU is running leave the battery switch in the ON position If the aircraft is being completely shut down for the night last flight of the day...

Страница 70: ...Super 80 Professional AOM OPERATING TECHNIQUES Section 4 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 4 OPERATING TECHNIQUES...

Страница 71: ...ection 4 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 4 OPERATING TECHNIQUES 0 TABLE OF CONTENTS 1 PREFACE 2 TAXI 2 JET BLAST 3 TAKE OFF 4 CLIMB 4 CRUI...

Страница 72: ...excessive thrust Taxiing The MD 81 has a very responsive nose wheel steering and light nose wheel footprint Special caution is therefore required when taxiing on wet or slippery surfaces Turning too r...

Страница 73: ...throttles This should give the aircraft sufficient momentum to sustain taxi out of the congested area If 1 2 EPR is not sufficient to move the aircraft out of a gate area where there is danger of jet...

Страница 74: ...a rejected take off situation is very sudden and abrupt Consider using manual braking during a rejected take off situation if runway length is not critical and immediate maximum braking is not require...

Страница 75: ...ts with flaps slats extended and or gear down should be avoided as they are airspeed limited noisy and expensive The FMS will present an optimum descent profile with Top of Descent TD and End of Desce...

Страница 76: ...ltitude to lower fuel consumption If prolonged holding is expected request ATC to increase the size of the holding pattern This will reduce the number of turns required Turns require increased power a...

Страница 77: ...be short or unnecessarily long The landing distance is affected by the glide path as well as the height above the runway threshold For example crossing the threshold at 100 feet instead of 50 can inc...

Страница 78: ...ide Path Angle Degrees Estimated Body Angle Degrees Pilot Eye Height At Threshold Feet Main Gear Height At Threshold Feet Main Gear Touchdown Point T Feet 2 5 4 9 44 29 664 2 75 4 65 48 34 708 3 0 4 4...

Страница 79: ...ide Path Angle Degrees Estimated Body Angle Degrees Pilot Eye Height At Threshold Feet Main Gear Height At Threshold Feet Main Gear Touchdown Point T Feet 2 5 4 9 44 24 550 2 75 4 65 48 28 583 3 0 4 4...

Страница 80: ...d puts more weight on the main gear This increases rolling friction as well as braking effectiveness This procedure is five times more effective than holding the nose off for aerodynamic braking Direc...

Страница 81: ...bles Brakes The brakes slow down the aircraft by absorbing the motion energy of the aircraft The brakes convert this motion energy into heat which is dissipated through cooling The brakes are required...

Страница 82: ...Super 80 Professional AOM EMERGENCY PROCEDURES Section 5 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 5 EMERGENCY PROCEDURES...

Страница 83: ...Super 80 Professional AOM EMERGENCY PROCEDURES Section 5 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 Emergency techniques are currently not described...

Страница 84: ...Super 80 Professional AOM AIR CONDITIONING AND PRESSURIZATION Section 6 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 6 AIR CONDITIONING AND PRESSURIZATION...

Страница 85: ...er 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 6 AIR CONDITIONING AND PRESSURIZATION 0 TABLE OF CONTENTS 1 GENERAL 2 FUNCTIONAL SCHEMATIC PNEUMATICS 3 CONTROLS AND...

Страница 86: ...identical air conditioning systems designed for independent or parallel operation Normally the right system operates from the right engine bleed air and supplies the passenger compartment temperature...

Страница 87: ...Super 80 Professional AOM AIR CONDITIONING AND PRESSURIZATION Section 6 Page 3 Super 80 Professional Aircraft Operating Manual Coolsky 2018 FUNCTIONAL SCHEMATIC PNEUMATICS...

Страница 88: ...packs from one operating engine and for making pneumatic crossfeed starts from opposite operating engine Also on the ground supplies APU bleed air or air from pneumatic ground source for operating on...

Страница 89: ...TOP Momentary Stops movement of TEMP CONTROL VALVE in manual mode 4 CABIN TEMPERATURE SELECTOR See Cockpit Temperature Selector 5 SUPPLY SWITCH L R OFF Closes off all pneumatic valves for the air cond...

Страница 90: ...and increases differential pressure across air conditioning turbine thus lowering temperature of conditioned air during ground operation Use of this switch position significantly reduces airflow in th...

Страница 91: ...ARO SELECTOR KNOB Used to set departure destination barometric pressure in Mb In Hg window 6 FLOW LIGHT Indicates current air flow is insufficient maintain cabin pressure The cause may be insufficient...

Страница 92: ...LEVER Auto Up Cabin altitude is controlled automatically Manual Down Cabin altitude is manually controlled by adjusting the Cabin Altitude Control Wheel 3 CABIN ALT CONTROL WHEEL With Cabin Altitude C...

Страница 93: ...0 Professional Aircraft Operating Manual Coolsky 2018 WARNING AND CAUTION INDICATORS 10 CABIN ALT LIGHT Red Comes on when cabin altitude exceeds 10 000 ft The CABIN ALT light is accompanied by the MAS...

Страница 94: ...Super 80 Professional AOM ANTI ICE AND RAIN PROTECTION Section 7 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 7 ANTI ICE AND RAIN PROTECTION...

Страница 95: ...D RAIN PROTECTION Section 7 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 7 ANTI ICE AND RAIN PROTECTION 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND IN...

Страница 96: ...ge by the tail de ice pushbutton Heat is then diverted from the wing leading edge slats and strakes to the horizontal stabilizer Tail de icing is provided for 2 5 minutes and then flow is reverted bac...

Страница 97: ...o flow to the wing leading edge slats strakes and horizontal stabilizer 4 TAIL DE ICE PUSHBUTTON Closes shutoff valve to the wings and strakes and opens up the shutoff valve to de ice the tail After a...

Страница 98: ...ns selector valve from primary to reserve fluid container Selector valve cannot be reset to primary until serviced by maintenance 2 RAIN REPELLENT PUSHBUTTONS L R Discharges a metered quantity of flui...

Страница 99: ...ANTI ICE ON LIGHT Blue Indicates anti ice heat has been selected for wing leading edge and strakes 9 TAIL DE ICE ON LIGHT Blue Indicates de ice heat has been selected for the leading edge of the hori...

Страница 100: ...Super 80 Professional AOM AUTO FLIGHT Section 8 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 8 AUTO FLIGHT...

Страница 101: ...OF CONTENTS 1 GENERAL 2 FLIGHT DIRECTOR 5 AUTOTHROTTLE 6 ROLL MODE SELECTORS 7 PITCH MODE SELECTORS 8 YAW DAMPER MACH TRIM AND ALTITUDE ADVISORY LIGHT 10 EFIS CONTROLS 11 EFIS CONTROL AND DIMMING PAN...

Страница 102: ...utomatically controls the airplane in pitch roll and yaw maneuvering axes The AP will actuate the appropriate control surfaces to control the aircraft for the selected AP mode of operation The AP mode...

Страница 103: ...tard the throttles go around The autothrottle function is engaged by moving the AUTO THROT switch from OFF to AUTO THROT position When the autothrottle function is disengaged the THROTTLE warning ligh...

Страница 104: ...conjunction with other interfacing equipment on the aircraft provides automatic navigation guidance map display and in flight performance optimization It eliminates many routine tasks and computations...

Страница 105: ...ts and DFGC 2 provides the First Officer s FD command bars and fast slow pointer with command inputs BOTH ON 1 DFGC 1 provides both the Captain s and First Officer s FD command bars and fast slow poin...

Страница 106: ...Readout Digital readout of the indicated airspeed or Mach value selected with the SPD MACH select knob 3 SPD MACH select knob Click the numbers to select the value in the SPD MACH Readout Press knob...

Страница 107: ...zer Pitch FMA will annunciate GS CAP when capturing selected glideslope and CAP TRK when tracking selected glideslope AUTO LAND Arms the DFGC to engage AUTO LAND mode after selected localizer and glid...

Страница 108: ...will pitch up to lose speed and pitch down to gain speed TURB Varies aircraft pitch attitude ALT HOLD Disengages ALT HOLD mode and engages VERT SPD mode 3 Mode Selector Buttons ALT HOLD Engages ALT H...

Страница 109: ...attitude data is unable to supply the data the AP master switch will disengage The other DFGC should be selected if this occurs 6 ALT Preselect Readout Digital readout of the altitude selected with t...

Страница 110: ...sation mode is inoperative YAW DAMP OFF Digital display Comes on to indicate yaw damper is off 60 MACH TRIM INOP Digital display Comes on to indicate Mach trim compensator is off or Mach Trim Comp swi...

Страница 111: ...ntrols PFD brightness Turn knob full counter clock wise to turn off PFD screen This will cause the compact mode to be displayed on the ND 4 ND WX KNOBS Inner knob Controls weather radar overlay bright...

Страница 112: ...e AP1 AP2 light indicates whether DFGC 1 or DFGC 2 is providing guidance input 6 THROTTLE Warning Light Red The light comes on flashing whenever the autothrottle disengages automatically or the AUTO T...

Страница 113: ...tion that does not permit autoland has been detected The light comes on flashing during the Autoland Preflight Test AP Trim Light Amber This legend indicates that the autopilot has a sustained out of...

Страница 114: ...ted takeoff thrust EPR CL ATS is in EPR LIM mode with CL mode selected on the TRP ATS will maintain maximum climb thrust EPR CR ATS is in EPR LIM mode with CR mode selected on the TRP ATS will maintai...

Страница 115: ...TS is restricting thrust to prevent exceeding the slat limit airspeed This mode engages automatically when a speed higher than the slat limit speed is selected in the SPD MACH readout In this panel th...

Страница 116: ...nd preflight test in progress VOR VOR mode armed for capture of VOR course UP Automatic power up test in progress Go around Modes When the autopilot or flight director is engaged in LOC TRK and G S TR...

Страница 117: ...hold mode The DFGC will maintain the heading of the aircraft at the time the mode was engaged HDG SEL The autopilot is in heading select mode The DFGC is providing commands to maintain the heading in...

Страница 118: ...he autopilot is engaged in VOR mode and VOR station passage is occurring cone of silence The DFGC is maintaining the magnetic VOR course displayed in the CRS readout VOR TRK The autopilot is engaged i...

Страница 119: ...iated G S TRK The autopilot is engaged in either ILS or LAND mode and the glideslope of the selected ILS is being tracked GO Go around mode has been RND engaged If active the autopilot and or FD comma...

Страница 120: ...FD take off mode is engaged The DFGC will command the FD command bars to maintain a 10 degree pitch up TEST Autoland preflight test in progress TURB The Turbulence mode is engaged The DFGC maintains t...

Страница 121: ...Super 80 Professional AOM APU Section 9 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 9 APU...

Страница 122: ...Super 80 Professional AOM APU Section 9 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 9 APU 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 3...

Страница 123: ...rable in flight to supply an alternate source of electrical power The APU installed aft of the rear pressure bulkhead in the unpressurized area of the lower fuselage All APU controls and indicators ar...

Страница 124: ...onditioning turbine lowering temperature of conditioned air during ground operation Use of this switch position although providing cooler air significantly reduces cockpit cabin airflow OFF Remove ele...

Страница 125: ...Super 80 Professional AOM COMMUNICATIONS Section 10 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 10 COMMUNICATIONS...

Страница 126: ...ofessional AOM COMMUNICATIONS Section 10 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 10 COMMUNICATIONS 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND IN...

Страница 127: ...panel has two frequency selectors and a transfer switch to select the transmitter frequency to be used The VHF radios are located just aft of the throttle quadrant MODE S TRANSPONDER A Mode S transpo...

Страница 128: ...d VHF frequency 2 VHF FREQUENCY SELECTOR 2 Click the frequency readout to change the frequency 3 VHF TFR SWITCH The VHF transfer switch selects which frequency is currently active This permits communi...

Страница 129: ...threat The mode S transponder and altitude reporting are active 2 CODE READOUT Digital readout of the code numbers selected with the code selector knobs Also indicates which of the two transponders i...

Страница 130: ...ts for non threat category targets open white diamonds ABOVE Selects display of non threat targets up to 8700 feet above own aircraft and down to 2700 feet below own aircraft NORM Selects display of n...

Страница 131: ...IO INT SWITCH Momentary in RADIO only RADIO Keys radio transmission circuit for mask or boom microphone as selected by the microphone selector buttons INT Depending upon position of boom mask switch b...

Страница 132: ...Super 80 Professional AOM ELECTRICAL Section 11 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 11 ELECTRICAL...

Страница 133: ...OM ELECTRICAL Section 11 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 11 ELECTRICAL 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 4 WARNING A...

Страница 134: ...the event of loss of the other two generators For ground operations an external power source may be connected to the airplane The external power receptacle is located on the lower fuselage left side T...

Страница 135: ...olt batteries are connected in series to supply 28 volt DC power The battery is automatically being charged when electrical power is on the aircraft and the battery switch is ON When operating on emer...

Страница 136: ...D OIL TEMPERATURE GAUGE L R Indicates CSD oil outlet temperature or oil temperature rise across the drive 3 CSD TEMP PUSH FOR RISE BUTTON When actuated temperature rise outlet temperature minus inlet...

Страница 137: ...gether 14 DC BUS X TIE SWITCH CLOSE Connects left and right DC buses allowing any combination of T R s to power both DC buses OPEN Normal position Isolates left and right DC distribution systems 15 DC...

Страница 138: ...d Service Bus 3 APU PWR AVAIL LIGHT Blue Indicates that APU generator power is available 4 EXT PWR SWITCH OFF Removes external power from the Ground Service Bus ON Connects external power to the Groun...

Страница 139: ...lay Comes on to indicate oil pressure in CSD is below operating limits MASTER CAUTION lights also come on AC CROSSTIE LOCKOUT LIGHT Digital display Comes on to indicate AC crosstie relay is locked ope...

Страница 140: ...Super 80 Professional AOM FIRE PROTECTION Section 12 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 12 FIRE PROTECTION...

Страница 141: ...fessional AOM FIRE PROTECTION Section 12 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 12 FIRE PROTECTION 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND I...

Страница 142: ...d parallel to each other With the loop switch set to BOTH only one loop needs to detect a fire or overheat condition to activate the fire warning system Fire Warning System The fire warning for an eng...

Страница 143: ...ghts within the handle are turned on by the engine fire detection system or test circuit Pulling the handle will silence the aural warnings and shut off engine fuel 2 AGENT LOW Light 1 and 2 Amber Com...

Страница 144: ...E AGENT switches for subsequent discharge of fire extinguishing agent 1 LOOPS Selector Switch L Eng R Eng APU The Loops Selector switch connects the applicable engine or APU to the selected fire detec...

Страница 145: ...Super 80 Professional AOM FLIGHT CONTROLS Section 13 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 13 FLIGHT CONTROLS...

Страница 146: ...t Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 13 FLIGHT CONTROLS 0 TABLE OF CONTENTS 1 GENERAL 2 MAJOR COMPONENT LOCATION 7 LONGITUDINAL CONTROL AND TRIM 8 RUDDER CONTROL AND TRIM 11 SPEED...

Страница 147: ...ntrol tab An anti float tab geared to horizontal stabilizer movement is installed outboard of the gear tab The purpose of the anti float tab is to fly the elevator up when the horizontal stabilizer is...

Страница 148: ...nob on the pedestal Rudder Throw Limiter A Rudder Throw Limiter is installed to protect the empennage from overload in case of inadvertent application of excessive rudder control The limiter operates...

Страница 149: ...o the armed position Arming the spoilers for take off without positioning the AUTO BRAKE selector to TO causes the take off warning horn to sound when the throttles are advanced accompanied by the wor...

Страница 150: ...s operated by moving the trim control handle on the pedestal Operation of the trim control handle will cause the autopilot to disengage A cable operated indicator moves fore and aft along a track on t...

Страница 151: ...ill be activated At stall the claxon aural warning and vocal Stall will sound Stall warning light will come one Stick Pusher will be activated Autoslats When the flap slat handle is set to the 0 13 de...

Страница 152: ...Super 80 Professional AOM FLIGHT CONTROLS Section 13 Page 7 Super 80 Professional Aircraft Operating Manual Coolsky 2018 MAJOR COMPONENT LOCATION...

Страница 153: ...M Control Column 2 Movement of the control wheel deflects an aileron control tab Aerodynamic forces on the control tab moves the aileron 1 AILERON TRIM Control Rotate the trim control knob left or rig...

Страница 154: ...lsky 2018 1 ALT LONG TRIM Control Alternate longitude trim control Currently not simulated 2 STABILIZER TRIM PRIMARY MOTOR BRAKE Switch This switch is only used to stop a runaway stabilizer condition...

Страница 155: ...lizer It indicates position and movement of the stabilizer 3 LONG TRIM TAKE OFF POSITION Indicator This indicator is positioned by the Take off Condition Computer based on CG and flap setting input Th...

Страница 156: ...d 2 RUDDER TRIM Control Rotate trim knob left or right to trim rudder during power operation and trim rudder control tab during manual operation 3 RUDDER TRIM Indicator Indicates the amount of left or...

Страница 157: ...r aft to the EXT position On the ground the lever is used deploy all spoiler panels flight spoilers and ground spoilers Automatic mode When the speedbrakes are armed prior to landing all spoiler panel...

Страница 158: ...orizontal bars which move vertically to indicate the position of the left and right flaps respectively 3 SLAT ADVISORY LIGHTS TAKE OFF Blue Indicates the FLAP SLAT lever and wing slats are in the take...

Страница 159: ...Turns the test off normal operating mode SYS1 Tests the left stall system Same tests performed as with SYS2 2 MACH TRIM COMP Switch NORM The system will automatically provide Mach trim when needed OV...

Страница 160: ...w damper is not operating SPOILER DEPLOYED Digital display Comes on to indicate Ground Spoiler is extended in flight or any spoiler is deployed on the ground with the spoiler lever in the stowed posit...

Страница 161: ...Super 80 Professional AOM FLIGHT INSTRUMENTS Section 14 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 14 FLIGHT INSTRUMENTS...

Страница 162: ...E OF CONTENTS SECTION 14 FLIGHT INSTRUMENTS 0 TABLE OF CONTENTS 1 GENERAL 2 AIRSPEED MACH INDICATOR 4 CADC AND STATIC AIR SWITCHING 5 TAS SAT INDICATOR 6 ALTIMETER 7 RADIO ALTIMETER 8 SLIP INDICATOR 8...

Страница 163: ...nput to the Captain s primary instruments and CADC 2 provides input to the FO s primary instruments In the event of a CADC failure either CADC may be selected to provide input to both the Captain s an...

Страница 164: ...be heard from the Central Audio Warning System CAWS until airspeed is back below 280 knots or the slats are retracted Standby Instruments The standby instruments consist of the standby horizon standby...

Страница 165: ...tes computed airspeed 4 AIRSPEED REFERENCE BUGS Freely movable pointers normally used to alert the pilot to specified airspeeds Click the corners and center top part of the ASI to manually position th...

Страница 166: ...in s and FO s primary instruments receive input from CADC 1 BOTH ON 2 Both the Captain s and FO s primary instruments receive input from CADC 2 2 CADC LIGHT Amber The light comes on to indicate that t...

Страница 167: ...erating Manual Coolsky 2018 TAS SAT INDICATOR 1 TAS READOUT Digital readout of computed True Air Speed in knots 2 SAT READOUT Digital readout of Standard Air Temperature in degrees Celsius 3 TAT BUTTO...

Страница 168: ...nuously rotating drum which indicates barometric altitude from 1000 to 50 000 feet The leftmost number on the drum counter is marked green in the 0 position to alert of altitudes of less than 10 000 f...

Страница 169: ...Height as set with the DH knob on the EFIS Control Panel 4 DECISION HEIGHT BUG Green The Decision Height Bug is set using the Set Knob The bug travels with the altitude tape 5 DH Annunciator Yellow T...

Страница 170: ...ot simulated 5 100 FOOT POINTER The pointer will make a full circle for each 1 000 feet of altitude gained or lost 6 DIGITAL READOUT The Digital Readout is made with a continuously rotating drum excep...

Страница 171: ...ky 2018 VERTICAL SPEED INDICATOR 1 VERTICAL SPEED POINTER The pointer indicates vertical speed in feet per minute 2 TA SEL Pushbutton The VSI doubles as a TCAS display in addition to displaying vertic...

Страница 172: ...deviation from the glideslope The Rising Runway symbol will be rising until it appears to touch the aircraft symbol at actual touchdown The symbol is removed from view when no glideslope is tuned 6 F...

Страница 173: ...n from the center of the localizer beam The pointer is removed from view when no localizer is tuned When PLAN or MAP mode is active on ND the pointer indicates deviation from FMS flight plan cross tra...

Страница 174: ...is unusable 4 F S FAIL LEGEND Appears when input data for slow fast indications are unusable 5 EFIS STATUS LEGEND Appears when the EFIS Selector switch is out of the NORM position EFI 1 EFIS Selector...

Страница 175: ...S select knob on the VHF NAV control panel In NAV mode the Course Pointer indicates the desired track to the next waypoint 5 HEADING CURSOR The Heading Cursor indicates selected heading set by HDG kno...

Страница 176: ...Super 80 Professional AOM FLIGHT MANAGEMENT Section 15 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 15 FLIGHT MANAGEMENT...

Страница 177: ...Page 12 Performance Initialization Page 14 Takeoff Reference Page 15 Approach Reference Page 16 Reference Navigation Data Page 17 Route Page 18 Legs Page 21 Legs Page Continued 22 Legs Page Continued...

Страница 178: ...selection and tuning of DME stations for accurate estimation of aircraft position FMS Components The FMS consists of one Advanced Flight Management Computer AFMC and two Multipurpose Control and Disp...

Страница 179: ...ved with the SAVE feature Enter LOAD followed by a filename separated by space to load saved FMS data from a file Example LOAD VHHH ZSSS 2 Example Enter LOAD VHHH ZSSS 2 into the scratchpad and press...

Страница 180: ...de and function keys line select keys and annunciator lights 1 Light Sensor Senses ambient light and automatically adjusts reference brightness level not simulated 2 Data Display Area The CRT is parti...

Страница 181: ...a second time changes to a plus 8 Alpha Numeric Keys Push to enter selected character into the scratchpad 9 Function Keys EXEC Command key of the FMS Push to implement changes to the active flight pla...

Страница 182: ...to the FMS POS INIT REF page NAV This is the normal in flight switch position When IRS alignment is complete navigation and attitude data will be available ATT Only attitude data is available Note Whe...

Страница 183: ...can supply commands to fly a constant heading track or follow a DME arc not simulated NAV Engagement NAV mode may be coupled to the DFGS by selecting NAV on the FGCP as long as the following conditio...

Страница 184: ...eed Holding Pattern Entry The aircraft must first pass the holding waypoint before entering the holding pattern The FMS will use three types of hold entry depending on the entry angle 1 Direct entry 2...

Страница 185: ...ile calculated by entering forecast winds anti ice requirements not simulated or changing the target speed For deviation below the vertical profile the FMS will make corrections through throttle comma...

Страница 186: ...de such as VERT SPD The armed mode becomes active such as G S armed to G S CAP A loss of data sensor required for VNAV A loss of navigation data position or velocity The Autopilot and both Flight Dire...

Страница 187: ...es the flight management computer This is the only subsystem on AHRS aircraft Not simulated IRS INIT REF Provides access to the IRS INIT REF page Not simulated Initialization Reference Index Page INIT...

Страница 188: ...abase INDEX Push to display the INIT REF INDEX page POS INIT Push to display the POS INIT page Position Initialization Page POS INIT PAGE 1 3 Displays position page for starting AFMC and IRU alignment...

Страница 189: ...selection LAST POS REF AIRPORT or GATE ROUTE Push to display the RTE 1 or 2 page GMT The Captain s clock provides time input to the FMC The first two digits hours can be changed by MCDU entries The mi...

Страница 190: ...simulated INDEX Push to display the INIT REF INDEX page ROUTE Push to display the RTE 1 or 2 page Performance Initialization Page PERF INIT PAGE This page provides for insertion of performance data i...

Страница 191: ...ght level Valid entries are XXX flight level FLXXX or XXXXX feet CRZ WIND Cruise Wind Enter expected wind at cruise level Valid entry for wind and speed are 3 digits each Entries are propagated to the...

Страница 192: ...d DEPARTURE pages When all preflight entries have been complete PRE FLT COMPLETE is displayed INDEX Push to display the INIT REF INDEX page V1 VR and V2 Values for V speed may be entered for display p...

Страница 193: ...ated landing flap setting at the selected displayed gross weight The VREF fields are blank prior to entering a gross weight on the PERF INIT page or on this page FRONT CRS Displays the ILS front cours...

Страница 194: ...raft position is displayed INDEX Push to display the INIT REF INDEX page ELEVATION Displayed for navaids airports and runways only otherwise blank LENGTH Displayed for runways only otherwise blank NAV...

Страница 195: ...plans For further information on how to load P3D flight plans into the FMS please refer to the General chapter under Section 15 of this AOM RUNWAY Valid entries are origin airport runways contained in...

Страница 196: ...ayed for discontinuities gaps in route Dashes are displayed at end of route ACTIVATE Displayed on non active RTE page only After activation on the ground the ACTIVATE prompt is replaced with PERF INIT...

Страница 197: ...active waypoint All the waypoints of the route are displayed on the legs pages in flight sequence The flight crew can change the sequence delete or add new waypoints to the route on the legs pages New...

Страница 198: ...ght level FLXXX or XXXXX feet Speed constraint entries also require a corresponding altitude constraint entry Small characters indicate estimates computed by the AFMC Large characters indicate pilot e...

Страница 199: ...hat after waypoint NOSON the route includes a published procedure turn It also indicates a conditional waypoint at the point where the procedure turn is completed and a 172 course to NOSON is intercep...

Страница 200: ...key or ACTIVATE line select key or any RTE page and then pushing the INTC LEG TO line select key The INTC CRS prompt permits entry of a course intercept to a waypoint After course entry and appropria...

Страница 201: ...s made on the PERF INIT page 000 00 is displayed The flight crew can overwrite cruise winds Wind field is blank for waypoints other than cruise waypoints LEGS Selection displays the RTE LEGS page SELE...

Страница 202: ...tion can then be transferred to the prompt boxes to create a holding pattern with the fix at the present position when the EXEC key is pushed ACT RTE 1 HOLD This page is used to modify holding pattern...

Страница 203: ...t Altitude SPD TGT ALT Displays target speed and altitude If not specified dashes are displayed Entry of a TGT ALT higher than the waypoint altitude results in a climb after entering holding Entry of...

Страница 204: ...orts or each route and for any other airport in the database Active Label ACT Displayed next to route number when it is active DEP RTE 1 Selects departures for origin airport in route 1 DEP RTE 2 Sele...

Страница 205: ...and transitions for the selected SID are displayed SEL appears next to the selected SID If the SID is runway dependent a runway must be selected before the SID can be activated and entered into the ro...

Страница 206: ...nt a runway must be selected before the STAR can be activated and entered into the route TRANSITION Selection causes that transition to be entered into the route SEL appears next to the selected trans...

Страница 207: ...on is in progress information on the Progress page is relative to the modified flight plan An alternate destination waypoint may be entered over the displayed destination The DEST label is replaced wi...

Страница 208: ...ine Displays headwind H WIND tailwind T WIND and crosswind X WIND Wind is resolved on heading XTK ERROR Crosstrack Error Display Indicates the distance the aircraft is left or right of the active rout...

Страница 209: ...bearing from the fix Up to three bearings may be entered When entering a bearing the radial and distance from the fix to the intersection with the flight plan route will be displayed Additionally ETA...

Страница 210: ...rom the PERF INIT page Valid entries are XXX flight level XXXXX feet Entries are automatically displayed as flight levels or altitudes based on the transition altitude on the PERF INIT page Values gre...

Страница 211: ...the altitude will be reached MAX ANGLE Displays maximum angle of climb speed ENG OUT Currently not simulated CLB DIR Climb Direct Displayed when climb is active and an altitude constraint exists on t...

Страница 212: ...PENALTY when appropriate The SAVINGS or PENALTY readout will be suffixed by W MOD if a flight plan modification is pending Blank if no step altitude is displayed FUEL AT XXXX Fuel at Destination Disp...

Страница 213: ...s flight data for the descent phase of the flight enabling the flight crew to evaluate and revise the vertical flight profile Available speed modes are ECON SPD SEL and POLICY The page will be blank i...

Страница 214: ...raint AT SOVIR The first waypoint speed altitude constraint on the active route is displayed here when constraints have been entered on a RTE LEGS page procedure or by crew entry When passing the wayp...

Страница 215: ...llow the AFMC to more accurately calculate the descent path TRANS LVL Transition Level Automatically displays 18 000ft but can be change by the flight crew WIND SPD Wind Speed Permits entry of altitud...

Страница 216: ...h IRS Mode Select switches to NAV Observe ON BAT annunciations illuminate during self test extinguish and then the ALIGN annunciations will illuminate Select the FMS POS INIT page Enter present positi...

Страница 217: ...tion Select the RTE page RTE key Clear previous route o Enter a new origin or re enter the previous origin to clear the route Enter a destination airport Enter runway and route information o If runway...

Страница 218: ...peed is controlled by the AFMC according to the set cost index o A zero cost index yields minimum fuel burn low speed o A 999 cost index yields minimum flight time high fuel burn high speed Enter flig...

Страница 219: ...key Enter the desired waypoint ident into the DIRECT TO boxes Review the modified route on the ND Execute the modified route Intercepting a leg to a waypoint Select the DIRECT TO page for the active r...

Страница 220: ...the modified route Select the DIRECT TO page for the active route DIR INTC key Enter the first waypoint on the airway leg to be intercepted into the INTC LEG boxes Execute the modified route Route di...

Страница 221: ...from the fix on the DNTKFX downtrack fix line or press the ABEAM prompt if the desired radial should be perpendicular to the route course Line select the DNTKFX or ABM line to the scratchpad Select t...

Страница 222: ...ute discontinuities Review the modified route on the ND Execute the modified route Contingency route Select the RTE page RTE key Line select RTE 2 Enter desired route information Review route 2 on the...

Страница 223: ...ll appear If there is already a hold present in the route the hold data for the first hold in the route will be displayed Line select NEXT HOLD to enter another hold into the route Enter the desired h...

Страница 224: ...ude on the Flight Guidance Control Panel Press the VNAV button Setting a speed altitude constraint at a waypoint Select the LEGS page LEGS key Enter speed altitude and line select it into the desired...

Страница 225: ...trol Panel Descent At Top of Descent TD o When the Thrust Rating Panel is set to CR Cruise mode and a lower altitude is armed on the altitude select panel on the Flight Guidance Control Panel the AFMC...

Страница 226: ...nation Determining distance to cross radial from a fix Select the FIX page FIX key Enter the desired fix identifier Enter the desired radial from the fix on the DNTKFX downtrack fix line or press the...

Страница 227: ...p climb evaluation Select the CRZ page CRZ key Enter desired STEP TO altitude Enter wind direction and speed if known at the step to altitude Check savings Descent forecast Select the DES page DES key...

Страница 228: ...Super 80 Professional AOM FUEL Section 16 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 16 FUEL...

Страница 229: ...Section 16 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 16 FUEL 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 3 WARNING AND CAUTION INDICATO...

Страница 230: ...Fuel loaded in the center tank should be used before the main wing tank fuel The two center tanks pumps are connected in series to provide higher pressure than that of the wing tank pumps connected i...

Страница 231: ...ying fuel pressure to the right engine and APU 2 FUEL BOOST PUMP SWITCHES left center right aft and forward OFF Turns off applicable fuel boost pumps ON Turns on applicable fuel boost pumps 3 FUEL HEA...

Страница 232: ...ck to display fuel flow A blue light will illuminate the USED legend 3 FUEL USED RESET SWITCH When the switch is pushed the digital fuel used counter is reset to zero The digital readout will momentar...

Страница 233: ...Opens fuel cross feed valve allowing either or both main tanks to feed both engines and APU 2 FUEL CONTROL LEVERS L R Fuel lever lock release button must be depressed to unlock lever prior to actuatio...

Страница 234: ...pressure from the center tank pumps This is usually a result of the center tank becoming empty FUEL LEVEL LOW Digital display Comes on to indicate either wing main tank fuel quantity has reached 2500...

Страница 235: ...532 9 266 19 032 FULL 500 19 532 1 000 20 032 1 500 20 532 2 000 21 032 2 500 21 532 3 000 22 032 3 500 22 532 4 000 23 032 4 500 23 532 5 000 24 032 5 500 24 532 6 000 TOTAL FUEL LOAD LEFT RIGHT MAI...

Страница 236: ...Super 80 Professional AOM HYDRAULICS Section 17 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 17 HYDRAULICS...

Страница 237: ...OM HYDRAULICS Section 17 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 17 HYDRAULICS 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 3 WARNING A...

Страница 238: ...ressure or low pressure mode The high pressure mode provides 3000 PSI and is used for taxi take off and landing The low pressure mode provides 1500 PSI and is selected on the After Take off Checklist...

Страница 239: ...WITCH L R HI Engine driven pump operate at 3000 PSI upper green band LOW Engine driven pump operate at 1500 PSI lower green band OFF No pressure output for system circulation other than pump lubricati...

Страница 240: ...r 80 Professional Aircraft Operating Manual Coolsky 2018 WARNING AND CAUTION INDICATORS HYD PRESS LOW LIGHTS L R Digital display Comes on when hydraulic pressure to the spoiler supply system drops bel...

Страница 241: ...Super 80 Professional AOM LANDING GEAR Section 18 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 18 LANDING GEAR...

Страница 242: ...LANDING GEAR Section 18 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 18 LANDING GEAR 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 5 WARNING...

Страница 243: ...in the forward lower section of the nose of the airplane A ground shift mechanism mounted on the nose gear strut is operated by compression and extension of the nose gear strut This mechanism is used...

Страница 244: ...ing gear is down and locked Nose gear verification is provided by a green indicator pin on the pedestal just behind the throttle quadrant Brakes Each main gear wheel is fitted with a dual system disc...

Страница 245: ...he system compares actual airplane deceleration with the pilot s selection In the MAX position full brake system pressure is applied to the brakes and maximum deceleration is limited to anti skid syst...

Страница 246: ...n to indicate either one or both main gear doors are not fully closed and locked 3 NOSE GEAR DOWN LOCK INDICATOR A pin indicator green will appear up when the nose gear is down and locked The pin will...

Страница 247: ...ted on the right hand side of the pedestal on the floor Open the cover plate to uncover the lever 2 NOSE GEAR STEERING WHEEL The Nose Gear Steering Wheel provides control of the nose gear steering dur...

Страница 248: ...or automatic braking during take off or landing The switch is magnetically held in the arm position DISARM ABS is inoperative Manual braking available 6 AUTO BRAKE Selector TO Provides automatic braki...

Страница 249: ...HT LIGHT Comes on when the brake temperature exceeds 305 C and goes off when the temperature has cooled to 260 C 3 BRAKE TEMP TEST BUTTON Tests the brake temperature circuit and overheat light Tempera...

Страница 250: ...ON Digital display Comes on to indicate the parking brakes are set L OUTBD ANTI SKID Digital display L INBD ANTI SKID Digital display R OUTBD ANTI SKID Digital display R INBD ANTI SKID Digital display...

Страница 251: ...Super 80 Professional AOM MISCELLANEOUS Section 19 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 19 MISCELLANEOUS...

Страница 252: ...ENTS SECTION 19 MISCELLANEOUS 0 TABLE OF CONTENTS 1 EXTERIOR LIGHTING 2 COCKPIT LIGHTING 3 VOICE RECORDER 5 ELECTRONIC OVERHEAD ANNUNCIATON PANEL EOAP 6 Warning and Advisory Lights 7 Electrical Warnin...

Страница 253: ...y 2 NOSE LTS OFF Nose landing and taxi lights are off DIM Nose landing and taxi lights are dim not simulated BRT Nose landing and taxi lights are on 3 GRD FLOOD LTS Turns the ground flood lights on of...

Страница 254: ...im off switch for circuit breaker panel floodlights 2 STBY COMP LT Switch On dim off switch for standby compass floodlights 3 THNDRSTRM LT Switch OFF Lighting is controlled individually by the FO and...

Страница 255: ...douts of the Flight Mode Annunciator FLOOD On off switch for instrument panel flood lights CTR INSTR PED LTS Knobs PANEL On off switch for center instrument panel integral lights DIGITAL On off switch...

Страница 256: ...s The test cycle is completed in 5 seconds 3 ERASE Button When the Erase button is pushed and held for more than 2 seconds the tape will be erased The aircraft must be on the ground and the parking br...

Страница 257: ...annunciations stored off screen 3 CUE LIGHTS 7 The associated system cue light ELEC ICE ENG CTRL MISC HYD or DOOR will flash 4 times on detection of a caution and a new annunciation is displayed on t...

Страница 258: ...for wing leading edge and strakes 9 TAIL DE ICE ON Blue Indicates de ice heat has been selected for the leading edge of the horizontal stabilizer 10 TAIL COMPT TEMP HIGH Not in use 11 APU FIRE Red Com...

Страница 259: ...mes on to indicate either left or right DC bus is not powered MASTER CAUTION lights also come on Engine Warnings ENG SYNC ON Comes on to indicate ENG SYNC switch is selected to N1 or N2 when landing g...

Страница 260: ...tank fuel quantity has reached 2500 pounds PITOT STALL HEATER OFF Comes on to indicate METER SEL HEATER selector in OFF MASTER CAUTION light also comes on APU OIL PRESS LOW Comes on the APU oil pressu...

Страница 261: ...WAY DOOR Comes on to indicate the aft stairway door is open AFT CABIN DOOR Comes on to indicate the aft cabin door is open AFT GALLEY DOOR Comes on to indicate the aft galley door is open FWD STAIRWAY...

Страница 262: ...Super 80 Professional AOM NAVIGATION Section 20 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 20 NAVIGATION...

Страница 263: ...OF CONTENTS SECTION 20 NAVIGATION 0 TABLE OF CONTENTS 1 GENERAL 2 VHF NAV CONTROL PANEL AND ADF CONTROL PANEL 3 RADIO DISTANCE MAGNETIC INDICATOR RDMI 4 NAVIGATION DISPLAY ROSE MODE 5 NAVIGATION DISP...

Страница 264: ...ading inputs from an associated flux valve Compass heading is displayed on the compass indicators and NDs at all times VHF Navigation System There are two independent VHF navigation systems VOR1 LOC1...

Страница 265: ...frequency 4 VOR LOC FREQUENCY SELECTOR Click the numbers in the course readout to increase and or decrease the course 5 VHF NAV CP 1 2 SELECTOR In this panel NAV1 and NAV2 are located on top of each...

Страница 266: ...OR ADF 1 selector knob 3 VOR ADF 2 POINTER Indicates bearing to VOR or ADF station as selected on the VHF NAV radio or ADF control panel VOR ADF function is selected with the VOR ADF 2 selector knob 4...

Страница 267: ...N DISPLAY Indicates vertical deviation from the glideslope The display is removed from view when no valid ILS frequency is tuned on the applicable VHF NAV radio 6 ADF 1 INDICATOR Indicates ADF is sele...

Страница 268: ...tuned on the applicable VHF NAV radio 5 TO FROM ARROW Indicates direction to from the selected station 6 VOR ILS NAV Indicates current navigation mode VOR VOR mode selected ILS ILS mode selected NAV F...

Страница 269: ...enta Indicates selected VOR LOC course as set by the CRS SELECT knob on the applicable VHF NAV radio 11 ADF POINTER Blue Indicates ADF bearing to the selected station The pointer is removed when the s...

Страница 270: ...t waypoint 5 VOR ILS NAV Indicates current navigation mode VOR VOR mode selected ILS ILS mode selected NAV FMS mode selected NAV 1 in amber indicates both pilots in MAP or PLAN mode An amber box is pl...

Страница 271: ...LECT knob on the applicable VHF NAV radio 4 ESTIMATED TIME OF ARRIVAL ETA Displays the ETA to the next waypoint 5 VOR ILS NAV Indicates current navigation mode VOR VOR mode selected ILS ILS mode selec...

Страница 272: ...ND on off Note Only ADF 1 is simulated 3 RANGE SELECTOR Selects desired range with associated range marks 4 DECLUTTER BUTTONS 4 The declutter buttons remove information from the ND in order to make th...

Страница 273: ...Super 80 Professional AOM OXYGEN Section 21 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 21 OXYGEN...

Страница 274: ...er 80 Professional AOM OXYGEN Section 21 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 21 OXYGEN 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS...

Страница 275: ...itch must be set to ON the diluter control switch to NORMAL OXYGEN and the TEST MASK NORMAL EMERGENCY switch to NORMAL This setup will supply oxygen to the masks upon demand In the event of a cabin de...

Страница 276: ...MAL This is the normal operating position TEST MASK Momentary The regulator supplies oxygen under pressure to the masks for testing purposes 3 DILUTER DEMAND CONTROL 100 OXYGEN The regulator supplies...

Страница 277: ...Super 80 Professional AOM POWER PLANT Section 22 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 22 POWER PLANT...

Страница 278: ...POWER PLANT Section 22 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 22 POWER PLANT 0 TABLE OF CONTENTS 1 GENERAL 2 CONTROLS AND INDICATORS 5 WARNING A...

Страница 279: ...he starter of the respective engine Ignition Systems Two ignition systems one 20 Joule high energy ignition system and one four Joule low energy ignition system are provided for each engine An IGN ign...

Страница 280: ...the operating engine The ART system consists of a two position switch and three annunciator lights A green ready light comes on when the ART self test has been completed The amber ART light comes on w...

Страница 281: ...e Five seconds after the nose gear indicates down and locked the engines shift from normal idle to approach idle Approach idle RPM is approximately 10 higher than normal idle RPM During landing five s...

Страница 282: ...d for one minute opening shutoff valve supplying hot air to air fuel heat exchanger FUEL HEAT ON annunciator light comes on OFF Removes power from fuel heat circuit 3 ENGINE START SWITCH L R FLT Provi...

Страница 283: ...2018 1 THRUST REVERSER LEVER L R Moving thrust reverser lever aft actuates thrust reverser 2 THROTTLE L R Each throttle is cable connected to its respective engine fuel control unit to regulate engine...

Страница 284: ...n thrust reverser are unlatched and extending 3 ENGINE PRESSURE RATIO L R See section 21 page 9 4 N1 TACHOMETER L R Indicates RPM of N1 compressor stage 5 EGT L R Indicates exhaust gas temperature in...

Страница 285: ...ure drops below 35 PSI Oil pressure below 40 PSI is tolerable for low power settings Oil pressure below 35 PSI requires a precautionary engine shutdown If the oil pressure exceeds 56 PSI the display w...

Страница 286: ...ating Panel 5 EPR READOUT Digital readout of current operating engine pressure ratio of engine EPR pointer displays corresponding value 6 ASSUMED TEMPERATURE SELECTOR Rotate knob to set assumed temper...

Страница 287: ...is released the EPR LIM flag will appear the NO MODE light will come on and all mode buttons will be off 10 RAT READOUT Displays digital readout of RAM air temperature 11 ASSUMED TEMPERATURE READOUT T...

Страница 288: ...indicate ENG SYNC switch is selected to N1 or N2 when landing gear handle is in the down position 31 38 L R START VALVE OPEN Amber Comes on to indicate the engine starter valve is open allowing bleed...

Страница 289: ...Super 80 Professional AOM PERFORMANCE Section 23 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 23 PERFORMANCE...

Страница 290: ...ND 24 8 MINIMUM V1 VMCG 9 MINIMUM VR 9 MINIMUM V2 9 CLIMB 10 MAX CLIMB EPR 10 MAX CONTINUOUS EPR 11 CRUISE 12 MAX CRUISE EPR 12 320 KNOT CRUISE 13 MACH 76 CRUISE 14 MACH 77 CRUISE 15 MACH 78 CRUISE 16...

Страница 291: ...which prohibit the use of standard thrust Tailwind Snow slush ice or standing water on the runway De ice anti ice fluid has been applied and temperatures at or below 6 C 42 F Engine anti ice ON MEL it...

Страница 292: ...aft configurations and weights The maneuvering landing Speed Cards provide the pilots with various maneuvering landing speeds such as for example VREF for various aircraft configurations and weights S...

Страница 293: ...7 9 8 7 9 9 07 6 9 7 7 8 4 9 5 08 6 6 7 4 8 1 9 1 09 6 3 7 1 7 9 8 8 10 6 1 6 9 7 6 8 5 11 5 8 6 6 7 3 8 1 12 5 6 6 3 7 1 7 7 13 5 4 6 0 6 8 7 4 14 5 2 5 8 6 5 7 1 15 5 0 5 6 6 2 6 7 16 4 8 5 3 5 9 6...

Страница 294: ...1 72 1 72 RESERVE TAKE OFF N1 BASED ON AC Pack ON Airfoil Anti Ice ON or OFF Engine Anti Ice ON or OFF CORRECTION AC Pack OFF 0 9 OAT F PRESSURE ALTITUDE 1000 FEET 1000 0 1000 2000 3000 4000 5000 40 8...

Страница 295: ...90 9 20 84 3 86 2 87 3 88 3 89 4 90 6 91 8 30 85 1 87 1 88 2 89 2 90 3 91 5 92 8 40 86 0 88 0 89 1 90 1 91 2 92 4 93 7 50 86 9 88 9 89 9 91 0 92 1 93 3 94 7 60 87 7 89 7 90 8 91 9 93 0 94 3 95 6 70 8...

Страница 296: ...170 161 165 170 163 165 170 164 166 170 166 167 170 160 167 170 177 168 170 177 170 171 177 172 172 177 173 173 177 175 175 177 F L A P S 11 90 130 119 127 103 117 125 104 115 123 106 115 121 107 115...

Страница 297: ...138 145 135 138 145 137 138 145 139 139 145 140 140 145 142 142 145 150 141 144 150 143 144 150 144 145 150 146 146 150 148 148 150 150 150 1 50 F L A P S 24 90 95 115 123 96 113 120 97 111 118 96 10...

Страница 298: ...0 TO S L 2000 4000 6000 8000 40 TO 65 121 119 117 114 110 70 121 119 117 112 109 80 121 119 115 111 107 90 120 117 112 109 105 100 118 114 110 106 103 110 116 112 108 104 120 114 110 122 113 109 MINIM...

Страница 299: ...0 feet 0 9 Engine Anti Ice 0 08 Airfoil Anti Ice 2 Engines Operating 0 02 1 Engines Operating 0 04 PRESS 20 RAT C ALT AND FEET BELO W 10 0 10 20 30 40 50 SL 1 96 1 96 1 92 1 86 1 78 1 74 1 73 1 61 100...

Страница 300: ...82 1 76 4000 2 04 2 04 2 00 1 99 1 98 1 96 1 90 1 83 1 82 1 76 5000 2 06 2 04 2 00 1 99 1 98 1 96 1 90 1 83 1 82 1 76 10000 2 06 2 04 2 00 1 99 1 98 1 96 1 90 1 83 1 82 1 76 15000 2 05 2 03 2 00 1 98...

Страница 301: ...000 2 04 1 97 1 90 1 83 1 77 1 68 1 58 1 49 25000 2 03 1 97 1 90 1 83 1 76 1 68 1 58 1 48 27000 2 05 1 99 1 92 1 85 1 78 1 70 29000 2 07 2 01 1 93 1 86 1 80 1 71 31000 2 07 2 01 1 94 1 87 1 80 1 72 33...

Страница 302: ...7 320 19 1 52 1 51 1 50 1 49 1 49 1 48 1 48 1 47 1 47 1 46 1 46 1 45 1 44 1 44 1 43 49 6 50 1 50 6 51 0 51 4 51 8 52 2 52 6 53 1 53 6 54 0 54 4 54 8 55 2 55 7 15 395 320 15 1 48 1 47 1 46 1 45 1 45 1...

Страница 303: ...66 4 1 78 67 5 1 76 68 6 1 75 69 7 1 74 70 8 1 72 71 9 1 71 72 9 1 70 74 1 1 68 75 2 1 67 76 3 1 66 77 4 1 65 78 5 1 64 79 6 1 63 80 6 29 450 294 17 1 78 61 8 1 76 62 8 1 75 63 7 1 74 64 7 1 72 65 6...

Страница 304: ...5 1 73 71 6 1 71 72 8 1 70 73 9 1 69 75 0 1 68 76 1 1 66 77 1 1 65 78 1 1 64 79 1 29 456 298 16 1 80 60 7 1 78 61 6 1 77 62 5 1 76 63 4 1 74 64 3 1 73 65 2 1 72 66 2 1 71 67 1 1 69 68 0 1 68 68 9 1 67...

Страница 305: ...7 76 4 1 66 77 4 29 462 302 16 1 82 59 1 1 81 60 0 1 79 60 9 1 78 61 8 1 76 62 8 1 75 63 7 1 74 64 6 1 73 65 5 1 71 66 4 1 70 67 3 1 69 68 3 1 68 69 1 1 67 69 9 1 66 70 8 1 65 71 8 1 64 72 3 27 466 31...

Страница 306: ...66 4 1 78 67 6 1 77 68 6 1 76 69 7 1 74 70 7 1 73 71 7 1 72 72 6 29 474 311 16 1 91 53 9 1 89 55 1 1 87 56 1 1 85 57 3 1 84 58 3 1 82 59 3 1 81 60 3 1 79 61 3 1 78 62 2 1 76 63 1 1 75 64 0 1 74 64 8...

Страница 307: ...4 442 436 432 417 400 379 353 60 4 63 0 66 3 68 9 72 2 76 5 80 7 27 38 1 72 1 69 1 64 1 62 1 55 1 49 1 45 300 295 286 276 263 248 238 443 435 422 407 388 366 351 59 0 61 4 64 0 67 0 70 3 74 4 78 3 25...

Страница 308: ...idle power below 10 000 feet down to initial approach configuration Clean configuration above 2000 feet Add 80 pounds fuel burn for each minute of terminal area maneuvering PRESSURE ALTITUDE FEET TO S...

Страница 309: ...5 4 5 1 4 9 4 7 4 4 4 2 4 0 23 31 6 3 6 1 5 8 5 6 5 4 5 1 4 9 4 7 4 5 4 3 4 1 21 47 6 3 6 1 5 8 5 6 5 4 5 2 5 0 4 8 4 5 4 3 4 1 19 23 6 3 6 1 5 9 5 6 5 4 5 2 5 0 4 8 4 6 4 4 4 2 17 19 6 4 6 2 6 0 5 7...

Страница 310: ...RRIVAL MINIMUM CONTROL SPEEDS VMCA BASED ON Slats Extended One Engine Inoperative Max Reserve Thrust Any Bleed Air Configuration TEMP F FLAPS 4 EXT 11 EXT 17 EXT 24 EXT 81 BELOW 119 116 114 111 102 11...

Страница 311: ...3000 2 02 2 02 4000 2 04 2 03 5000 ABOVE 2 06 2 03 GO AROUND N1 BASED ON Both AC Packs ON Engine Anti Ice ON or OFF CORRECTION AC Pack OFF 0 5 Airfoil Anti Ice ON 2 Engines Operating 0 5 1 Engine Oper...

Страница 312: ...169 172 174 176 177 15 EXT MIN MAN 128 131 134 136 139 142 144 147 149 152 154 157 159 162 164 166 169 171 173 174 28 EXT MIN MAN 119 122 124 127 130 132 135 137 139 142 144 146 149 151 153 155 157 15...

Страница 313: ...TOMATIC BRAKE SYSTEM TOUCHDOWN TO FULL STOP BASED ON Flaps 28 or 40 Spoilers deployed No wind No reverse thrust CORRECTIONS ABS SETTING FOR TAILWINDS ADD FEET PER EACH 5 KNOTS TAILWIND FOR TEMP DEV AD...

Страница 314: ...6 16 6 6 13 6 23 30 335 13 31 7 13 30 0 12 28 4 11 26 9 11 25 4 10 24 1 10 22 8 9 21 5 9 20 4 8 19 2 8 18 2 7 17 1 7 16 1 6 15 1 6 14 2 6 13 3 5 12 4 21 26 326 12 28 2 11 26 7 10 25 3 10 24 0 9 22 8...

Страница 315: ...Super 80 Professional AOM WARNING SYSTEMS Section 24 Page 0 Super 80 Professional Aircraft Operating Manual Coolsky 2018 SECTION 24 WARNING SYSTEMS...

Страница 316: ...TEMS Section 24 Page 1 Super 80 Professional Aircraft Operating Manual Coolsky 2018 TABLE OF CONTENTS SECTION 24 WARNING SYSTEMS 0 TABLE OF CONTENTS 1 RADAR 2 GROUND PROXIMITY WARNING SYSTEM 5 WARNING...

Страница 317: ...d red colors Areas of light precipitation or ground targets with low level reflectivity are represented by green areas on the display Areas of lower density precipitation or ground targets with modera...

Страница 318: ...M intervals 3 GAIN CONTROL Adjusts radar receiver sensitivity Currently not simulated 4 MODE SELECTOR OFF Turns the radar system off TEST The indicator displays a test pattern consisting of three arcs...

Страница 319: ...ween each range mark 10 ANTENNA TILT READOUT Blue Indicates the antenna tilt angle up or down 11 WEATHER OR GROUND TARGET Areas of light precipitation or ground targets with low level reflectivity are...

Страница 320: ...ng all normal flight conditions and annunciates dangerous flight conditions TEST Momentary Performs a systems integrity test The GPWS BELOW G S and GPWS FAIL lights will come on accompanied by the aur...

Страница 321: ...rrent altitude and the condition should be corrected The mode is independent of aircraft configuration and is active from 2450 feet to 50 feet AGL This mode indicates that terrain closure rate is too...

Страница 322: ...GPWS will continue to compare the current aircraft altitude to the initial altitude of descent Should the aircraft descend again before reaching the initial altitude another warning will be generated...

Страница 323: ...ach 0 29 and 200 feet AGL with the flaps not extended too low flaps is announced Above Mach 0 29 and below 1000 feet AGL to low terrain is announced The mode is inhibited below 50 feet AGL This mode w...

Страница 324: ...Page 9 Super 80 Professional Aircraft Operating Manual Coolsky 2018 WARNING AND CAUTION INDICATORS GPWS FAIL Digital display Comes on to indicate that the Ground Proximity Warning System is inoperati...

Страница 325: ...A identifies traffic which is projected to pass at less than IFR separation standards and present a potential conflict An aural alert TRAFFI TRAFFIC calls the attention of the pilot to the TCAS displa...

Страница 326: ...ompromised and the time of the closure is less than 45 seconds An RA is issued when the conflicting aircraft is less than 35 seconds away and the conflicting traffic is determined to be a threat Perim...

Страница 327: ...RA Climb as directed by TCAS VSI vertical guidance Airplane will climb through the altitude of the traffic DESCEND DESCEND RA Descend as directed by TCAS VSI vertical guidance DESCEND CROSSING DESCEND...

Страница 328: ...utical miles and 1200 feet vertically White solid Other Traffic Any traffic within TCAS range and 2700 feet vertically White hollow DISPLAY THREAT LEVELS AND DATA TAG THREAT LEVEL CAUSE SYMBOL COLOR R...

Страница 329: ...RA mode is selected on the transponder panel TA only mode is enabled automatically All TCAS voice annunciations are inhibited below approximately 500 feet radio altitude All TCAS alerts are inhibited...

Страница 330: ...displayed 2 Maximum range border 3 TCAS Range Indicates displayed TCAS range 4 TA SEL Pushbutton Push to cancel TCAS traffic display 5 TCAS Intruders Threat Intruder Red filled square Traffic advisory...

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