background image

NOTE: If the main tanks are to be fueled individually, fuel the right main tank 

first. 

(12) Observe right main tank master fuel quantity indicator. 

NOTE: The right main tank should be approximately 1/4 full to ensure a 

continuous fuel supply to the right tank boost pumps when transferring 
fuel to the center and forward auxiliary tanks. 

(13) Place forward and aft right main tank fuel boost pump switches in on position. 

NOTE: Fuel boost pump switches are located in the flight compartment on 

forward overhead switch panel. 

(14) Maintain maximum fuel flow through right main tank overwing fill adapter. 
(15) Place right main tank boost pump switches in off position when desired partial fuel 

load in center and forward auxiliary tank is attained. 

(16) If center and forward auxiliary tank maximum fuel load is desired, continue to 

transfer fuel until tank (s) fuel fill valve automatically close; place right main tank 
boost pump switches in off position. 

NOTE: Maximum usable capacity loads are: 

  (a) 6440 lbs. for center tank. 
  (b) 4118 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 tank until fuel level 

reaches overwing fill adapter screen retainer bead. 

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

(20) If main tanks are to be fueled to less than maximum capacity (see paragraph 3.A.). 
(21) Remove fueling nozzle; disconnect nozzle grounding plug. 

CAUTION: MAKE CERTAIN FILL ADAPTER CAP IS LOCKED. 

(22) Install overwing fill adapter cap; lock cap. 
(23) If center and forward auxiliary tank fuel fill valve(s) requires manual control to 

open, use following procedure. 

(a) Place applicable tank fuel fill valve manual control lever to closed position.

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 5

1999/11/15

This page must not be retained for reference

Summary of Contents for DC-9

Page 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...

Page 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...

Page 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...

Page 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...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Page 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 ...

Reviews: