Aeronautical Engineers, Inc. AFM Supplement to · SECTION 0 – SYSTEM DESCRIPTION This aircraft...

Aeronautical Engineers, Inc. AFM Supplement to 7765 N.W. 54th Street Boeing 737-300/-400 Miami, FL 33166 Airplane Flight Manual Aeronautical Engineers Inc. Report R-777 STC ST01827LA

of 25

LOG OF PAGES

REV. PAGES DESCRIPTION FAA APPROVAL

Orig.

All

Complete Supplement

__Patrick Power_ Manager Flight Test Branch, ANM-160L FAA, Los Angeles Aircraft Certification Office Transport Airplane Directorate Date __9/13/2005___

A

All

Added sections 1.6, 1.7

__Patrick Power_ Manager Flight Test Branch, ANM-160L FAA, Los Angeles Aircraft Certification Office Transport Airplane Directorate Date ___3/16/2006___

B

All

Added sections 1.8 and 3.4

__Patrick Power_ Manager Flight Test Branch, ANM-160L FAA, Los Angeles Aircraft Certification Office Transport Airplane Directorate Date ____6/2/2006___

C

All

Revised section 3.1

__Hank H. Tong_ Manager Flight Test Branch, ANM-160L FAA, Los Angeles Aircraft Certification Office Transport Airplane Directorate Date __5/22/2007___

D

1 to 19

Added B737-400 data

__Joe Hashemi_ Manager Flight Test Branch, ANM-160L FAA, Los Angeles Aircraft Certification Office Transport Airplane Directorate Date __8/9/2007___


FAA APPROVED Oct 3, 2008 of 25

TABLE OF CONTENTS LOG OF PAGES.......................................................................................................................................2 LOG OF PAGES.......................................................................................................................................3 TABLE OF CONTENTS..........................................................................................................................4 SECTION 0 – SYSTEM DESCRIPTION................................................................................................5

0.1 MAIN DECK CARGO DOOR .......................................................................................................5 0.2 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM ..............................5 0.3 MAIN CARGO COMPARTMENT AIR SUPPLY SHUTOFF SYSTEM.....................................7 0.4 SECONDARY MAIN LANDING GEAR POSITION INDICATING SYSTEM..........................8

SECTION 1-CERTIFICATE LIMITATIONS .........................................................................................8 1.1 MAIN DECK CARGO DOOR .......................................................................................................8 1.2 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM ..............................8 1.3 AIR CONDITIONING PACKS ......................................................................................................8 1.4 SECONDARY MAIN LANDING GEAR POSITION INDICATING SYSTEM..........................9 1.5 CENTER OF GRAVITY ENVELOPE - B737-300 ONLY............................................................9 1.6 CENTER OF GRAVITY ENVELOPE – B737-400 ONLY.........................................................15 1.7 MINIMUM OPERATING WEIGHT............................................................................................16 1.8 WEIGHT & BALANCE CONTROL AND LOADING LIMITATIONS ....................................16 1.9 MAIN CARGO COMPARTMENT AIR SUPPLY SHUTOFF ..................................................16

SECTION 2 - NON-NORMAL PROCEDURES ...................................................................................16 2.1 CARGO SMOKE ANNUNCIATORS (red) illuminate................................................................16 2.2 ONE OR BOTH MAIN LANDING GEAR POSITION INDICATORS SHOW UNSAFE ........17

SECTION 3 – NORMAL PROCEDURES ............................................................................................17 3.1 VB SPEED (Design speed for maximum gust intensity.) .............................................................17 3.2 MAIN DECK CARGO DOOR .....................................................................................................17 3.3 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM ............................19 3.4 MISCELLANEOUS ANNUNCIATORS .....................................................................................19 3.5 MAIN DECK CARGO COMPARTMENT AIR SUPPLY SHUTOFF........................................19

SECTION 4 - PERFORMANCE............................................................................................................20 APPENDIX.............................................................................................................................................21

CIRCUIT BREAKERS - B737-300 ONLY........................................................................................21 CIRCUIT BREAKERS – B737-400 ONLY .......................................................................................23 MAIN DECK CARGO DOOR EXTERNAL VIEWPORTS..............................................................25



DOOR

CARGOMAINCARGOSMOKE

SECTION 0 – SYSTEM DESCRIPTION

This aircraft has been modified by the installation of a Main Deck Cargo Door and a Main Deck Class E Cargo Compartment.

0.1 MAIN DECK CARGO DOOR The Main Deck Cargo Door is operated by a hydraulic/electrical system independent of the ship’s systems. Electrical power for the hydraulic pump is supplied from the Battery Bus. The hydraulic/electrical system is operated from a Main Deck Cargo Door Control and Relay Box located on the front of the 9g cargo barrier. The door is provided with a Collective Locking System and a system of micro switches which indicate whether the door is closed, the latches are activated and the lock pins are engaged. There are door-warning lights on the Control and Relay Box (see Fig 2), and on the pilot’s and copilot’s instrument panels (see Fig 1).

In the cockpit, there is one Cargo Door (red) annunciator on the lower instrument panel in front of each pilot, and one Cargo Door Armed annunciator in the top center of the instrument panel, above the engine instruments. The Cargo Door Annunciators illuminate any time the door is not closed and locked. The Cargo Door Armed annunciator illuminates any time the cargo door Power Master Control switch on the Control and Relay Box is in the ON position.

On the 737-400 aircraft only, the Cargo Door warning system is connected in parallel to the existing aircraft Takeoff Configuration Warning. If during take-off roll the cargo door is not properly closed, latched and locked, the Takeoff Warning intermittent horn will sound.

Three exterior View Ports are installed to visually verify from outside the airplane that the cargo door is latched and locked (see Fig 8). The cargo door is equipped with two vent doors to prevent cabin pressurization unless the cargo door is fully closed, latched and locked. The main deck cargo door is electrically un-powered in flight.

Fig 1.

0.2 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM Twelve smoke detectors are mounted in the main deck cargo compartment ceiling and are connected to the Main Deck Cargo Smoke Detection System panel. This panel is located in the cockpit aft P5 overhead panel (see Fig 3). Cargo Smoke Annunciator (red) lights are located at the bottom of the captain’s and first officer’s instrument panels (see Fig 1). These two red lights are Press-to-Test lamps and do not dim. The smoke detection system is armed when the No. 2 Main DC bus is energized. Each smoke detector contains an illuminated internal lamp and a light sensor. When the air passing through a detector unit reaches a predetermined smoke density, the internal lamp illumination is reflected on the sensor and a signal is sent to the respective cargo smoke indicator light. The lights remain on until the smoke clears from the detector housing.



SECTION 0 – SYSTEM DESCRIPTION (Continued) MAIN DECK CARGO DOOR CONTROL AND RELAY BOX

Fig 2



SECTION 0 – SYSTEM DESCRIPTION (Continued) 0.2 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM (Cont’d) The Main Deck Cargo Smoke Detection System panel contains twelve individual numbered Smoke Detector lights to indicate which detector(s) has sensed smoke (see Fig 3). The lights are numbered 1 through 12, and correspond to detectors from front to rear of the main deck cargo compartment. A smoke detector test switch is located on the panel to enable a test of the smoke detectors and lights. When this switch is pressed-to-test, the Smoke Detection System lights illuminate, the two Main Cargo Smoke (red) annunciators also illuminate, one in front of each pilot (see Fig 1).

Fig 3.

0.3 MAIN CARGO COMPARTMENT AIR SUPPLY SHUTOFF SYSTEM

The Main Cargo Compartment Air Supply Shut-off System uses two valves to close off the supply of ECS air from the mix manifold to the main cargo compartment during smoke emergencies. The shut-off valves are powered from the No. 2 DC Main bus. The valves are controlled by a guarded, OPEN/CLOSED switch located on the cockpit aft P5 overhead panel (see Fig 4). An adjacent amber light illuminates when the valves are CLOSED. The valves must remain in the OPEN position during all normal operating conditions. In the CLOSED position all airflow to the main cabin is shut off and airflow only continues to the flight deck.

Fig 4.



SECTION 0 – SYSTEM DESCRIPTION-(Continued) 0.4 SECONDARY MAIN LANDING GEAR POSITION INDICATING SYSTEM A Secondary Main Landing Gear Position Indication System has been installed on the cockpit overhead P5 panel to provide the flight crew a back-up means of verifying that the main landing gear is down and locked. This system is provided because the cabin-located main landing gear viewing port is not accessible in flight. The panel consists of two green press-to-test lights to show when the gear is down and locked (see Fig 5). Each main landing gear has a separate back-up gear down and locked sensor to support these Secondary indicators.

Fig 5

SECTION 1-CERTIFICATE LIMITATIONS 1.1 MAIN DECK CARGO DOOR

WIND LIMIT Do not open MAIN DECK CARGO DOOR in actual or anticipated winds exceeding 45 knots. GROUND HANDLING Aircraft is not to be taxied, towed or jacked unless the MAIN DECK CARGO DOOR is in the fully closed and latched position.

1.2 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM

Preflight inspection of the system is required prior to each flight, or each series of flights by the same crew on the same day. See Normal Procedures section of this supplement.

1.3 AIR CONDITIONING PACKS

Flight with freight in the Main Deck Cargo Compartment without at least one air conditioning pack operating is prohibited.



SECTION 1-CERTIFICATE LIMITATIONS (Continued) 1.4 SECONDARY MAIN LANDING GEAR POSITION INDICATING SYSTEM

Preflight inspection of the system is required prior to each flight, or each series of flights by the same crew on the same day. See Normal Procedures section of this supplement under Miscellaneous Annunciators.

1.5 CENTER OF GRAVITY ENVELOPE - B737-300 ONLY The forward center of gravity limit is moved aft for higher weight. See Figures 6a through 6e on the following pages for the new envelope.



1.5 CENTER OF GRAVITY ENVELOPE - B737-300 ONLY (Continued)

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CENTER OF GRAVITY (%MAC)

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FREIGHTER CG CUTBACK

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MAXIMUM TAXIWEIGHT ~ 135500 LB

MAXIMUM TAKEOFFWEIGHT ~ 135000 LB

11.88% 25.99%

MAXIMUM LANDINGWEIGHT ~ 114000 LB

MAXIMUM ZERO FUELWEIGHT ~ 106500 LB

FREIGHTER MIN FLYINGWEIGHT - 78000 LB

27%

133500 LBAT 27.7%

135500 LBAT 11.88%

4.0%

11300

108200

114000 LBAT 8.5%

90000 LBAT 31.0%

127700 LBAT 29%

Airplane Serial Numbers22950, 22952 thru 22959, 23228 thru 23232, 23237, 23310 thru 23314, 23216 thru 23219, 23552 thru 23556, 23558

Fig 6a




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WEIGHT ~ 139000 LB


13% 23%




27%

133500 LBAT 27.7%

135500 LBAT 11.88%

4.0%

11300

108200

114000 LBAT 8.5%

90000 LBAT 31.0%

127700 LBAT 29%

Airplane Serial Numbers23257, 23377,23379 thru 23385, 23514, 23550, 23560, 23594, 23595, 23699 thru 23704, 23739, 23742, 23856 thru 23862, 23931 thru 23937, 24410, 24411, 24412, 24478, 24479, 24515, 24516

Fig 6b




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ITMAXIMUM TAXI

WEIGHT ~ 139000 LB


13% 23%




27%

133500 LBAT 27.7%

135500 LBAT 11.88%

4.0%

11300

108200

114000 LBAT 8.5%

90000 LBAT 31.0%

127700 LBAT 29%

Airplane Serial Numbers23705, 23706

Fig 6c




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ITMAXIMUM TAXI

WEIGHT ~ 140000 LB


13.3% 22.1%




27%

133500 LBAT 27.7%

135500 LBAT 11.88%

4.0%

11300

108200

114000 LBAT 8.5%

90000 LBAT 31.0%

127700 LBAT 29%

Airplane Serial Numbers23255, 23256, 23229, 23230

Fig 6d




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ITMAXIMUM TAXI

WEIGHT ~ 140000 LB


13.3% 22.1%




27%

133500 LBAT 27.7%

135500 LBAT 11.88%

4.0%

11300

108200

114000 LBAT 8.5%

90000 LBAT 31.0%

127700 LBAT 29%

Airplane Serial Numbers23553, 23741, 23743

Fig 6e



1.6 CENTER OF GRAVITY ENVELOPE – B737-400 ONLY

The forward center of gravity limit is moved aft for higher weight. See Figure 7 below for the new envelope.

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ITMAXIMUM TAXI

WEIGHT ~ 143000 LB


15% 28%




24.4%

140000 LBAT 6.1%

4.0%

11300

121000 LBAT 8.5%

97000 LBAT 30.6%

135500 LBAT 5%

Fig. 7



SECTION 1-CERTIFICATE LIMITATIONS (Continued) 1.7 MINIMUM OPERATING WEIGHT

Minimum Operating Weight is 78,000 pounds.

1.8 WEIGHT & BALANCE CONTROL AND LOADING LIMITATIONS Refer to the Weight and Balance control and loading Manual supplements as follows:

• B737-300 Refer to AEI Report No. R-778 Revision D dated May 2, 2007 or later approved Revision

• B737-400 Refer to AEI Report No. R-809 Revision IR dated May 4, 2007 or later approved Revision

1.9 MAIN CARGO COMPARTMENT AIR SUPPLY SHUTOFF

Functionally operate the Main Cargo Compartment Air Supply Shutoff Valve to insure proper operation, prior to each flight, or each series of flights by the same crew on the same day. See Normal Procedures section of this supplement.

SECTION 2 - NON-NORMAL PROCEDURES 2.1 CARGO SMOKE ANNUNCIATORS (red) illuminate

1. Flight Crew - Oxygen Masks and Regulators…………………….……….……ON, 100% 2. Smoke Goggles (If required)………………………………….………………………..ON 3. Crew Communications……………………………………………..………..ESTABLISH 4. Cabin Air Shutoff Valve………………………………………….……….……...CLOSED 5. Cabin Air Shutoff CLOSED light............................................................…....VERIFY ON 6. Isolation Valve….…………………………………………….…….…………....CLOSED 7. Left or Right Air Conditioning Pack ……………………………………………....AUTO 8. Associated Engine Bleed Switch………………………………………..…...VERIFY ON 9. Associated Engine Thrust………………………………………..…………MIN 70 % N1 10. Other Air Conditioning Pack…….………………………………………………..…..OFF 11. Cockpit Air Conditioning Outlets….…………………………………………..…....OPEN 12. Land as soon as possible. If a suitable airport is not immediately available, manually control

the cabin altitude to 20,000 to 25,000 ft until decent to the first suitable airport can be made. Upon departing 20,000 ft, in the landing descent, depressurize the airplane completely.

13. Pressurization Mode Selector…………………..……….……..….MANUAL (AC or DC) 14. Outflow Valve Switch…………….…OPEN, TO SET REQUIRED CABIN PRESSURE

CAUTION: AFTER LANDING, KEEP COCKPIT DOOR AND WINDOWS CLOSED UNTIL READY TO EGRESS.



SECTION 2 - NON-NORMAL PROCEDURES (continued)

2.2 ONE OR BOTH MAIN LANDING GEAR POSITION INDICATORS SHOW UNSAFE

1. Verify the Gear Handle is DOWN. 2. Verify Secondary Main Gear Down and Locked Indicators, on aft P5 overhead panel, are

illuminated green. Main Landing Gear is down and locked as long as at least one green landing gear indicator (center panel or overhead panel) is illuminated for the left gear main and for the right main gear.

3. If lights are not illuminated, follow standard flight manual procedures for unsafe landing gear. SECTION 3 – NORMAL PROCEDURES 3.1 VB SPEED (Design speed for maximum gust intensity.)

VB = 264 KIAS or 0.65 Mach whichever is lower.

3.2 MAIN DECK CARGO DOOR

PRE-FLIGHT CHECK 1. Aircraft Ground Power Bus is active. 2. With the cargo door in the fully open position, verify the indicator lights on the Control and

Relay Box and Pilot and First Officer’s instrument panels are illuminated.

3. Close door per normal operating procedure, below. As the door moves to the fully closed position, monitor the door and lights on the Pilot’s, First Officer’s instrument panel and Control and Relay Box to verify:

a. Main Cargo Door Not Closed light is extinguished b. Hooks Unlocked and Latches Unlocked lights are extinguished c. Latch Lock Pin Not Engaged light is extinguished d. Vent Door Open light is extinguished e. All cargo door related lights on the Control and Relay Box and cockpit instrument panel

are extinguished

4. Return the cargo door Master Power Switch to the OFF position and put the switch guard down.



SECTION 3 NORMAL PROCEDURES (Continued)

5. From the exterior of the aircraft verify:

a. Through the forward and aft View Ports that the lock pins are through the latches b. Through the upper View Port, the black and yellow flag is visible c. The Vent Doors are fully closed and flush with the cargo door d. The cargo door is flush with the surrounding fuselage

TO OPEN MAIN DECK CARGO DOOR (Ground operation only)

1. Turn the Power Master Control Switch, on the Cargo Door Control Panel, to the ON position. Upon selecting the cargo door control to the door OPEN position, the vent doors open and the lock system retracts. The Master Door Warning Light on the Control and Relay Box and the Cargo Door Warning Lights on the cockpit instrument panels will illuminate.

2. Select OPEN on the Door Control Switch. The motor and pump will operate, building hydraulic pressure through the electrically positioned control valve, and supply pressure to the door OPEN hydraulic lines. The latches unlatch and the door opens. When the door reaches its full up position, a micro switch will shut off power to the pump, stopping the door.Return the Door Control Switch to the neutral position. All Cargo Door Warning Lights should be illuminated under this condition.Switch the Master Power Control Switch OFF and put the guard down.

TO CLOSE MAIN DECK CARGO DOOR (Ground operation only)

1. Turn the Power Master Control Switch to the ON position. 2. Select CLOSE on the Door Control Switch. This will activate the pump, sending pressure through the closing lines of the cargo door, and through the electrically positioned selector valve.

a. The door will reach the closed position, extinguishing the “Main Cargo Door Not Closed” light on the control panel.

b. When the door has reached its full down position, the torque tube rotates and the latch hooks move down onto the spools, then move over center, pulling the cargo door into the latched position, and extinguishing both the “Hooks Unlocked”, and “Latches Unlocked” lights on the control panel.

c. The Gang Bar actuator then operates. This pushes the lock pins into place in all latches and closes the two vent doors simultaneously.



3 NORMAL PROCEDURES (Continued)

3. Verify all Door Warning lights on the Control and Relay Box and on the cockpit instrument

panel are extinguished. 4. Move the Door Control Switch to the center position and the Power Master Control Switch to

the OFF position and lower the guard over the switch.

3.3 MAIN DECK CARGO COMPARTMENT SMOKE DETECTOR SYSTEM

PRE-FLIGHT CHECK Main Deck Cargo Compartment Smoke Detector Panel.

1. Press-To-Test Switch……………………………………PRESS and HOLD 2. Verify 12 smoke detector lights………………………...ON 3. Verify both MAIN CARGO SMOKE (red) lights ……..ON

Note: The MAIN CARGO SMOKE (red) lights are located on each pilots’ lower instrument panel.

3.4 MISCELLANEOUS ANNUNCIATORS PRE-FLIGHT CHECK-COCKPIT

Press-To-Test each of the following annunciators

1. CARGO DOOR (P/CP) 2. CARGO DOOR ARMED 3. CABIN AIR SHUTOFF CLOSED 4. SECONDARY MAIN LANDING GEAR DOWN AND LOCKED INDICATORS (2 lights) Note: These lamps must be tested by Press-to-Test as they are not integrated into the cockpit annunciator test circuit.

3.5 MAIN DECK CARGO COMPARTMENT AIR SUPPLY SHUTOFF

PRE-FLIGHT OPERATIONAL CHECK

Cabin Air Shutoff Control Panel. 1. Cabin Air Shutoff Switch Switch-Guard………………..…….....…UP 2. Cabin Air Shutoff Control Switch…………….………….…….…..CLOSED 3. Verify Cabin Air Shutoff CLOSED Indicator (Amber) light …..….ON 4. Cabin Air Shutoff Control Switch…………….………….…….…..OPEN 5. Cabin Air Shutoff Switch Switch-Guard………………..…….....…DOWN 6. Verify Cabin Air Shutoff CLOSED Indicator (Amber) light ……...OFF



SECTION 4 - PERFORMANCE

No change.



APPENDIX CIRCUIT BREAKERS - B737-300 ONLY The following circuit breakers were changed, as indicated, by the Passenger to Freighter conversion:

Circuit Breakers ADDED AC

LABEL CIRCUIT BREAKER PANEL & CB LOCATION

Cargo Door Flood Lts P18-3, B10 Entry Area Lights P18-3, B13

Circuit Breakers ADDED DC

LABEL CIRCUIT BREAKER PANEL & CB LOCATION

Cargo Door Control P6-2, E7

Cabin Lights P18-3, A6

Cabin Lights, Control P18-3, A8

Cargo Door Indication P6-2, E8

Smoke Detection P6-2, E9


Cabin Air Shut-Off P6-2, E10

Hydraulic Pump J9 BATT SHIELD

TCAS / GPWS Spkr P18-1, A4

Secondary MLG Ind P6-2, E11



CIRCUIT BREAKERS - B737-300 ONLY (Continued)

Circuit Breakers Removed-AC (collared)

LABEL BUS NAME Galley System No. 1 115 VAC Gen # 1 Galley System No. 2 115 VAC Gen # 2 Lav Mirror Light, Aft 115 VAC Main # 1

Passenger Reading Lts 28 VAC Main # 1 Vac Clnr Outlet, Fwd 115 VAC GND SVCE

Ceiling Lts, LH 115 VAC GND SVCE Ceiling Lts Cont 115 VAC GND SVCE

Galley Lts 115 VAC GND SVCE Ceiling Lights, R 115 VAC GND SVCE

Vac Clnr Outlet, Aft 115 VAC GND SVCE Window Lts, LH 115 VAC GND SVCE Window Lts, RH 115 VAC GND SVCE

Brt. Entry Lts 115 VAC GND SVCE Night Light Cont 28 VAC GND SVCE

Ceiling Lights Cont 115 VAC XFER # 1 Night Light Cont 28 VAC XFER # 1 Seat Belt Signs 28 VAC XFER # 1

No Smoking Signs 28 VAC XFER # 1 Toilet Flush Mtr, Aft L 115 VAC MAIN # 2

Ceiling Lights, R 115 VAC MAIN # 2 Lav Water Htr, Aft L 115 VAC MAIN # 2 Pass Reading Lts 28 VAC MAIN # 2

Circuit Breakers Removed-DC (collared)

LABEL BUS NAME

28 Volt Svce Outlets 28 VDC BUS No. 1 Pass & Crew Call 28 VDC BUS No. 1 Emerg Exit Lights 28 VDC BUS No. 1

Water Qty Ind 28 VDC BUS No. 1 Pass Sign Control 28 VDC BUS No. 2

Pass Address Ampl 28 VDC BATT BUS Pass Oxygen, L 28 VDC BATT BUS Pass Oxygen, R 28 VDC BATT BUS



CIRCUIT BREAKERS – B737-400 ONLY The following circuit breakers were changed, as indicated, by the Passenger to Freighter conversion:

Circuit Breakers ADDED AC

LABEL CIRCUIT BREAKER PANEL & CB LOCATION Cabin Lights P18-3, A6



Cargo Door Flood Lts P18-3, B10

Entry Area Lights P18-3, B13

Circuit Breakers ADDED DC

LABEL CIRCUIT BREAKER PANEL & CB LOCATION Cargo Door Control P6-2, E7

Cargo Door Indication P6-2, E8

Smoke Detection P6-2, E9

Cabin Air Shut-Off P6-2, E10

Secondary MLG Ind P6-2, E11

TCAS / GPWS Spkr P18-1, A4

Cabin Lights, Control P18-3, A9

Hydraulic Pump J9 BATT SHIELD



APPENDIX CIRCUIT BREAKERS - B737-400 ONLY (Continued)

Circuit Breakers Removed-AC (collared) LABEL BUS NAME

Galley System No. 1 115 VAC Gen # 1 Galley System No. 2 115 VAC Gen # 2 Lav Mirror Light, Aft 115 VAC Main # 1

Passenger Reading Lts 28 VAC Main # 1 Vac Clnr Outlet, Fwd 115 VAC GND SVCE

Ceiling Lts, LH 115 VAC GND SVCE Ceiling Lts Cont 115 VAC GND SVCE

Galley Lts 115 VAC GND SVCE Ceiling Lights, R 115 VAC GND SVCE

Vac Clnr Outlet, Aft 115 VAC GND SVCE Window Lts, LH 115 VAC GND SVCE Window Lts, RH 115 VAC GND SVCE

Brt. Entry Lts 115 VAC GND SVCE Night Light Cont 28 VAC GND SVCE

Ceiling Lights Cont 115 VAC XFER # 1 Night Light Cont 28 VAC XFER # 1 Seat Belt Signs 28 VAC XFER # 1

No Smoking Signs 28 VAC XFER # 1 Toilet Flush Mtr, Aft L 115 VAC MAIN # 2

Ceiling Lights, R 115 VAC MAIN # 2 Lav Water Htr, Aft L 115 VAC MAIN # 2 Pass Reading Lts 28 VAC MAIN # 2

Circuit Breakers Removed-DC (collared) LABEL BUS NAME

28 Volt Svce Outlets 28 VDC BUS No. 1 Pass & Crew Call 28 VDC BUS No. 1 Emerg Exit Lights 28 VDC BUS No. 1

Water Qty Ind 28 VDC BUS No. 1 Pass Sign Control 28 VDC BUS No. 2

Pass Address Ampl 28 VDC BATT BUS Pass Oxygen, L 28 VDC BATT BUS Pass Oxygen, R 28 VDC BATT BUS



APPENDIX MAIN DECK CARGO DOOR EXTERNAL VIEWPORTS

Fig. 8

Aeronautical Engineers, Inc. AFM Supplement to · SECTION 0 – SYSTEM DESCRIPTION This aircraft...

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