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INCREMENT NO. (FrO;"O~~ h.J OTHER REMARKS LENGTH WIDTH HEIGHT II.. (10,000) (Tota/Pounds) STATION (10,000)
OF PAGES
h. REMARKS
CODES
(For use in col. d.)
1. OFF CENTER:
1A RIGHT
1 B LEFT
2. CENTER LINE
LOAD
~--~------------+------------_+---~-------~---_+---__i,_----t_----__i----+----~-----~----+-------i3.SHORING
t----+---------------+-------------+----__+_-------1-~--+---__+_---t-------+----- .. -. . - ~-
REQUIRED:
3A PARKING
3B ROLLING
3C SLEEPER
3D SPECIAL
--1------+----+-------1 ~~,¥r(M'6 IN
DIRECTION OF
ARROW
1------1------------+-------------+----+--------+---+----11-----+-------1----+-----+------+---+-------~5.SPECIAL
HANDLING
(DO Form 1387-2)
I-----+-------------+-------------+-----+--------+---+----il-----+-------i----+-----+------+---+------~6.HAZARDOUS
MATERIAL
CERTIFICATION
r---~-=-=~~ ____ -----~~~~~~~~~~~~~~--L-------L--~--~-'-----t----------i~~:==_+-----+-------~~~~1---------_i~~gfa:~iooror
12. PASSENGER SEATS PLANNING DATA 13. TOTAL WEIGHTIMOMENT FROM BACK ~~:~,g= ~~~= Dangerous Goods)
NUMBER AVG. WEIGHT I TOTAL PLANNED f-:.,=-===,------------------------------If-------_+---~-----_+-----1----+--------1 77X,Afi~MfA~~UEL:
SEATS (Pounds Each) WT. 14. TOTALS 7B 1/2 TANK
1-:-: 15:-.--,.L :-:O:-:A:::D:-!PLA::-:-N"'N:::ER::::----L-----~D:-:A-=T=-E" 'CE::-:R::::T"'IF"'IE::::D---r.T""Y::::P:::ED'"'/::::PR:::C,N"'T:::E"'D-:-N:-:A-:-M:::E-.G "'R=-A:-:D:::E-, O=-R"'G"'A:-:N"'IZ:-:A-=T"'IO:N7,-,O::-:F:-:L-=O:-:A"'D::::PLA....,-"N"'N:::ER::-----f-::S:-I::G::"'N-:-A::::TU-;-:R::::E-~-'----......L-------'------L----'-------j M?~Jb~p~NRi,ED
8A DRAINED
NOT PURGED
8B PURGED
15b. ACTUAL LOAD PLAN VAlIOATOR DATE CERTIFIED
DD FORM 2130-11. SEP 1998
TYPED/PRINTED NAME. GRADE, ORGANIZATION OF LOADPLAN VALIDA TOR SIGNATURE
PREVIOUS EDITION IS OBSOLETE. DeSIgned uSing Perform Pro, WHS/DIOR
9. VENT KIT
REQUIRED
B707-300C LOAD PLAN
Defense Transportation Regulation – Part III 28 January 2010
Mobility
Figure V-13. DD Form 2130-11, B707-300C Load Plan (w/Cargo Pallet Positions)
III-V-27
1. UNIT BEING AIRLIFTED (Name or Number) 3. TYPE MOVEMENT PLAN
OF PAGE OF PAGES
6. MISSION NUMBER 7. AIRCRAFT SERIAL NO. 9. DEPARTURE AIRFIELD
11. ACTUAllOADOUT (Continued on back.) SCALE - 114 INCH = 3 FEET
t, , t ' , t ' I ' t : I I I§', I I ' t
200 300 400 soo: ~1iJ~0 11&0
2400
5~5
ZONES, VA VB Ve~VD- VE VF------";
~ I
135541365
VCMINIZONE
'100F SIDE DOOR ONLY
20De NOSE DOOR ONLY
200F NOSE AND SIDE DOOR
514 611 730 827 924
t t t t t 15t3 1 16128 117 25 18t2 2
DO FORM 2130-12, SEP 1998 PREVIOUS EDITION IS OBSOLETE. CARGO MANIFEST, B747-100F/200C/200F
Defense Transportation Regulation – Part III 28 January 2010
Mobility
Figure V-14. DD Form 2130-12, Load Plan B747-100F/200C/200F
III-V-28
Defense Transportation Regulation – Part III 28 January 2010
Mobility
C-17A PLANNING DATA
Maximum Takeoff Weight: 585,000 lbs
Normal Operating Weight: 276,000 lbs
Peacetime Planning ACL: 90,000 lbs
CARGO COMPARTMENT:
Length - 1056 inches Width - 216 inches Height - 148 inches**
CARGO AREA:
From Fuselage Station 347-1165 (main cargo floor) and from Station 1165-1403 (aircraft ramp).
VEHICLE LOADING: Maximum weights.
Station 347-578 and Station 1073-1165 27,000 lbs per individual axle
Station 578-1073 36,000 lbs per individual axle
Aircraft Ramp (Station 1165-1403 27,000 lbs per individual axle
PALLETIZED CARGO LOADING: Maximum allowables using HCU-7/E & HCU-15/C nets.
Logistics rail system:
(Pallet positions 1L-9L and 1R-9R): 10,355 ***
Aerial delivery system:
(Pallet positions 1-11): 10,355 ***
Height of all pallet positions: 96 inches
PASSENGER LOADING:
Permanently installed seats: 54 passengers
Onboard centerline seat kit: 48 passengers
Paratroops (maximum): 102 paratroops
Onboard litter capacity: 12 litters
Additional litter capacity: 36 passengers
MAXIMUM ON OVER-WATER FLIGHTS: 102 passengers
NOTES:
1. * The maximum payload is computed without regard to cargo density. It is limited only by aircraft structural
limitations or critical leg fuel (2500NM) and is shown primarily for information. It includes weight on any passengers
carried. It should not be used unless cargo density is known to be high and physical characteristics of 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. If tanker support can be provided with aerial refueling qualified aircrews, the C-
　
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