Legendary 727 (For MSFS 2002 ONLY)

Legendary 727

Flight and Training Manual

Part I – SYSTEMS MANUAL

FOR FLIGHT SIMULATION USE ONLY

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Legendary 727 (For MSFS 2002 ONLY)

PILOTS’ MAIN INSTRUMENT PANEL

1. Handle 24. Master comparator warning light 43. MACH indicator *

2. Compass light (amber) 44. Airspeed indicator *
3-6. Landing lights switches * 25. Altitude alert light 45. Attitude director indicator *
7. Taxi light switch 26. Pull up / GPWS test switch (red) * 46. Altimeter-1 *
8-9. Runway turnoff switches * 27. Below GS light (white) * 47. Low range radio altimeter *
10. Engine failure light 28. MDA light (amber) * 48. Clocks *
11. ILS category II sign 29. Approach progress display * 49. Gyrosyn compass system *
12. Autopilot controls and indicators* 30. Pneumatic brake lever 50. Horizontal situation indicator *
13. Wheel well fire warning light (red) * 32. Master test and dim switch 51. Vertical speed indicator *
14-16. Engine fire handle and warning 33. Altitude alert panel * 52. Altimeter-2 *
light (red) * 34. Marker beacon sensitivity switch * 53. Standby artificial horizon *
17-19. Bottle discharged switch * 35. Airways light (clear) * 54. Trimmer indicators *
20. Bottle transfer selector switch * 36. Middle marker light (amber) * 55-57. Reverse operating lights (amber)
21. Freon bottle discharged light 37. Outer marker light (blue) * 58-60. Engine pressure ratio indicators
(amber) * 38. Stabilizer out of trim light (amber) 61-63. N1 tachometers
22. Pilot’s sliding windows operation 39. Elevator low pressure light (red) 64-66. Engine exhaust gas temperature
handle 40. DME indicator* indicators
23. Autopilot disengaged warning 41-42. Windshear ahead lights 67-69. N2 tachometer
light(red) (amber) 70-72. Engine fuel flow indicators

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Legendary 727 (For MSFS 2002 ONLY)

73. Landing gear annunciator panel * 77-78. Leading edge flap lights 82. Speed brake lever *
74. Master warning light (flashing red) * 79-81. Low oil pressure and Oil filter
75-76. Flap position indicators * bypass display caution lights (amber) *

NOTE: * - See detailed description

CONTROLS ASSIGNMENTS OTHER THAN DEFAULT

LIGHTS:
Control cabin lights -- Shift +L
Background lighting -- Ctrl+Shift+L
Cockpit lighting control (day only)-- Shift+F1, Shift+F2, Shift+F3

EXITS:
Pilot’s Sliding Windows -- Shift+E
Passenger Cabin Door (FWD) -- Shift+E+2 or Alt+E
Passenger Cabin Door/Ramp (AFT) -- Wing Fold *
Luggage Door/ Cargo Door -- Tail Hook *

GPWS:
Aural warnings On/Off -- Shift+Q

“CHECK & SET” VOICE CREW PACKAGE:

Activate Next Check List -- Shift+~
Skip To Next Item Active Check List -- Space
Instruments digital readouts – Shift+T

ENGINE:
Engine fire test switch -- Shift+F
Engine fire alarm bell cutout switch -- Shift+B
Fuel Heat -- Shift+H+1, Shift+H+2, Shift+H+3

RADAR:
Weather radar function selector -- Shift+W
Weather radar test pattern -- Ctrl+W

NOTE: * -- must be assigned

PANEL SELECTION ICONS FOR VC ONLY VERSION (Shift+2)

(Shift+1 or Num 8)* Main Panel Æ

(Num 3)* Second Officer Panel Æ Å Overhead Panel (Num 5)*

(Shift+3) Radio Stack Panel Æ Å Checked & Set Control Panel

(Shift+4) Autopilot Panel Æ Å Flaps / Trimmers Panel (Shift+7)

Map View Æ Å Auxiliary Power Unit Panel (Shift+5)

Yoke Æ Å Air Traffic Control ( ` )

Jeppesen Chart on Yoke Æ Å Kneeboard (F10)

Digital Readout Æ Å GPS (Shift+6)

Å Close Panel (Shift+2 To Open)

*NOTE - Num Lock must be ON

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Legendary 727 (For MSFS 2002 ONLY)

PANEL SELECTION ICONS FOR VC+2D VIEWS COCKPIT VERSION (Shift+2)

(Shift+1 or Num 8)* Main Panel Æ

(Num 7)* Forward Left View Æ Å Forward Right View (Num 9)*

(Num 4)* Left View Æ Å Right View (Num 6)*

(Num 1)* Rear Left View Æ Å Second Officer Panel (Num 3)*

(Num 2)* Rear View Æ Å Overhead Panel (Num 5)*

(Shift+3) Radio Stack Panel Æ Å Checked & Set Control Panel

(Shift+4) Autopilot Panel Æ Å Flaps / Trimmers Panel (Shift+7)

Map View Æ Å Auxiliary Power Unit Panel (Shift+5)

Passenger Left View Æ Å Air Traffic Control ( ` )

Yoke Æ Å Passenger Right View

Jeppesen Chart on Yoke Æ Å Kneeboard (F10)

Digital Readout Æ Å GPS (Shift+6)

Å Close Panel (Shift+2 To Open)

*NOTE - Num Lock must be ON

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Legendary 727 (For MSFS 2002 ONLY)

3-6. LANDING LIGHTS SWITCHES

LANDING, INBOARD Left and Right and LANDING, OUTBOARD Left and Right lights provides high intensity lighting for takeoff
and landing.

8-9. RUNWAY TURNOFF Left AND Right SWITCHES

The lights provide ground roll illumination.
Do not illuminate LANDING and RUNWAY TURNOFF lights for more than 5 minutes while stationary on the ground.

12. AUTOPILOT CONTROLS AND INDICATORS

1. PITCH COMMAND CONTROL - Permits manual selection of a pitch-up or pitch-

down command bar display. The control is calibrated in 5-dergee increments from
+15 through –10 degrees. Not effective after glide slope capture
2. AUTOPILOT MODE SELECTOR
3. HDG (HEADING SELECT) – When engaged the autopilot will turn the aircraft to
and hold the heading selected on the captain’s present heading selector. Effective in
MAN and NAV/LOC mode prior to course capture.
4. NAV / LOC – The autopilot will fly the airplane at the existing heading near the
course selected until on the captain’s instruments. Airplane will then turn to and
track the selected course. Automatic crosswind compensation is provided. During
passage over a VOR station the autopilot hold the existing heading.
5. APPR AUTO - The autopilot glide slope mode is armed and will fly the airplane on
the localizer until intercepting the glide slope. The pitch controller controls attitude.
The glide slope mode is now engaged and will pitch the airplane down and fly the
glide slope, while the autopilot the memorizes the rate of descent. After glide slope
engaged, the roll and pitch sensitivities are reduced at 1500’ on the radar altimeter
to compensate for beam convergence. Automatic crosswind compensation is provided. After glide slope engaged, the pitch
controller is ineffective.
6. APPR MAN – Same as APPR AUTO except the airplane will seek and engaged the glide slope from above or below. Pitch
controller is ineffective.
7. ALTITUDE HOLD – Autopilot holds constant airplane altitude if elevator switch engaged. Pitch controller is ineffective. On
APPR AUTO switch trips OFF when glide slope engages.

13. WHEEL WELL FIRE WARNING LIGHT (Red)

Indicates a fire in any wheel well. Fire ALARM bell also sounds.

14-16. ENGINE FIRE HANDLE AND WARNING LIGHT (Red)

Indicates a fire on respective engine or firewall. Fire ALARM bell also sounds.
If pulled the fire handle arms the bottle discharge switch, trips the generator field relay, and overrides closed the following
valves:
- engine fuel shutoff,
- hydraulic fluid shutoff,
- engine bleed air,
- wing anti-ice.
The engine driven hydraulic pump low pressure light is also deactivated.

17-19. BOTTLE DISCHARGED SWITCH

If depressed, will discharge to the respective engine, the bottle selected by the bottle transfer switch.

20. BOTTLE TRANSFER SELECTOR SWITCH

Selects freon bottle to be discharged.

21. FREON BOTTLE DISCHARGED LIGHT (Amber)

ON – when freon bottle discharge.

26. PULL UP / GPWS TEST SWITCH (Red)

Illuminates flashing to provide visual warning for Mode 1,2,3,4.
Press to test aural and visual warnings. System cannot be tested between 50 and 1000 feet.

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Legendary 727 (For MSFS 2002 ONLY)

27. BELOW GS LIGHT (Amber)

Illuminates to provide visual warning to Mode 5. When below 1000 feet, pressing light inhibits or cancels Mode 5, if the
airplane has not penetrated the loud warning area.

28. MDA light (amber) *

The MDA light illuminate when you pass the altitude you have set on the radio alt bug for the MDA (Minimum Descent
Altitude) for the approach.

29. APPROACH PROGRESS DISPLAY

1-2. VOR / LOG ANNUNCIATOR.

AMBER – System armed in NAV LOC or AUTO G/S modes prior to intercept of VOR
radial or localizer beam).
GREEN – Radial or localizer captured.
3-4. GLIDE SLOPE ANNUNCIATOR.
AMBER – System armed in AUTO G/S prior to intercept of glide slope.
GREEN – Glide slope captured. When MAN G/S selected.
5-6. FLARE
7. GO AROUND
8. HDG. Parallels green ENG annunciator of HDG SEL switch on autopilot control
panel.
GREEN – Autopilot heading select is active.
9. ALT HOLD.
AMBER – autopilot altitude select is armed.
GREEN – Autopilot is operating in altitude hold.

30. PNEUMATIC BRAKE LEVER (emergency brake handle)

Clockwise rotation increases braking.

32. MASTER TEST AND DIM SWITCH

1. Master test and dim switch

2. Photoelectric cells (One set with each APD)

33. ALTITUDE ALERT PANEL

1. Altitude set indicator (Indicated selected altitude in 100-foot increments)
2. Altitude set control(Used to set selected altitude in altitude indicator)
An altitude alerting system gives audible and visual indication of approaching an
altitude (acquisition) or departing from an altitude (deviation). In the acquisition
mode an aural signal tone will sound momentarily and the alert lights will come on
when passing through a point approximately 900 feet above or below the selected
altitude. The light will remain on until approximately 300 feet from the selected
altitude. In the deviation mode when departing the selected altitude the aural signal
will sound momentarily and the alert lights will come on when passing through a
point approximately 300 feet above or below the selected altitude. The alert light will
remain on until reset by pressing the alert light.

34. MARKER BEACON SENSITIVITY SWITCH

HIGH position is used at high altitudes. LOW position is used at low altitudes.

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Legendary 727 (For MSFS 2002 ONLY)

35. AIRWAYS LIGHT (Clear)

Illuminates steady when over airways beacon or flashing when over airway fan marker beacon (3000 Hz signal)

36. MIDDLE MARKER LIGHT (Amber)

Illuminates flashing when over ILS middle marker beacon (1300 Hz signal)

37. OUTER MARKER LIGHT (Blue)

Illuminates flashing when over ILS outer marker beacon (400 Hz signal)

40. DISTANCE MEASURING EQUIPMENT

Distance measuring equipment (DME) system provides slant range in nautical miles to station tuned.

43. MACH INDICATOR

1. MACH POINTER (Displays indicated Mach derived from pitot-static pressures)

2. MMO POINTER (Displays maximum operating Mach)

44. AIRSPEED INDICATOR

1. VMO POINTER (Displays maximum operating airspeed)

2. AIRSPEED POINTER (Displays indicated airspeed derived from pitot-static
pressures)
3. MOVABLE EXTERNAL REFERENCE MARKERS
4. VMO MODE SELECTOR (Selects maximum operating airspeed)
5. CURSOR (BUG) (Airspeed cursor indicates reference speed or airspeed for speed
command)
6. CURSOR CONTROL (Position cursor on scale to indicate reference airspeed
selected)

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Legendary 727 (For MSFS 2002 ONLY)

45. ATTITUDE DIRECTOR INDICATOR

1. COMMAND BARS (Airplane is maneuvered to fly the symbolic airplane into the vee
formed by the command bars)
2,3. BANK INDICATOR AND SCALE (Index indicates roll angle against calibrated
scale. Scale has minor markings at 10O, 20O, 45O and major markings at 30Oand 60O
4. HORIZON AND PITCH SCALE TAPE (Scale marks above horizon: 5, 10, 15, 20, 30,
50, 70, 90 degrees. Below: 3, 10, 15, 20, 30, 50, 70, 90 degrees)
5. SIMBOLIC AIRPLANE
6. RUNWAY SIMBOL (Show lateral deviation from localizer beam or VOR radial)
7. COURSE DEVIATION SCALE (Displays expanded center portion of the Course
Deviation Scale on the HIS (50). Out side marks represent one dot displacement
from localizer beam centerline or VOR radial)
8. FLIGHT DIRECTOR MODE SELECTOR (Has four position):
OFF –– HDG (heading select) –– GYRO (NAV/LOC select) –– APPR (Approach)
9. SLIP INDICATOR

10. PITCH COMMAND CONTROL (permits manual selection of a pitch-up or pitch-down)

11. GLIDE SLOPE SCALE (Fixed scale measures airplane displacement above or below glide slope beam)
12. GLIDE SLOPE POINTER (In parallel with pointer on HSI (see 50)

46. ALTIMETER-1

1. DIGITAL DISPLAY (Show altitude in increments of 100 ft)

2. POINTER (Registers 1000 ft for each rotation)
3. ALTIMETER SETTING WINDOWS (Can be set in millibars or inches/Hg)
4. ALTIMETER SETTING CONTROL

47. LOW RANGE RADIO ALTIMETER

1. POINTER (The range of the altimeter is from 0 feet to 2,500 feet)

2. ADJUSTABLE ALTITUDE TRIP CURSOR (A decision height cursor can be moved
about the periphery of the altimeter with the decision height selector, thus selecting
the altitude at which a decision height light will illuminate)
3. ADJUSTABLE ALTITUDE TRIP (A decision height selector)
4. PUSH TO TEST BUTTON (Operating the test switch will cause the altimeter to
indicate 250+ 10 feet and the warning flag to appear)
5. FLAG DISPLAY (When the altimeter is operating properly, the flag is retracted. The
cross-hatched warning flag appear with power loss to the instrument, loss of a return
radio signal and operation above the altitude range of the equipment)

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Legendary 727 (For MSFS 2002 ONLY)

48. CLOCKS

1. ELAPSED TIME HOURS & MINUTES HANDS

2. ELAPSED TIME SWITCH
3. PUSH BUTTON
4. SWEEP SECOND HAND FLAG
5. LOWER MINUTE REGISTER HAND (controlled by push button)
6. WINDING & SETTING CONTROL

49. GYROSYN COMPASS SYSTEM

1. ROTATING COMPASS GARD

2. NO. 1 ADF / VOR POINTER
3. SYNCHRONIZING KNOB
4. NO. 2 ADF / VOR POINTER
5. NO. 2 ADF / VOR SELESTOR KNOB
6. RECIPROCAL HEADING MARKER
7. NO. 1 ADF / VOR SELESTOR KNOB

50. HORIZONTAL SITUATION INDICATOR

1. COURSE COUNTER (digital readout displays course as set by course selector)

2. COURSE CURSOR (indicates course corresponding to digital readout on course
counter)
3. COMPASS GRAD (indicates airplane magnetic heading under lubber line)
4. LUBBER LINE
5. DME INDICATOR (indicates slant range in nautical miles)
6. SYMBOLIC AIRPLANE
7. COURSE DEVIATION SCALE
8. COURSE BAR
9. COURSE SELECTOR
10. HEADING SELECTOR
11. GLIDE SLOPE INDEX
12. GLIDE SLOPE SCALE
13. GLIDE SLOPE POINTER

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Legendary 727 (For MSFS 2002 ONLY)

51. VERTICAL SPEED INDICATOR

1. VERTICAL SPEED POINTER

2. VERTICAL SPEED FLAG
3. RA OFF TCAS FLAG
4. AMBIENT LIGHT SENSOR

52. ALTIMETER-2

1. DIGITAL DISPLAY (show altitude in increments of 100 ft)

2. POINTER (registers 1000 ft for each rotation)
3. ALTIMETER SETTING WINDOWS (display altimeter setting in millibars and inches
of mercury)
4. SELECTOR KNOB,
5. BAROMETRIC SETTING KNOB (set barometric pressure reference in millibars and
inches of mercury)
6. ALTITUDE REFERENCE “BUG”

53. STANDBY ARTIFICIAL HORIZON

1. HORIZON BAR
2. BANK SCALE
3. BANK INDICATOR
4. SYMBOLIC AIRPLANE
5. PITCH TRIM SCALE
6. PITCH TRIM AND GARD CAGING CONTROL
7. HORIZON DRUM

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Legendary 727 (For MSFS 2002 ONLY)

54. CONTROLS / TRIMMER POSITION INDICATORS

1, 3, 4, 6. CONTROLS / TRIMMER POSITION INDICATOR

Show positions of left (6) and right (4) elevators and upper (3) and lower (1)
rudders when airplane power is on the bus or autopilot ground test switch is in the
GRD TEST position when using EXT or APU power.

2, 5. YAW DAMPER WARNING FLAGS.

Flag is in view when respective yaw damper is disengaged

Click on the gauge to switch to trimmer position indicator. Blue flag indicates
trimmer position mode is ON.

73. LANDING GEAR ANNUNCIATOR PANEL

1. LANDING GEAR DOOR WARNING LIGHT (Red).

ON – Any gear door open.
2-4. LANDING GEAR DISAGREEMENT LIGHT (3 Red).
ON – gear not locked in landing gear lever position selected or any thrust lever
retarded with gear up. Also illuminates if landing gear lever moved out of down
detent with aircraft on ground.
5-7. LANDING GEAR DOWN AND LOCKED INDICATOR LIGHT (3 Green).
ON – gear locked down.

74. MASTER WARNING LIGHT (flashing red)

ON – WHEN essential ac bus not energized.
PUSH – extinguishes light on center panel. Will not extinguish power failure warning light on third crewman’s upper panel.

75-78. FLAP POSITION INDICATORS and LEADING EDGE FLAP LIGHTS

Range marks indicate acceptable needle deviation from selected flap position.
Asymmetry protection stops hydraulic drive if needless separate approximately 1 to 3
needle widths.

AMBER ILLUMINATED
- Any leading edge device in transit.
- At flap lever position 2, leading edge device 2, 3, 6 or 7 not extended.
GREEN ILLUMINATED
- At flap lever position 2, stats 2, 3, 6 & 7 fully extended.
- At any other flap lever position, all leading edge flaps and stats fully
extended.
No Light – All leading edge flaps and stats retracted

1. FLAP POSITION INDICATOR

2. FLAP POSITION INDICATOR
3. AMBER ILLUMINATED (any leading edge device in transit, at flap level position 2,
leading edge device 2,3,6 & 7 not extended)
4. GREEN ILLUMINATED (at flap level position, stats 2 & 3, 6 & 7 7 fully extended, At
any other flap level position, all leading edge flaps and stats fully extended)

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Legendary 727 (For MSFS 2002 ONLY)

79-81. LOW OIL PRESSURE and OIL FILTER BYPASS display caution lights (Amber)
Normally the lights should extinguish during engine start.

84. SPEEDBRAKE LEVER

Selects flight spoilers in flight and both flight and ground spoilers on the ground.

RADIO PANEL

1 VHF NAVIGATION AND DME SYSTEMS

1.1 FREQUENCY SELECTOR
1.2 FREQUENCY INDICATOR
1.3 VOLUME CONTROL
2 ATC TRANSPONDER
2.1 FUNCTION SELECTOR
2.2 DISPLAY WINDOW
2.3 TCAS DISPLAY RANGE SELECTOR
2.4 IDENT PUSHBUTTON
2.5 ALTITUDE SOURCE SELECTOR
2.6 CODE SELECTOR KNOBS
3 AUDIO SELECTOR PANELS
3.1 TRANSMITTER SELECTORS
3.2 COMMUNICATIONS RECEIVE SWITCHES
3.3 ADF1 - ADF2 SELECTOR
3.4 R/T - I/C SWITCH (spring-loaded to neutral)
3.5 MASK / BOOM MICROPHONE SWITCH
3.6 FILTER SELECTOR
4 ADF. FORWARD OR AFT ELECTRONIC CONTROL PANEL
4.1 LOOP CONTROL
4.2 BEAT FREQUENCY OSCILLATOR (BFO) SWITCH
4.3 TUNING CONTROL
4.4 VOLUME CONTROL
4.5 FREQUENCY INDICATOR
4.6 TUNING METER
4.7 FUNCTION SELECTOR
4.8 FREQUENCY BAND SELECT

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Legendary 727 (For MSFS 2002 ONLY)

AUTOPILOT CONTROLS PANEL

1. AUTOPILOT MODE SELECTOR

MAN – Autopilot holds a constant airplane heading and
pitch attitude, which can be changed with the turn and
pitch controller. The mode selector will spring load
from any mode to MAN if the turn controller is not
centered.
NAV / LOC – The autopilot will fly the airplane at the
existing heading near the course selected until on the captain’s instruments. Airplane will then turn to and track the selected
course. Automatic crosswind compensation is provided. During passage over a VOR station the autopilot hold the existing
heading.
AUTO G/S - The autopilot glide slope mode is armed and will fly the airplane on the localizer until intercepting the glide slope.
The pitch controller controls attitude. The glide slope mode is now engaged and will pitch the airplane down and fly the glide
slope, while the autopilot the memorizes the rate of descent. After glide slope engaged, the roll and pitch sensitivities are
reduced at 1500’ on the radar altimeter to compensate for beam convergence. Automatic crosswind compensation is
provided. After glide slope engaged, the pitch controller is ineffective.
MAN G/S – Same as AUTO G/S except the airplane will seek and engaged the glide slope from above or below. Pitch controller
is ineffective.
2. AUTOPILOT TURN AND PITCH CONTROLLER – controls the airplane angle of bank and rate of pitch change.
3, 4 AUTOPILOT OF AILERON AND ELEVATOR SWITCHES – Engage autopilot roll pitch axis. Will not engage unless a yaw
damper engaged and interlock circuit satisfied. Elevator switch will not stay engaged unless aileron switch engaged.
5. ALTITUDE HOLD SWITCH
ALT HOLD - Autopilot holds constant airplane altitude if elevator switch engaged. Pitch controller is ineffective. On APPR AUTO
switch trips OFF when glide slope engages.
6. PITCH CHANNEL SELECTOR
A – Selects hydraulic system A to power autopilot command signals to the left elevator (right elevator acts as a slave).
B – Selects hydraulic system B to power autopilot command signals to the right elevator (left elevator acts as a slave).
7. HDG (HEADING SELECT) – When engaged the autopilot will turn the aircraft to and hold the heading selected on the
captain’s present heading selector. Effective in MAN and NAV/LOC mode prior to course capture.

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Legendary 727 (For MSFS 2002 ONLY)

OVERHEAD PANEL

1. Aileron switch (system A) 14,17-20. (Nose, OUTBD & INBD LEFT and Right) Brake
2. Aileron Switch (System B) release indicator *
3. Spoiler switch (system b) * 21. Stall warning off light (amber) *
4. Spoiler switch (system a) * 22. Test indicator *
5. Elevator switch (system a) 23. Stall warning switch *
6. Elevator switch (system B) 24. Flight recorder – off light (Amber)
7-8. Lower rudder switches (standby and system A) * 25. Test light
9. Upper rudder switches (system b) * 26. Altitude warning system
10-11. Yaw damper switches * 27. Altitude warning test switch
12. Flight control warning test switch * 28. The #2 compass system switch
13. Anti-skid test switch * 29. The #1 compass system switch
15. Nose gear brake and anti-skid switch * 30-31. The control stand hooded floodlights
16. Main gear and anti-skid switch * 32-33. Rain repellent switches (left and right) *
34. Windshield wiper switch *

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Legendary 727 (For MSFS 2002 ONLY)

35. Emergency exit lights unarmed (armed) * 77-79. Engine inlet anti-ice valve positions
36. Emergency exit lights switch lights (green) *
37. Cockpit door indication light switch 80-82. Engine inlet anti-ice switches *
38. The ignition system switch 83. Ammeters *
39. Engine access door light * 84. Pitot static heat ammeters selector *
40-42. Engine start switches * 85. Left pitot static heat switch *
43-46. Window heat power on lights (green) * 86. Hearer off light (amber) *
47-50. Window overheat lights (amber) * 87. Right pitot static heat switch *
51-54. Window heat switches * 88. Map light *
55. Window heat test switch * 89. Left fwd & side panel lights *
56. Alternate flaps master switch * 90. Centre fwd panel lights *
57-58. Alternate flaps switches * 91. Fwd panel background lights *
59. Anti-ice duct temperature indicator * 92. Compass light *
60. Anti-ice duct overheat light (amber) * 93. Fwd panel fluor lights *
61. Anti-ice duct temperature selector. 94. Overhead panel lights *
62. Cabin attendant call switch * 95. Control stand red lights *
63. Cabin attendant call light (blue) * 96. Control stand white lights *
64. No smoking switch * 97. Light override switch *
65. Fasten seat belts switch * 98. Right fwd & side panel lights *
66. Ground crew call switch * 99. Map light *
67. Microphone * 100. Dome red *
68. Test jack * 101. Dome white *
69. Test switch * 102-105. Landing lights switches *
70. Monitor * 106. Taxi light switch *
71. Erase switch * 107-108. Runway turnoff left and right switches *
72. Wing anti-ice switch * 109. Navigation lights switches *
73. Temperature symbol * 110. Beacon (anti-collision) light switch *
74. Wing anti-ice valve position light (green) * 111. Wing illumination lights switch *
75. Temperature symbol * 112. Main wheel well lights switch *
76. Anti-ice valve position light selector *

NOTE: * - See detailed description

FLIGHT CONTROL HYDRAULIC SHUTOFF SWITCHES

OFF – Shuts off respective hydraulic system pressure to designated flight controls

3. SPOILER SWITCH (system B)

OFF – Shuts off system B hydraulic pressure to inboard flight spoilers.

4. SPOILER SWITCH (system A)

OFF – Shuts off system A hydraulic pressure to outboard flight spoilers.

7-8. LOWER RUDDER SWITCHES (standby and system A)

Switches and guards ganged together.
GUARDS UP, SWITCHES UP – Shuts off system A hydraulic pressure to lower rudder.
Turn on Standby System Pump.

9. UPPER RUDDER SWITCHES (system B)

OFF – Shuts off system B hydraulic pressure to upper rudder.

10-11. YAW DAMPER SWITCHES

ON- Engages upper and lower yaw damper system.
OFF – Disengages respective yaw damper system.

12. FLIGHT CONTROL WARNING TEST SWITCH

SAFETY RELAY BYPASS.
Air sensor signal bypassed so that the in-flight speed brake flap position warning system (intermittent horn) can be checked
on the ground.

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Legendary 727 (For MSFS 2002 ONLY)

ANTI-SKID SYSTEM

13. ANTI-SKID TEST SWITCH

INBOARD AND NOSE – IND & NOSE indicators BLANK, OUTBD indicator REL
OUTBD AND NOSE – IND & NOSE indicators BLANK, INBOARD indicator REL

15. NOSE GEAR BRAKE AND ANTI-SKID SWITCH

System deactivated.

16. MAIN GEAR AND ANTI-SKID SWITCH

Turns off anti-skid system.
System active only when landing gear lever is down or the nose gear is not locked up and parking brake is off.

14,17-20. (Nose, OUTBD & INBD LEFT and Right) BRAKE RELEASE INDICATOR
IN AIR (GEAR UP) All blank (System deactivated)
IN AIR (GEAR DOWN) All REL
ON GROUND (Above 15 KTS) - blank
ON GROUND (Below 15 KTS) – NOSE – REL, remainder – blank.
PARKING BRAKE ON – All blank (System deactivated)

STALL WARNING SYSTEM

21. STALL WARNING OFF LIGHT (Amber)

EXTINGUISHED – Normal operation
- During test when using APU or external power.

22. TEST INDICATOR

Rotates during test to indicate reliable inputs from stall warning sensor and flap position transmitter.

23. STALL WARNING SWITCH

Spring loaded to the NORMAL position and locked from the HTR OFF position Pulling the switch will bypass the lock.
HTR OFF – Cuts power to the heater for maintenance purposes.
NORMAL – The system including the vane heater is powered when the airplane landing gear safety sensor is in the air
position.
TEST
- with APU or external power.
1. Off light extinguishes.
2. Indicator spins.
3. Control columns shake.
- with airplane power.
1. Off light remains extinguished.
2. Indicator spins.
3. Control columns shake.

32-33. RAIN REPELENT SWITCHES (Left and Right)

Measured amount of repellent sprayed on associated windshield

34. WINDSHIELD WIPER SWITCH

PARK – (Spring loaded to OFF) stows wiper blades.
LOW to HIGH – Controls speed of wipers.

35. EMERGENCY EXIT LIGHTS UNARMED (Armed)

Will be on when emergency exit lights switch is either in the ON or OFF positions, provided the battery switch is on.

STARTING SYSTEM

39. ENGINE ACCESS DOOR LIGHT

The access door for the pneumatic ground service connection.

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Legendary 727 (For MSFS 2002 ONLY)

40-42. ENGINE START SWITCHES

Switches have three positions: GROUND – OFF – FLIGHT. They are spring – load from the GROUND position to the OFF
position, but will remain in FLIGHT, if selected. The FLIGHT position is used for inflight starting.

WINDOW HEAT

43-46. WINDOW HEAT POWER ON LIGHTS (Green)

ILLUMINATED – Power being applied to window.

47-50. WINDOW OVERHEAT LIGHTS (Amber)

ILLUMINATED – Respective window overheated. Power removed.

51-54. WINDOW HEAT SWITCHES

ON: R-1 - Power to windows R-1, R-4, R-5
R-2 - Power to windows R-2, R-4, R-5
L-1 - Power to windows L-1, L-4, L-5
L-2 - Power to windows L-2, L-4, L-5
OFF/RESET:
- Removes power
- Extinguishes overheat

55. WINDOW HEAT TEST SWITCH

Both test positions require window heat switches to be ON.
POWER ON TEST – Verifier power circuit to each window (4 green)
OVERHEAT TEST – Simulates overheat in control unit. Overheat lights illuminate (4 amber).

56. ALTERNATE FLAPS MASTER SWITCH

Operates bypass valve for inboard and outboard trailing edge flaps and slats. Turns on Standby System pump.
Arms alternate flap switches

57-58. ALTERNATE FLAPS SWITCHES

DN (DOWN) – Electrically extends trailing edge flaps. Hydraulically extends leading edge flaps and slaps using Standby
System.
UP – Electrically retracts trailing edge flaps only.

62. CABIN ATTENDANT CALL SWITCH

Momentarily pressed illuminates forward and aft pink master call lights and sounds two-tone (hi-low) chime.

63. CABIN ATTENDANT CALL LIGHT (Blue)

Illuminates and single-tone chime sounds in cockpit while captain call switch is pressed at either attendant’s panel.

64. NO SMOKING SWITCH

ON – Illuminates signs of passenger service units and sounds a single low tone chime over PA system.
Also Illuminates (dim) the emergency exit lights.

65. FASTEN SEAT BELTS SWITCH

ON – Illuminates signs of passenger service units and a RETURN TO SEAT sign in each lavatory. Sounds a single low tone
chime over PA system.

66. GROUND CREW CALL SWITCH

Sounds horn in nose wheel well while switch is pressed.

FLIGHT RECORDER

Maintains a 30-minute record of flight crew communication and cockpit area conversation.

67. MICROPHONE
Pick up all conversation in the cockpit from the time 115V AC is applied to airplane

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Legendary 727 (For MSFS 2002 ONLY)

68. TEST JACK

Plug in headset during test.

69. TEST SWITCH

- Connect headset into monitor jack on panel.
- Press test switch 5 seconds and release.
- Tone will be head and monitor needle will indicate while switch is depressed.

70. MONITOR
- Indicator moves during test.
- Monitors four channels: area microphone, Captain’s, First Officer’s and Third Crewman’s headset circuits.
- Monitors last 30 minutes in audio inputs. Inputs older than 30 minutes are automatically erased.

71. ERASE SWITCH

- Will erase tape if airplane is on the ground and parking brakes set.
- Hold erase switch a minimum of 7 seconds
- Erases all four channels together.

WING & ENGINE ANTI – ICE

59. ANTI-ICE DUCT TEMPERATURE INDICATOR

Temperature indication as determined by duct temperature selector.

60. ANTI-ICE DUCT OVERHEAT LIGHT (Amber)

ILLUMINATED – Excessive temperature if left or right wing anti-ice supply or duck.
- Engine 2 cowl duct.
- Independent of duct temperature selection.

61. ANTI-ICE DUCT TEMPERATURE SELECTOR.

Determines source of temperature displayed by duct temp indicator.
ENG 1 – Wing anti-ice left supply duct temperature.
ENG 2 – Engine 2 cowl duct temperature.
ENG 3 – Wing anti-ice right supply duct temperature.

72. WING ANTI-ICE SWITCH

GRD TEST – Spring loaded to close. Opens wing anti-ice valves on ground for test
OPEN – Opens wings anti-ice valves in flight.

73. TEMPERATURE SYMBOL

Location of Eng 1 and Eng 3 anti-ice supply duct temperature sensors.

74. WING ANTI-ICE VALVE POSITION LIGHT (Green)

ILLUMINATED – Both wings anti-ice valves in the Engine 1 supply duct agree with the Eng 1 wing anti-ice switch position.

75. TEMPERATURE SYMBOL

Location of Eng 2 cowl anti-ice duct temperature and overheat sensors.

76. ANTI-ICE VALVE POSITION LIGHT SELECTOR

Select valves to be checked y the valve position lights.
L – Left inlet valve; Engine 1,2 and 3.
COWL – Cowl valve; Engines 1and 3 – cowl shutoff valve and high pressure valve; Engine 2.
R - Right inlet valve; Engine 1,2 and 3.
WING – Both wing shutoff valves and both wing high stage valves.

77-79. ENGINE INLET ANTI-ICE VALVE POSITIONS LIGHTS (Green)

ILLUMINATED – Valve position agrees with switch position.

80-82. ENGINE INLET ANTI-ICE SWITCHES

OPEN – Opens all engine anti-ice valves for respective engine.

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Legendary 727 (For MSFS 2002 ONLY)

PITOT STATIC HEAT

83. AMMETERS
Current for selected units.

84. PITOT STATIC HEAT AMMETERS SELECTOR

Select input in ammeters:
AUX P – Auxiliary pitot.
STATIC – Static ports
P – pitots
T PROBE – Total air temperature probes
ELEV P – Elevator feel system pitots

85. LEFT PITOT STATIC HEAT SWITCH

ON – Applies heat to:
Left pitot
Left static ports
Left temperature probe
Left elevator feel system pitot.

86. HEARER OFF LIGHT (Amber)

ILLUMINATED
- Pitot static heat switch OFF.
- Pitot static heat switch ON and left or right pitot probe heater inoperative.

87. RIGHT PITOT STATIC HEAT SWITCH

ON – Applies heat to:
Right pitot
Right static ports
Right temperature probe
Right elevator feels system pitot.
Auxiliary pitot

LIGHTING SYSTEM. COCKPIT LIGHTS CONTROLS

88. MAP LIGHT

Located in the Captain’s NO. 4 window.

89. LEFT FWD & SIDE PANEL LIGHTS

Controls integral Instrument illumination on left forward and side panels.
Also controls panel light for first and second observes.

90. CENTRE FWD PANEL LIGHTS

Controls integral Instrument illumination on centre panel.

91. FWD PANEL BACKGROUND LIGHTS

Controls lights located under light shield.

92. COMPASS LIGHT

Controls lights in standby compass

93. FWD PANEL FLUOR LIGHTS

Controls white fluorescent lights under light shield.

94. OVERHEAD PANEL LIGHTS

Controls integral Instrument illumination on overhead panel.

95. CONTROL STAND RED LIGHTS

Controls red floodlights located in overhead panel for illuminating the control stand.

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Legendary 727 (For MSFS 2002 ONLY)

96. CONTROL STAND WHITE LIGHTS

Controls white floodlights located in overhead panel for illuminating the control stand.

97. LIGHT OVERRIDE SWITCH

FLIGHT ONLY position – Turn off or prevents turning on the cockpit fluorescent panel lights, white control stand, and white
dome lights.
NORMAL position – Allows all white lights to be controlled by there respective light switches.
All WHITE position - turn on the cockpit fluorescent panel lights, white control stand lights to full intensity and allows selection
of the dome lights by their switches.
The background lights in the pilots and Second Officer’s light shields and the cockpit red lights are not affected by the
override switch.

98. RIGHT FWD & SIDE PANEL LIGHTS

Controls integral Instrument illumination on right forward and side panels.

99. MAP LIGHT

Located in the First Officer’s NO. 4 window.

100. DOME RED

Controls three red dome lights.

101. DOME WHITE

Controls three white dome lights.

THE LOWER EDGE OF THE LIGHTING SYSTEM

102-105. LANDING LIGHTS SWITCHES

LANDING, INBOARD Left and Right and LANDING, OUTBOARD Left and Right lights provides high intensity lighting for takeoff
and landing.

106. TAXI LIGHT SWITCH

107-108. RUNWAY TURNOFF Left AND Right SWITCHES

The lights provide ground roll illumination.
Do not illuminate LANDING and RUNWAY TURNOOF lights for more than 5 minutes while stationary on the ground.

109. NAVIGATION LIGHTS SWITCHES

Navigation lights, red Left and green Right, are provided in the outboard edge of each wing.
ON – lights are powered by 28 V AC. (The ON position will be used for all flight operations)
ON BAT - lights are powered by 28 V DC.

110. BEACON (Anti-Collision) LIGHT SWITCH

The beacon lights on the top and button of fuselage, provide high intensity red flashes, as a proximity warning of the aircraft.

111. WING ILLUMINATION IIGHTS SWITCH

Two wing illumination lights are mounted flush with the fuselage and forward of the wing leading edge.

112. MAIN WHEEL WELL LIGHTS SWITCH

NORMAL – The wheel well lights are controlled by the switch in each respective wheel well.
ON - The wheel well lights will be on regardless of the switch position in the wheel well.

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Legendary 727 (For MSFS 2002 ONLY)

SECOND OFFICER PANEL

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Legendary 727 (For MSFS 2002 ONLY)

AIR CONDITIONING & PRESSURIZATION PANEL 105-106. Cooling doors position indicator *
107. Pack temperature indicator *
ELECTRICAL POWER PANEL 108. Pack temperature indicators *
109. Pneumatic duct pressure indicator *
HYDRAULIC SYSTEMS PANEL 110. Auto pack trip armed light (green) *
111-112. Air conditioning pack switch *
FUEL SYSTEM PANEL 113-114. Pack trip off light (amber) *
115-116. Engines no. 1 /no. 3 bleed air switch *
1. Dc voltmeter * 117-118. Engines no. 1/ no. 3 trip off light (amber) *
2. Dc ammeter * 119-120. Engine no. 2 bleed air switch (2) *
3. Dc meters selector * 121. Engine no. 2 overheat light (amber) *
4. Battery switch *
122. Duct overheat reset switch *
5-7. Generator drive disconnect switch *
123-124. Duct overheat light (amber) *
8-10. Generator drive low pressure light (amber)
125-126. Air mix valves indicator *
11-13. Generator drive temperature switch*
127-128. Temperature selector *
14-15. Galley power switches * 129. Air temperature indicator *
16. External power switch * 130. Air temperature selector switch *
17. External power connected light (clear) * 131. Cabin altimeter and differential pressure gage *
18-20. Generator drive oil temperature indicator 132. Cabin rate of climb indicator *
21. Essential power selector * 133. Cargo door light (amber) *
22-24. Bus the breaker light (amber) *
134. Cabin pressure control indicator *
25-27. Bus tie breaker switch *
28-30. Generator breaker light (amber) * 135. Manual cabin pressure control indicator *
31-33. Generator breaker switch * 136. Altitude horn cutout switch *
34-36. Generator field light (amber) * 137-139. Start valve open of engines 1,2,3 lights (amber)
37-39. Generator field switch * 140. Smoke detection system
40. Essential power failure warning light (red) * 141. Secondary main landing gear position indicate lights
41. Residual volts switch * (green) *
142. Wing anti-ice auto trip off switch *
42. Ac voltmeter *
143. Wing anti-ice auto trip off light (amber) *
43. Frequency indicator * 144-146. Overheat lights (amber) *
44. KVAR switch * 147. Test switch *
45-47. Power meter * 148. Clock
48-50. Frequency control knob * 149-151. The oil quantity instruments *
51-52. Synchronizing light (clear) * 152-154. Oil temperature indicators *
53. Ac meters selector * 155-157. Oil pressure indicators *
158. Oil quantity test
54-57. Fuel aft boost pump switch *
159. Engine vibration indicator.
58-61. Fuel fwd boost pump switch * 160. Panel flour switch
62-69. Fuel boost pump low pressure light (amber) * 161. Control circuit breaker lights
70-72. Fuel quantity indicator test switch * 162. Control panel background lights
73-75. Fuel tank quantity indicator * 163. Control panel lights
76-78. Fuel crossfeed manifold valve in transit light (blue) * 164. Control table lights
79-81. Engine fuel shutoff valve in transit light (blue) * 165. Service interphone switch.
82-84. Fuel crossfeed manifold valve switch * 166. Second officer’s lower instrument panel *
85-86. Engine fuel shutoff valve switch * 167. Lights test switch
168-169. System a hydraulic fluid shutoff switch *
87-89. Fuel heat. Icing eng. 1,2,3 lights (amber)
170-173. Systems A,B pump low pressure light – (amber) *
90-91. Fuel heat. Valve in transit eng. 2,3 lights (green)
174-175. System A hydraulic pump switch *
92. Flight crew oxygen pressure indicator
176-177. System B hydraulic pump switch *
93. Passenger oxygen pressure indicator
178. System A hydraulic overheat light – (amber) *
94. Passenger oxygen switch *
179. System B hydraulic overheat light – (amber) *
95. Oxygen pressure indicating light (amber) *
180. Ground interconnect switch *
96. Auto pack trip cutout switch *
181. Standby hydraulic system quantity indicator *
97. Valve position indicator *
182. Standby hydraulic system light – (green) *
98. Zone control switch * 183. Standby hydraulic system overheat light –(amber) *
99. Zone temperature overheat light (amber) * 184. System A hydraulic pressure indicator *
100. Cargo heat outflow switch * 185. System B hydraulic pressure indicator *
101. Gasper fan switch * 186. System A hydraulic quantity indicator *
102. Air conditioning pack reset switch * 187. System B hydraulic quantity indicator *
103-104. Cooling doors switch

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188. Hud. Brake interconnect light (green) 194. Oxygen mask microphone switch
189. Hud. Brake interconnect switch 195. Mic – hand – boom switch
190. Oxygen emergency lever 196. Oil cooler selector switch (csd) *
191. Oxygen diluter lever 197. No equipment cooling light (amber) *
192. Flow indicator 198. Elevator feel differential pressure light (amber) *
193. Oxygen supply lever 199. Rudder load limiter light *

NOTE: * - See detailed description

ELECTRICAL POWER PANEL

1. DC VOLTMETER
Indicates voltage of selected source.

2. DC AMMETER
Indicates DC current of selected source.

3. DC METERES SELECTOR

BAT - indicate battery current and

voltage when no AC power on airplane.
Battery charging shows positive voltage.

ESS TR / TR1 / TR2 - indicate

transformer-rectifier current and TR bus
voltage.

4. BATTERY SWITCH
ON -- battery serves as a buck-up for battery busses.
OFF -- battery isolated from loads except those on hot battery busses, but continues to charge. Trips the APU (if
running).

5-7. GENERATOR DRIVE DISCONNECT SWITCH

Disconnect drive from engine and trips generator breaker.

11-13. GENERATOR DRIVE TEMPERATURE SWITCH

RISE – indicates oil temperature increase through generator drive
IN - indicates temperature of oil at in-put.

14-15. GALLEY POWER SWITCHES

ON - galley power available to galleys as selected.

16. EXTERNAL POWER SWITCH

ON - external power on the bus tie. When external power is connected, the generator breakers and APU generator
breaker automatically trips for over voltage or phase unbalance faults.
OFF – if external power connected, external power DC bus, battery transfer bus, and external power 115V AC bus
powered.
GRD SERVICE - 115V AC transfer bus also powered.

17. EXTERNAL POWER CONNECTED LIGHT (Clear)

ON – ground power available at external power connection.

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21. ESSENTIAL POWER SELECTOR

ESSENTIAL POWER SELECTOR is a rotary switch

with STANDBY -- APU -- GEN1 -- GEN2 -- GEN3
– EXT PWR position. Any of these source, except
STANDBY, can be selected to supply the essential
AC bus by manual position of the switch.

Selects power source for essential AC bus. If no

fault exists, a generator can supply essential
power with the generator breaker tripped.
Neither external power nor the APU can supply
essential power unless it is on the sync bus and
the bus the breaker is closed. In standby
position, required flight instruments and radios
are powered from battery bus and static inverter.

22-24. BUS THE BREAKER LIGHT (Amber)

ON – bus the breaker open and generator operating isolated.

25-27. BUS TIE BREAKER SWITCH

Opens circuit between respective A.C. bus and bus TIE. Automatically trips due to excitation faults or overload if
perspective generator breaker is closed. A phase unbalance on the bus tie will trip all bus tie breakers.

28-30. GENERATOR BREAKER LIGHT (Amber)

ON – generator breaker open and generator disconnected from load bus.

31-33. GENERATOR BREAKER SWITCH

Opens circuit between respective generator and A.C. bus automatically trips due to generator drive speed faults, if the
drive is disconnected, or if the generator field is off. Trips on engine shutdown. Closing a generator breaker trips the
external power contactor or the APU generator breaker.

34-36. GENERATOR FIELD LIGHT (Amber)

ON – generator field relay open, and generator field deenergized.
Generator electrically inoperative and essential power not available from this source.

37-39. GENERATOR FIELD SWITCH

Turns off generator field. Automatically trips due to
generator voltage faults, differential faults, generator overload, or if engine fire switch pulled.

40. ESSENTIAL POWER FAILURE WARNING LIGHT (Red)

ON – loss of essential power. Master warning light also illuminates.

41. RESIDUAL VOLTS SWITCH

Changes voltmeter scale from 150 to 30 volts. Indicates residual generator voltage to check rotation and proper
functioning.

42. AC VOLTMETER
Indicate voltage as selected

43. FREQUENCY INDICATOR

Indicate frequency as selected

44. KVAR SWITCH

Push switch for KVAR.

45-47. POWER METER

Indicates generator real (KW) or reactive (KWAR) load.

48-50. FREQUENCY CONTROL KNOB

Remits frequency adjustment isolated generator.

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Legendary 727 (For MSFS 2002 ONLY)

51-52. SYNCHRONIZING LIGHT (Clear)

Connected between the bus tie and the position of the AC meters selector. Blink rate is proportional to frequency
differences.

53. AC METERS SELECTOR

AC selector is a rotary switch with APU -- BUS

TIE -- GEN1 -- GEN2 -- GEN3 – EXT PWR position.
With the switch in any position, the synchronizing
lights are connected between that power source
the synchronizing bus.

The AC voltmeter and frequency indicator display

the voltage and frequency of source selected by
the AC meter selector.

FUEL SYSTEM PANEL

54-57. FUEL AFT BOOST PUMP SWITCH

ON – for fuel boost pump operation

58-61. FUEL FWD BOOST PUMP SWITCH

ON – for fuel boost pump operation

62-69. FUEL BOOST PUMP LOW PRESSURE LIGHT (Amber)

Indicates low boost pump discharge pressure from respective pump.

70-72. FUEL QUANTITY INDICATOR TEST SWITCH

Respective quantity indicator display will change to 0 quantity and indicate ERR after to 10 seconds. Upon release
system will self test and return to normal fuel quantity reading.

73-75. FUEL TANK QUANTITY INDICATOR

Indicates usable fuel in respective tank.

76-78. FUEL CROSSFEED MANIFOLD VALVE IN TRANSIT LIGHT (Blue)

ON – during respective valve transit
OUT – after valve attains new position.

79-81. ENGINE FUEL SHUTOFF VALVE IN TRANSIT LIGHT (Blue)

ON – during respective valve transit.
OUT – after valve attains new position.

82-84. FUEL CROSSFEED MANIFOLD VALVE SWITCH

Switch shown closed. Bar align with fuel flow line when open.
OPEN – opens valve to crossfeed manifold to supply fuel to other engines from respective tank.

85-86. ENGINE FUEL SHUTOFF VALVE SWITCH

Operates respective engine fuel shutoff valve. Must be open for engine operation valve overrides closed when
respective engine fire switch pulled, or engine start lever in cutoff.

OXYGEN SYSTEM

94. PASSENGER OXYGEN SWITCH

NORMAL – System is armed for automatic activation at 14,000 feet cabin altitude, if properly reset.
ON – Pressurizes passenger oxygen system. Passenger oxygen light illuminates and masks deploy.

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Legendary 727 (For MSFS 2002 ONLY)

95. OXYGEN PRESSURE INDICATING LIGHT (Amber)

ILLUMINATED – Passenger oxygen system is pressurized.
AIR CONDITIONING AND PRESSURIZATION PANEL

96. AUTO PACK TRIP CUTOUT SWITCH

NORMAL – Auto pack trip system will arm for takeoff.
CUTOUT - Auto pack trip system deactivated.

97. VALVE POSITION INDICATOR

Shows position of forward and AFT zone control valves with regard to the relative temperature selected.

98. ZONE CONTROL SWITCH

Controls position of the forward and AFT zone control valves in selecting temperature of AFT zone.

99. ZONE TEMPERATURE OVERHEAT LIGHT (Amber)

ON – indicates forward or AFT zone control supply air temperature is excessive. The respective zone control valve that
was open is automatically driven closed. The light wills extinguish and the system will reset when the overheat
condition no longer exists.

100. CARGO HEAT OUTFLOW SWITCH

NORMAL – opens cargo outflow valve causing passenger air to flow along the sides of the EFD. Cargo compt. for
warming. Automatically close & opens cargo heat outflow valve when pressure outflow valve is 1/2 a degree from
closed & 3 – ½ degrees back from closed, respectively.
OFF – valve is closed and no warming air is provided.
NOTE: must be closed to maintain a large cabin differential during single pack operation.

101. GASPER FAN SWITCH

Increases individual air outlet airflow.

102. AIR CONDITIONING PACK RESET SWITCH

Restore normal circuit control of the respective valves following automatic pack or engine bleed air trips. The
respective light will extinguish if the over temperature condition no longer exists.

105-106. COOLING DOORS POSITION INDICATOR

Modulates the ram air inlet cooling doors and heat exchanger exhaust doors to control the airflow through the heat
exchangers.

107. PACK TEMPERATURE INDICATOR

Indicates air temperature at air cycle machine compressor discharge. Serve as a reference for pack cooling door
operation. OPT INFLT temp. 30O – 40O C.

108. PACK TEMPERATURE INDICATORS

Indicates the temperature of the air entering the secondary heat exchanger.

109. PNEUMATIC DUCT PRESSURE INDICATOR

Indicates pneumatic duct pressure sensed at points indicated by dotted lines on panel. Pressure monitored to indicate
proper operation of bleed air system, APU, or external air sourc4e for engine starting and air conditioning.

110. AUTO PACK TRIP ARMED LIGHT (Green)

ON – indicates automatic pack shot-down is armed. Light normally on when engine thrust exceeds 1.5 ERD and the
flaps are NOT UP. Will not arm in the air.

111-112. AIR CONDITIONING PACK SWITCH

Controls LH/RH pack valves. With the air conditioning pack switch ON, the pack cooling fan will run if the flaps are
extended or the airplane is on the ground. If a pack trip has occurred on the ground, the fan will continue to run until
trip is reset. Pack switches must be off for engine start.

113-114. PACK TRIP OFF LIGHT (Amber)

ON – indicates pack has tripped off and air temperature is excessive at (1) the compressor discharge, (2) the turbine
inlet, or (3) the supply duct.
The pack valve overrides close and then the air mix valve goes to full cold position. Loss of thrust on any engine
during takeoff will cause both packs to trip off (if auto pack trip system is armed).

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115-116. ENGINES NO. 1 /NO. 3 BLEED AIR SWITCH

Controls bleed air valve. Must be open to start engine. Valve overrides close if the engine fire switch pulled.

117-118. ENGINES NO. 1/ NO. 3 TRIP OFF LIGHT (Amber)

ON – bleed air overheat. Bleed air valve overrides close. Light extinguished by reset button.

119-120. ENGINE NO. 2 BLEED AIR SWITCH (2)

Each switch controls the NO. 2 engine bleed air valve and one crossfeed valve to allow air conditioning operation from
engine 2. The NO. 2 engine bleed valve overrides closed if engine fire selector switch is pulled.

121. ENGINE NO. 2 OVERHEAT LIGHT (Amber)

ON – indicates engine NO 2 bleed air overheat.

122. DUCT OVERHEAT RESET SWITCH

Extinguishes duct overheat lights and restores normal control of air mix valves.

123-124. (Control and passenger cabins) DUCT OVERHEAT LIGHT (Amber)

ON – indicates excessive supply duct temperature, air mix valves override full cold.

125-126. (Control and passenger cabins) AIR MIX VALVES INDICATOR

Show relative position of cabin air mix valves.

127-128. (Control and passenger cabins) TEMPERATURE SELECTOR

AUTO – automatic temperature regulator controls temperature of the cabin as selected.
MANUAL – air mix valves controlled manually and automatic temperature regulator bypassed.

129. AIR TEMPERATURE INDICATOR

Indicator shows passengers cabin, supply duct, or pack temperature downstream of water separator as selected.

131. CABIN ALTIMETER AND DIFFERENTIAL PRESSURE GAUGE

Indicates cabin altitude (inside dial) and differential pressure (outside dial)

132. CABIN RATE OF CLIMB INDICATOR

Shows rate of cabin pressure (altitude) changes.

136. ALTITUDE HORN CUTOUT SWITCH

Silences intermittent horn, which sounds if cabin altitude exceeds 10.000 feet.

141. SECONDARY MAIN LANDING GEAR POSITION INDICATE LIGHTS (Green)

Left and Right main landing gear down and locked.

ICE AND RAIN PROTECTION SYSTEMS

142. WING ANTI-ICE AUTO TRIP OFF SWITCH

GROUND TEST – Simulates trip condition.
NORMAL – System armed.
GROUND RESET – Resets trip light and wing anti-ice valves after trip or test. Reset can only be accomplished on the
ground.

143. WING ANTI-ICE AUTO TRIP OFF LIGHT (Amber)

ILLUMINATED – Wing anti-ice duct rupture. All wing anti-ice valves close.

ENGINE OIL SYSTEM

149-151. THE OIL QUANTITY INSTRUMENTS

Measured in gallons. Indicate usable quantity of oil remaining.

152-154. OIL TEMPERATURE INDICATORS

Maximum oil temperature for all operating conditions is 120o C

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Legendary 727 (For MSFS 2002 ONLY)

155-157. OIL PRESSURE INDICATORS

The normal operating oil pressure are 45 to 55 PSI

PANEL LIGHTS CONTROLS

166. SECOND OFFICER’S LOWER INSTRUMENT PANEL

1. FWD ENTRY 9. AFT AIRSTAIR

2. L GEAR DOOR 10. TAIL SLID
3. AFT AIRSTAIR 11. GALLEY
4. CARGO V CLOSED 12. FWD CARGO
5. L SERVICE DOOR 13. R GEAR DOOR
6. NOSE GEAR DOOR 14. APU
7. EQUIP ACCESS 15. AFT CARGO
8. AFT ENTRY 16. R SERVICE DOOR

HYDRAULIC SYSTEMS

168-169. SYSTEM A HYDRAULIC FLUID SHUTOFF SWITCH

Except when A malfunction dictates the shutoff switches should not be closed.
Should the pumps be operated under the above condition, the operating time must be logged as maintenance is
required.
Overrides closed if engine fire switch is pulled.

170-173. SYSTEMS A,B HYDRAULIC PUMP LOW PRESSURE LIGHT – (Amber)

1. Goes out as pressure increases at 950 – 1450 PSI.
2. Comes on as pressure decreases at 1350 700 PSI
3. Deactivated by engine fire switch.

174-175. SYSTEM A HYDRAULIC PUMP SWITCH

Used to depressurize engine driven pumps.

176-177. SYSTEM B HYDRAULIC PUMP SWITCH

Operate electric motor driven pumps.

178. SYSTEM A HYDRAULIC OYERHEAT LIGHT – (Amber)

Indicates overheat in hydraulic pump return line.

179. SYSTEM B HYDRAULIC OYERHEAT LIGHT – (Amber)

ON – B pump overheating.
OFF – when overheating pump is switched off.

180. GROUND INTERCONNECT SWITCH

1. Allows system A operation from system B pumps, for ground check-out.
2. Requires external AC power plugged in or APU on bus to open; otherwise will automatically close.

181. STANDBY HYDRAULIC SYSTEM QUANTITY INDICATOR

1. .52 US GAL full *
2. .28 US GAL minimum dispatch quantity.

182. STANDBY HYDRAULIC SYSTEM LIGHT – (Green)

Comes on when standby system is pressurized.
Goes out when standby pressure bleeds off.

183. STANDBY HYDRAULIC SYSTEM OVERHEAT LIGHT –(Amber)

Indicates standby hydraulic fluid overheat.

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Legendary 727 (For MSFS 2002 ONLY)

184. SYSTEM A HYDRAULIC PRESSURE INDICATOR

1. 3000 PSI normal operating.
2. 2000 PSI normal operating.
3. 0, if precharge is lost.

185. SYSTEM B HYDRAULIC PRESSURE INDICATOR

1. 3000 PSI normal operating.
2. 2000 PSI normal operating.
3. 0, if precharge is lost.

186. SYSTEM A HYDRAULIC QUANTITY INDICATOR

1. 4.4 US GAL full (gear down).
2. 3.6 US GAL full (gear up).
3. 3.9 US GAL full (gear, flaps up).
4. 3.9 US GAL minimum dispatch quantity

187. SYSTEM B HYDRAULIC QUANTITY INDICATOR

Normally full, if system A quantity over 2.5 US GAL.

196. OIL COOLER SELECTOR SWITCH (CSD)

FLIGHT ON – Turns on cooler ejector in-flight for additional CSD oil cooling.
NORMAL – Cooler off in flight. ON on ground. On causes ejector to pull cooling air across heat exchanger.
GROUND
OFF - Ejector off, automatically resets to normal on takeoff.

197. NO EQUIPMENT COOLING LIGHT (Amber)

ON – indicates no airflow in equipment cooling duct.

198. ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT (Amber)

Illuminated when the pressure differential between the two hydraulic outputs from the elevator feel computer to the
elevator feel control unit is excessive.

199. RUDDER LOAD LIMITER LIGHT

Illuminated when the lower rudder is in the high pressure configuration with flaps up, or in the low pressure
configuration

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Legendary 727 (For MSFS 2002 ONLY)

PANELS

1. FUEL DUMP SYSTEM PANEL

The Fuel Dump lights indicate the selected dump valve is open and are blue.
The fuel dump system uses the fuel pump switches on the S/O fuel panel.
When operating with all fuel pumps on, the system will dump the fuel to a
level of aprox. 3,500 lbs in each tank at a rate of 2,300 lbs per minute.

1.1 FUEL DUMP VALVE IN TRANSIT LIGHT (Blue)

1.2 FUEL DUMP SWITCH
1.3 FUEL DUMP NOZZLE VALVE SWITCH
1.4 FUEL DUMP NOZZLE VALVE IN TRANSIT LIGHT (Blue)

2. E.L.T. (EMERGENCY LOCATOR TRANSMITTER) CONTROL SWITCH.

The red LED will illuminate if the switch is turned to on or if the E.L.T. is
triggered from an impact.

3. APU PANEL
3.1 APU MASTER SWITCH
ON – Opens the Fuel Shutoff valve and arms the automatic Start circuit.
START – Energizes the starter motor, activates the automatic start circuit.
OFF – Shuts down the APU.
NOTE: Battery switch is ON, APU Fire Switches closed, Remote APU stop
switch is in the NORMAL position; APU Fire Warning Test-Reset switch has
been reset.

3.2. GENERATOR BREAKER LIGHT (Amber)

ILLUMINATED – Generator disconnected from synchronous bus.

3.3 GENERATOR BREAKER SWITCH

CLOSE – Connects APU generator to airplane synchronous bus. Closing the
APU generator switch will automatically trip the airplane generator breakers
or external power contactor.
TRIP – disconnects circuit between APU generator and synchronous bus.

3.4 FIRE SWITCH

When pulled, will arm the respective APU bottle discharge switch, trip the
APU generator field relay and close the APU fuel shutoff and bleed air valves.

3.5 FIRE WARNING LIGHT (Red)

ILLUMINATED – indicates tire in APU shroud. Fire alarm bell (in cockpit) and
intermittent APU fire warning horn (in nose wheel well) also sound. Master
Fire Warning Lights also illuminate.

3.6 GENERATOR FIELD LIGHT (Amber)

ILLUMINATED – Generator field relay open, generator field de-energized.

3.7 GENERATOR FIELD SWITCH

CLOSE – Closes generator field relay and energizes field.
TRIP - De-energizes APU generator field. Automatically trips doe to voltage
or differential faults or if APU fire shutdown system is activated. Automatically trips APU generator breaker.

3.8 BOTTLE DISCHARGE SWITCH

Armed only if APU fire switch pulled.

3.9 AUTO FIRE SHUTDOWN ARMING SWITCH

ARMED – A fire warning or test will automatically shutdown APU.
OFF - Automatic shutdown deactivated.
NOTE: If shutdown is initiated by either fire switch or the automatic fire shutdown relay, the fuel shutoff valve will
close immediately accompanied by other normal shutdown actions.

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Legendary 727 (For MSFS 2002 ONLY)

3.10 FIRE WARNING TEST-RESET SWITCH

TEST – Heats fire detector to trigger fire warning system.
CAUTION: Limit test time to 60 seconds.
RESET – Will silence fire warning bell and horn and extinguish Master Fire Warning Lights. When APU Fire Warning
Light is extinguished, resets automatic fire shutdown to allow starting the APU.

3.11 APU AMMETER

Indicates APU or external power current flow.

3.12 EGT INDICATOR

Green band indicates normal operating range, yellow band indicates caution range. Red line indicates maximum
temperature.

4. LEADING EDGE DEVICER ANNUNCIATOR PANEL

4.1 – TEST SWITCH
LIGHT TEST – Illuminates all lights
POSITION TEST –
Amber – Flap or slat in transit.
Green - Flap or slat extended.
No light - Flap or slat retracted.
4.2 - LEADING EDGE FLAP AND SLAT LIGHTS

© 2002 Captain Sim www.captainsim.com 31