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Mobility
Figure V-6. DD Form 2130-5, DC 10-10/30CF Load Plan (Side 1 w/Cargo Pallet Positions)
III-V-18
1. UNIT BEING AIRLIFTED (Name or Number) 2. UNIT IDENTIFICATION CODE 3. TYPE MOVEMENT PLAN 4. MOVEMENT DATE 5. UNIT AIRCRAFT LOAD NO. I PAGE
6. MISSION NUMBER
11. ACTUAL LOAOOUT
7. AIRCRAFT SERIAL NUMBER
SIDE ONE - DC l()"30CF
+ , , , ,
577 676 765 854 943
8. CONFIGURATION 19. DEPARTURE AIRFIELD
,
1032
SCALE: 1/4 INCH - 3 FEET
•
, , + 1121 1210 1299
OF
10. DESTINATION AIRFIELD
,. ,.. , , , I 1477 1566 1665 1883
'~r_------,-~,--------14-Ry----=~42~,~~
1"'""1 I I I I. c.~o~~~ .. " ~113L 1'1 I I 4L1 I I I ISL I I I I ~ I I I ~ I I I 181.1 1_'1 I "-I I I I 'lOLl I I I"; I I I '12L I I I I I I I I I I I I I tl I IlL
523 550 590 630 I Jo I 71~ I 7do 1'90 830 870 910 950 990 1030 1070 1110 1150 1190 1230 1270 1310 1350 1390 1430 1470 1510 1550 1590 1630 1670 1710 1750 17'90 1830 1870 1910 r937
530 570 610 650 690 730 770 810 850 890 930 970 1010 1050 1090 1130 1170 1210 1250 1290 1330 1370 1410 1550 1490 1530 1570 1610 1650 1690 1730 lno 1810 1850 1890 1930
DC lQ..1OCF/40 C.B. CARGO PALLET POSITIONS
FORWARD LOWER COMPARTMENT J.S 71.5 8L.S ... J.n... 10stn
~==========~mmm#==~ [[J ·t-·_·,· -T--·'-
01.11.1. PLT. 4631... PlT
88X125" 88Xl08"
I I
---------3
~~~RP~~m~A~LlM~OOE=lS MCAER7N~~TR
2'12'»-
1 Pe5 8"X9
12. PASSENGER SEATS PLANNING DATA 13_ TOTAL WEIGHT/MOMENT LOADCB
STATION
LOADCB
STATION
OF PAGES
NUMBER I AVG. WEIGHT
SEATS (Pounds Each) WT. rl~4~.~TO~T~MS~------------------------------------------------------~-----------r------~---------r----------+-------r---------------------~
I
TOT AL PLANNED
15 •. LOAD PLANNEfC DATE CERTIFIED TYPED/PRINTED NAME. GRADE, ORGANIZA TlON OF LOADPLANNER SIGNATURE
15b. ACTUAL LOAD PLAN VALIDATOR DATE CERTIFIED TYPED/PRINTED NAME, GRADE, ORGANIZATION OF LDADPLAN VALIDATOR SIGNATURE
DD FORM 2130·5 (BACK), SEP 1998 DC 10-10/30CF LOAD PLAN
Defense Transportation Regulation – Part III 28 January 2010
Mobility
Figure V-6. DD Form 2130-5 (Reverse), DC 10-10/30CF Load Plan (Side 2 w/Cargo Pallet Positions).(Cont’d)
III-V-19
Defense Transportation Regulation – Part III 28 January 2010
Mobility
KC-10A PLANNING DATA
Maximum Takeoff Weight: 590,000 lbs
Normal Operating Weight: 252,000 lbs
Peacetime Planning ACL: 80,000 lbs
Wartime Planning ACL*: 148,600 lbs
NOTE: Maximum payload can only be carried at flight weight of 549,000 lbs or less. At maximum 1.8G flight weight
of 585,000 lbs. Maximum ACL is 137,600 lbs.
CARGO COMPARTMENT
Length - 1508 inches Width - 218 inches ***** Height - 108 inches **
CARGO AREA:
From Fuselage Station 496-2004 (main cargo floor). No lower lobe cargo capability.
VEHICLE LOADING: MAXIMUM WEIGHTS: ****
Station 630-1066: 4,500 lbs per individual axle
Station 1066-1175: 4,800 lbs per individual axle
Station 1175-1502: 3,200 lbs per individual axle
Station 1502-1937: 4,000 lbs per individual axle
PALLETIZED CARGO LOADING: Maximum allowable using HCU-7/E & HCU-15/c Nets
Pallet positions 1 thru 6 (left and right): 6,500 lbs ***
Pallet positions 7 thru 11 (left and right): 10,000 lbs ***
Pallet positions 12 thru 13 (left and right): 6,500 lbs ***
Height of pallet positions 2 thru 10: 96 inches **
Height of pallet position 11 and 12: 96 inches **
PASSENGER LOADING:
Airline seats (Code A): 8 passengers
Airline seats (Code B): 10 passengers
Airline seats (JA/ATT missions) (Code D): 65 passengers
Airline seats:
(Increased Accommodation Kit): 69 passengers
Web passenger seats: Not Available
Paratroops: Not Available
Litter patients (plus medical crew): Not Available
Full sidewall seats only: Not Available
MAXIMUM ON OVER-WATER FLIGHTS: 69 passengers
Figure V-7. KC-10A Planning Data
III-V-20
Defense Transportation Regulation – Part III 28 January 2010
Mobility
NOTES:
1. * Maximum payload is computed without regard to cargo density, is limited only by aircraft structural limitations or
critical leg fuel (4000 NM), and is shown primarily for information. It includes weight of any passengers carried and
should not be used unless cargo density is known to be high and physical characteristics of the cargo would permit
full use of compartment space. Flight route segments less than critical leg distances may allow for more or less ACL
depending on wind factors. Fuel offload requirements for aerial refueling missions may reduce cargo ACL allowable.
　
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