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CHECK THAT MAIN GEAR INBOARD DOORS ARE CLOSED 
BEFORE FUELING AIRPLANE. 

A. Main Fuel Tanks 

(1) Connect 

fueling 

unit/airplane grounding cable. 

CAUTION: OBSERVE THE NO STEP AREAS ON WINGS. 

(2)  Use ladder or suitable stand at wing leading edge to gain access to overwing fill 

adapter (see 

Figure 301 

). 

(3)  Connect fueling-nozzle-grounding plug to airplane grounding receptacle. 
(4)  Insert fueling nozzle in fill adapter. Slowly open fueling nozzle valve; commence 

fueling. 

(5)  If main tank maximum fuel load is desired, fuel each main tank until fuel level 

reaches overwing fill adapter screen retainer ring bead. 

NOTE: Maximum usable capacity loads are 9841 lbs. for each main tank.

(6)  If main tanks are to be fueled to less than maximum capacity, use following 

procedure. 

(a) Open fueling control panel access door.. 
(b) Place fueling control panel power switch in on position; verify that power 

indicator blue light comes on (see 

Figure 302 

). 

NOTE: If external electrical power is not available to supply the airplane load 

buses, airplane battery power will automatically be supplied to the 
ground refueling circuit when the fueling control panel power switch 
is placed in the on position. Conservative use of airplane battery 
power for fuel quantity indication is permissible. 

(c) Momentarily hold fuel quantity repeater-indicator (gage) test switch in test 

position to test indicators; pointers will move towards zero, when switch is 
released, pointers will return to original quantity. 

(d) Monitor main tank fuel quantity indicators (or magnetic dripless fuel 

measuring sticks, if fuel quantity indicators are inoperative). 

(e) Continue fueling until desired fuel load in each main tank is attained. 
(f)  Place panel power switch in off position. 
(g) Close access door. 

(7) Remove 

fueling 

nozzle. 

(8) Disconnect 

fueling 

nozzle grounding plug. 

ABX Air Inc. 
Printed: 8/27/2010 at 12:10:53 
PM 
REV 11 2008/12/11

DC-9 

MAINTENANCE MANUAL

 

EFFECTIVITY: 900-905, 909, 928, 930, 934, 939, 
953-960, 962-964, 980-984, 986 

12-12-00-3

CONFIG 00

Page 2

1999/11/15

This page must not be retained for reference

Содержание DC-9

Страница 1: ...upply Systems Los Altos Calif To drain sump B Sump drain tool 4298 1 Roylyn Inc Glendale Calif To drain sump C Drain bottle assembly 700200 1 Accessory Products Co Whittier Calif To drain sump 3 Gravity Fueling WARNING DO NOT OPERATE RADIO RADAR OR ANY OTHER ELECTRICAL ELECTRONIC EQUIPMENT ON AIRPLANE EXCEPT AS SPECIFIED RADAR AND HIGH FREQUENCY EQUIPMENT OPERATING IN VICINITY OF AIRPLANE DURING F...

Страница 2: ...TE If external electrical power is not available to supply the airplane load buses airplane battery power will automatically be supplied to the ground refueling circuit when the fueling control panel power switch is placed in the on position Conservative use of airplane battery power for fuel quantity indication is permissible c Momentarily hold fuel quantity repeater indicator gage test switch in...

Страница 3: ...ediately after upward force is applied to tool The sump tool permits a fluid flow rate in excess of 3 gallons per minute creating the siphoning action necessary to remove a maximum amount of free water from the tank sumps and thus reduces corrosion and soaping time b Drain tank sump until water ceases to flow NOTE Fuel tank sumps should be drained after sufficient time approximately 45 minutes for...

Страница 4: ...t position to test indicators pointers will move towards zero when switch is released pointers will return to original quantity 6 Determine fuel load 7 Place center and forward auxiliary tank fuel fill valve control switch in auto fill position verify that tank fill valve manual control lever s moves to open position see Figure 302 8 If applicable tank fuel fill valve s do not open use following p...

Страница 5: ...lbs for forward auxiliary tank 17 If center and forward auxiliary tank fuel fill valve s required manual control to open place boost pump switches in off position when either partial or full tank s fuel loading is attained 18 Place fueling control panel center and forward auxiliary tank fuel fill valve s control switch in closed position 19 If main tank maximum fuel load is desired fuel each main ...

Страница 6: ...drain valves operate identically a Insert probe of drain tool in center recess of sump drain valve and apply upward force NOTE Fuel should flow immediately after upward force is applied to tool The sump tool permits a fluid flow rate in excess of 3 gallons per minute creating the siphoning action necessary to remove a maximum amount of free water from the tank sumps and thus reduces corrosion and ...

Страница 7: ...ovisions ABX Air Inc Printed 8 27 2010 at 12 10 53 PM REV 11 2008 12 11 DC 9 MAINTENANCE MANUAL EFFECTIVITY 900 905 909 928 930 934 939 953 960 962 964 980 984 986 12 12 00 3 CONFIG 00 Page 7 1999 11 15 This page must not be retained for reference ...

Страница 8: ...rol Station ABX Air Inc Printed 8 27 2010 at 12 10 53 PM REV 11 2008 12 11 DC 9 MAINTENANCE MANUAL EFFECTIVITY 900 905 909 928 930 934 939 953 960 962 964 980 984 986 12 12 00 3 CONFIG 00 Page 8 1999 11 15 This page must not be retained for reference ...

Страница 9: ...ueling Transfer Schematic ABX Air Inc Printed 8 27 2010 at 12 10 53 PM REV 11 2008 12 11 DC 9 MAINTENANCE MANUAL EFFECTIVITY 900 905 909 928 930 934 939 953 960 962 964 980 984 986 12 12 00 3 CONFIG 00 Page 9 1999 11 15 This page must not be retained for reference ...

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