Load Planning Procedures for Airlift Operations
6 Steps to Load Planning
1.
I
DENTIFY
E
QUIPMENT
/ P
ERSONNEL
FOR
AIRLIFT
+
/
-
5
P
E
R
C
E
N
T
V
A
R
I
A
N
C
E
F
R
O
M
T
P
F
D
D
2.
R
EFERENCE
ATTLA C
ERTS
FOR
APPLICABLE
EQUIPMENT
A
IRCRAFT
L
OADING
I
NSTRUCTIONS
3.
P
LACE
EQUIPMENT
ON
AIRCRAFT
(
S
)
A
ROUND
AIRCRAFT
’
S
OPTIMAL
CG
P
YRAMID
OR
50 / 50
4.
A
DHERE
TO
AIRCRAFT
LIMITATIONS
(V
ISIBLE
L
AYERS
“C
ONSTRAINT
R
EGIONS
”)
R
OLLING
S
TOCK
R
ESTRICTIONS
A
XLES
, H
EIGHT
, W
IDTH
E
ASE
OF
OFF
-
LOAD
P
ALLETS
R
ESTRICTIONS
W
EIGHT
H
EIGHT
C
UTOUTS
B
AGGAGE
R
ESTRICTIONS
A
LWAYS
LOADED
LAST
P
ASSENGERS
R
ESTRICTIONS
R
ESTRICTIONS
NEXT
TO
CARGO
(
I
.
E
. C-17
AND
C-130)
5.
O
PTIMIZE
A
IRCRAFT
CG
C
L
O
S
E
T
O
O
P
T
I
M
A
L
A
S
P
O
S
S
I
B
L
E
(
W
I
T
H
I
N
+
/
-
1
P
E
R
C
E
N
T
F
O
R
C
L
A
S
S
)
6.
C
OMPLETE
HAZ DIP
S
WORKSHEET
FOR
EACH
C
HALK
395
PP 1 &2
Max Wt
7,500 lbs
Max Ht 96”
Note:
14” Aisleway
one 88” side
Pallet Position (PP) 2-34
Max Weight (Wt)
10,355 lbs
Max Height (Ht) 96”
Maximum Weight
36,000 lbs in any 40” Length
Maximum Weight
36,000 lbs in any 40” Length
Maximum Weight
20,000 lbs
in any 40” Length
Maximum
Weight
20,000 lbs
in any 40”
Length
Maximum
Weight
3,600 lbs in
any 20”
Length
Maximum
Weight
3,600 lbs in
any 20”
Length
Maximum Wt: 25,000 lbs
Excludes Tracked Vehicles
517
724
1458
1518
1884
1971
2131
PP 35 &36
Max Wt
7,500 lbs
Max Ht 70”
Note:
14” Aisleway
one 88” side
C-5 CHARACTERISTICS
Maximum Takeoff Weight:
840,000 lbs. (C-5A/B)
837,000 lbs. (C-5M)
Basic Operating Weight:
379,000 lbs. (C-5A/B)
384,000 lbs. (C-5M)
Planning ACL:
130,000 lbs. (C-5A/B)
150,000 lbs. (C-5M)
Optimum Zero Fuel CG:
38%
36% (when Pax/Bags not accounted for)
Height Restrictions
Items over 114 inches must be inset.
Use “Height Constraint” in ICODES to
maximize aircraft space.
Passenger Considerations
Troop compartment is located above
the aft end of the cargo compartment.
A maximum of 73 rear facing seats are
available for use.
*Cross section of C-5 Cargo Compartment
156”
228”
114”
162”
**Items with heights of 114’ to 162”
WILL
have special loading procedures. Reference ATTLA Certification Letter when load planning.
347
1403
Compartment D Floor Limits
Maximum Weight: 72,000 lbs
Maximum Axle:
27,000 lbs (+/- 8 inches of centerline)
22,000 lbs (Side-by-Side)
Compartment E Floor Limits
Maximum Weight: 170,900 lbs
Maximum Axle:
36,000 lbs (+/- 8 inches of centerline)
27,000 lbs (Side-by-Side)
Compartment F
Maximum Wt:
35,000 lbs
Maximum Axle:
27,000 lbs
(+/- 8” center)
22,000 lbs
(Side-by-Side)
Compartment G Floor Limits
Maximum Weight: 40,000 lbs
Maximum Axle:
27,000 lbs (+/- 8 inches of centerline)
22,000 lbs (Side-by-Side)
Aerial Delivery System (ADS)
Pallet Positions 1-11 Loaded on 108” width basis
Max Weight: 10,355 lbs
Max Height: 96”
Logistic Rail System (LRS)
Pallet Positions 1R/L-9R/L Loaded on 88” width basis
Max Weight: 10,355 lbs
Max Height: 96”
1165
1074
578
C-17 CHARACTERISTICS
Maximum Takeoff Weight:
585,000 lbs.
Basic Operating Weight:
284,945 lbs.
Planning ACL:
90,000 lbs.
Optimum Zero Fuel CG:
40% = ZFW less than 400K
39% = ZFW between 400K - 425K
38% = ZFW between 425K - 447K
Passenger Considerations
53 Sidewall Seats
48 Centerline Seats
NOTE
:
Sidewall seats adjacent to cargo
extending past
+/- 85 inches
of aircraft
centerline will
NOT
be used
Tracked Vehicles Beside Single Axle Restrictions
Compartments D, F and G:
Compartment E:
**Items with heights of 148’ to 162”
WILL
have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-130E/H CHARACTERISTICS
Maximum Takeoff Weight:
155,000 lbs.
Basic Operating Weight:
84,000 lbs.
Planning ACL:
25,000 lbs.
Optimum Zero Fuel CG:
20-22%
Pallet Position #2
Max Wt: 10,355 lbs
Max Ht 96”
Pallet Position #1
Max Wt: 10,355 lbs
Max Ht 96”
Note: 12” inset on one
or both 88” sides about
76” height
Pallet Position #3
Max Wt: 10,355 lbs
Max Ht 96”
Note: 6” inset one 88”
side for safety aisle
Pallet Position #4
Max Wt: 10,355 lbs
Max Ht 96”
Note: 6” inset one 88”
side for safety aisle
Pallet Position #5
Max Wt: 8,500 lbs
Max Ht 96”
Pallet Position #6
Max Wt: 4,664 lbs
Max Ht 76”
Note: 20” inset on one
side for safety aisle
257
Treadways:
6,000 lbs Axle
Treadways:
13,000 lbs Axle
Between the Treads:
5,000 lbs Axle
2,000 lbs Tongue
Treadways:
2,500
lbs. Axles**
2,501 – 3,500
lbs. Axle * / **
*Nothing else loaded on Ramp
**Limited to 4,664 lbs. total
Between the Treads:
1,200 lbs. Axle
450 lbs. Tongue
Max Over Land
- 90
Max Over Water
- 74
(Life Raft Capacity)
28 Sidewall Seats
14 Wheel Well Seats
48 Centerline Seats
NOTE
:
Sidewall seats 1L and 15R are not
visible in ICODES (reserved for aircrew)
Between the Treads
Outside the Treads
NO Axles
Outside the Treads
NO Axles
337
737
682
869
Passenger Considerations
Outside Wheel Wells:
Up to 76” = Both Sides
77” to 96” = One Side Only
Greater than 97” = No Pax
Inside Wheel Wells:
Up to 52” = Both Sides
53” to 72” = One Side Only
Greater than 73” = No Pax
Treadways:
6,000 lbs Axle
Most seats deploy as a set of
two(2). Seat sets are bolded
when passengers occupy one
of the seats.
NOTE
:
Ensure
NO
cargo
overlaps deployed seats.
**Items with heights of 102’ to 108”
WILL
have special loading procedures. Reference ATTLA Certification Letter when load planning.
Treadway
35” Wide
Starts 15” right of centerline
Treadway
35 “ Wide
tarts 15” left of centerline
C-130J(S) CHARACTERISTICS
Maximum Takeoff Weight:
164,000 lbs.
Basic Operating Weight:
84,000 lbs.
Planning ACL:
25,000 lbs.
Optimum Zero Fuel CG:
20-22%
Pallet Position #2
Max Wt: 10,355 lbs
Max Ht 96”
Note: 12” inset maybe
needed on one or
both 88” sides about
76” height
Pallet Position #1
Max Wt: 10,355 lbs
Max Ht 96”
Note: 12” inset on one
or both 88” sides about
76” height
Pallet Position #3
Max Wt: 10,355 lbs
Max Ht 96”
Note: 6” inset one 88”
side for safety aisle
Pallet Position #4
Max Wt: 10,355 lbs
Max Ht 96”
Note: 6” inset one 88”
side for safety aisle
Pallet Position #5
Max Wt: 8,500 lbs
Max Ht 96”
Pallet Position #6
Max Wt: 5,000 lbs
Max Ht 77”
Note: 20” inset on
right side for safety
aisle
257
Treadways:
6,000 lbs Axle
Treadways:
13,000 lbs Axle
Between the Treads:
5,000 lbs Axle
2,000 lbs Tongue
Treadways:
2,500
lbs. Axles**
2,501 – 3,500
lbs. Axle * / **
*Nothing else loaded on Ramp
**Limited to 5,000 lbs. total
Between the Treads:
1,200 lbs. Axle
450 lbs. Tongue
Max Over Land
- 90
Max Over Water
- 74
(Life Raft Capacity)
28 Sidewall Seats
14 Wheel Well Seats
48 Centerline Seats
NOTE
:
Sidewall seats 1L and 15R are not
visible in ICODES (reserved for aircrew)
Treadway
35” Wide
Starts 15” right of centerline
Between the Treads
Treadway
35 “ Wide
tarts 15” left of centerline
Outside the Treads
NO Axles
Outside the Treads
NO Axles
337
737
682
869
Passenger Considerations
Outside Wheel Wells:
Up to 76” = Both Sides
77” to 96” = One Side Only
Greater than 97” = No Pax
Inside Wheel Wells:
Up to 52” = Both Sides
53” to 72” = One Side Only
Greater than 73” = No Pax
Treadways:
6,000 lbs Axle
Most seats deploy as a set of
two(2). Seat sets are bolded
when passengers occupy one
of the seats.
NOTE
:
Ensure
NO
cargo
overlaps deployed seats.
**Items with heights of 102’ to 108”
WILL
have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-130J-30 CHARACTERISTICS
Maximum Takeoff Weight:
164,000 lbs.
Basic Operating Weight:
89,000 lbs.
Planning ACL:
40,000 lbs.
Optimum Zero Fuel CG:
20-22%
Max Over Land
- 126
Max Over Water
- 126
46 Sidewall Seats
14 Wheel Well Seats
66 Centerline Seats
NOTE
:
Sidewall seats 1L and 2L are not
visible in ICODES (reserved for aircrew)
Treadway
35” Wide
Starts 15” left of centerline
Between the Treads
Outside the Treads
NO Axles
Outside the Treads
NO Axles
Passenger Considerations
Outside Wheel Wells:
Up to 76” = Both Sides
77” to 96” = One Side Only
Greater than 97” = No Pax
Inside Wheel Wells:
Up to 52” = Both Sides
53” to 72” = One Side Only
Greater than 73” = No Pax
Most seats deploy as a set of
two(2). Seat sets are bolded
when passengers occupy one
of the seats.
NOTE
:
Ensure
NO
cargo
overlaps deployed seats.
PP #2
Max Wt 10,355 lbs
Max Ht 96”
Note: 12” inset
maybe needed on
one/both 88”
sides about 76” ht
PP #1
Max Wt 10,355 lbs
Max Ht 96”
Note: 12” inset on
one/both 88”
sides about 76”
height
PP #4
Max Wt 10,355 lbs
Max Ht 96”
Note: 6” inset one
88” side for safety
aisle
PP #5
Max Wt 10,355 lbs
Max Ht 96”
Note: 6” inset one
88” side for safety
aisle
PP #7
Max Wt 8,500 lbs
Max Ht 96”
PP #8
Max Wt 5,000 lbs
Max Ht 77”
Note: 20” inset on
right side for
safety aisle
345
Treadways:
6,000 lbs Axle
Treadways:
13,000 lbs Axle
Between the Treads:
5,000 lbs Axle
2,000 lbs Tongue
537
882
1133
Treadways:
6,000 lbs Axle
PP #3
Max Wt: 10,355
lbs
Max Ht 96”
PP #6
Max Wt: 10,355
lbs
Max Ht 96”
Treadway
35” Wide
Starts 15” right of centerline
1017
**Items with heights of 102’ to 108” have special loading procedures. Reference ATTLA Certification Letter when load planning.
Treadways:
2,500
lbs. Axles**
2,501 – 3,500
lbs Axle * / **
*Nothing else load’d on Ramp
**Limited to 5,000 lbs. total
Between the Treads:
1,200 lbs. Axle
450 lbs. Tongue
345
383
472
562
652
742
832
922
1124
1011
1042
1141
C-130J-30 COMPARTMENT LIMITATIONS
TO 1C-130J-9 Figure 2-4
T
HESE
LIMITATIONS
MUST
BE
USED
ALONG
WITH
THE
GROSS
WEIGHT
,
CENTER
OF
GRAVITY
,
FLOOR
LOADING
AND
MAXIMUM
CARGO
WEIGHT
LIMITS
OF
THE
AIRCRAFT
. T
HE
LESSER
OF
ALL
THESE
INDIVIDUAL
LIMITATIONS
DEFINE
THE
FINAL
LIMITATION
.
N
OTE
:
T
HESE
ARE
FLIGHT
LIMITS
FOR
THE
C-130J-30
WITH
A
GROSS
WEIGHT
OF
155,000
LBS
.
AT
2.25/2.5G
WITH
NO
ARMOR
(ICODES
STANDARD
). R
EFER
TO
F
IGURE
2-4
FOR
AIRCRAFT
WITH
DIFFERENT
GROSS
WEIGHTS
AND
EQUIPPED
WITH
ARMOR
.
PP 2R / 2L
Max Wt:
6,500 lbs
Max Ht 96”
NOTE
:
If distance between axles is less than 48”
Refer to the “Axle Reduction Chart”
630
1829
1066
1175
1502
PP 3R / 3L
Max Wt:
6,500 lbs
Max Ht 96”
PP 12R / 12L
Max Wt:
6,500 lbs
Max Ht 96”
*PP 11R / 11L
Max Wt:
10,000 lbs
Max Ht 96”
*7,500 lbs
Concentrated
*PP 10R / 10L
Max Wt:
10,000 lbs
Max Ht 96”
*7,000 lbs
Concentrated
PP 9R / 9L
Max Wt:
10,000 lbs
Max Ht 96”
PP 8R / 8L
Max Wt:
10,000 lbs
Max Ht 96”
PP 7R / 7L
Max Wt:
10,000 lbs
Max Ht 96”
PP 6R / 6L
Max Wt:
6,500 lbs
Max Ht 96”
PP 5R / 5L
Max Wt:
6,500 lbs
Max Ht 96”
PP 4R / 4L
Max Wt:
6,500 lbs
Max Ht 96”
Max Axle:
4,500 lbs
(PP 2R/L – 5R/L)
Max Axle:
3,200 lbs
(PP 7R/L – 9R/L)
Max Axle:
4,000 lbs
(PP 10R/L – 12R/L)
Max Axle:
4,800 lbs
(PP 6R/L)
KC-10 CHARACTERISTICS (B-1)
TO 1C-10(K)A-9 Reference Charts
All Cargo:
“Pallet Contour Chart and Aisle Configuration” (Figure 4-2)
Uniform Loads:
Pounds per Linear Foot (PLF) “Load Data” (Figure 4-7)
Concentrated Loads:
“Concentrated Load Limitations “ (Figure 4-19)
Vehicles:
“Vehicle Axle Weight Limitations “ (Figure 4-20)
Items Exceeding Coupled Pallet (T-2) Dimensions:
“Package Size Chart” (Figure 4-3)
D Contour
C Contour
Passenger Considerations
16 Seats
NOTE
:
3-8 seats Reserved for Aircrew
depending on Mission needs
*PP 10 R/L and 11 R/L Special Notes:
10 R/L
is limited to
7,000 lbs
when pallet contains
concentrated loads
11 R/L
is limited
7,500 lbs
when pallet contains
concentrated loads
10 R/L
and
11 R/L
is limited to
8,000 lbs
when loaded
with axles.
Maximum Takeoff Weight:
590,000 lbs.
Basic Operating Weight:
251,631 lbs.
Planning ACL:
65,200 lbs.
Optimum Zero Fuel CG:
24%
**Items with heights over 96”
WILL
have special loading procedures. Reference ATTLA Certification Letter when load planning.
NOTE
:
If distance between axles is less than 48”
Refer to the “Axle Reduction Chart”
1829
1066
1175
1502
PP 12R / 12L
Max Wt:
6,500 lbs
Max Ht 96”
PP 11R / 11L
Max Wt:
10,000 lbs
Max Ht 96”
*7,500 lbs
Concentrated
PP 10R / 10L
Max Wt:
10,000 lbs
Max Ht 96”
*7,000 lbs
Concentrated
PP 9R / 9L
Max Wt:
10,000 lbs
Max Ht 96”
PP 8R / 8L
Max Wt:
10,000 lbs
Max Ht 96”
PP 7R / 7L
Max Wt:
10,000 lbs
Max Ht 96”
PP 6R / 6L
Max Wt:
6,500 lbs
Max Ht 96”
PP 5R / 5L
Max Wt:
6,500 lbs
Max Ht 96”
Max Axle:
4,500 lbs
(PP 5R/L)
Max Axle:
3,200 lbs
(PP 7R/L – 9R/L)
Max Axle:
4,000 lbs
(PP 10R/L – 12R/L)
Max Axle:
4,800 lbs
(PP 6R/L)
KC-10 CHARACTERISTICS (D-1)
Maximum Takeoff Weight:
590,000 lbs.
Basic Operating Weight:
256,615 lbs.
Planning ACL:
65,200 lbs.
Optimum Zero Fuel CG:
24%
D Contour
C Contour
975
Passenger Considerations
75 Seats
NOTE
:
3-8 seats Reserved for Aircrew
depending on Mission needs
TO 1C-10(K)A-9 Reference Charts
All Cargo:
“Pallet Contour Chart and Aisle Configuration” (Figure 4-2)
Uniform Loads:
Pounds per Linear Foot (PLF) “Load Data” (Figure 4-7)
Concentrated Loads:
“Concentrated Load Limitations “ (Figure 4-19)
Vehicles:
“Vehicle Axle Weight Limitations “ (Figure 4-20)
Items Exceeding Coupled Pallet (T-2) Dimensions:
“Package Size Chart” (Figure 4-3)
*PP 10 R/L and 11 R/L Special Notes:
10 R/L
is limited to
7,000 lbs
when pallet contains
concentrated loads
11 R/L
is limited
7,500 lbs
when pallet contains
concentrated loads
10 R/L
and
11 R/L
is limited to
8,000 lbs
when loaded
with axles.
**Items with heights over 96”
WILL
have special loading procedures. Reference ATTLA Certification Letter when load planning.
Efficiently plan and execute the loading of equipment and personnel for airlift operations in compliance with aircraft limitations and constraints. Steps include identifying equipment, optimizing aircraft center of gravity, adhering to weight and height restrictions, and ensuring close-to-optimal distribution. Detailed specifications for C-5 and C-17 aircraft characteristics are provided to guide proper loading procedures.
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6 Steps to Load Planning IDENTIFY EQUIPMENT / PERSONNELFORAIRLIFT 1. +/- 5 PERCENTVARIANCEFROM TPFDD REFERENCE ATTLA CERTSFORAPPLICABLEEQUIPMENT 2. AIRCRAFT LOADING INSTRUCTIONS PLACEEQUIPMENTONAIRCRAFT(S) 3. AROUNDAIRCRAFT SOPTIMAL CG PYRAMIDOR 50 / 50 ADHERETOAIRCRAFTLIMITATIONS(VISIBLE LAYERS CONSTRAINT REGIONS ) ROLLING STOCK RESTRICTIONS 4. AXLES, HEIGHT, WIDTH EASEOFOFF-LOAD PALLETS RESTRICTIONS WEIGHT HEIGHT CUTOUTS BAGGAGE RESTRICTIONS ALWAYSLOADEDLAST PASSENGERS RESTRICTIONS RESTRICTIONSNEXTTOCARGO (I.E. C-17 AND C-130) OPTIMIZE AIRCRAFT CG 5. CLOSETO OPTIMALASPOSSIBLE (WITHIN +/- 1 PERCENTFORCLASS) COMPLETE HAZ DIPSWORKSHEETFOREACH CHALK 6.
C-5 CHARACTERISTICS Height Restrictions Items over 114 inches must be inset. Use Height Constraint in ICODES to maximize aircraft space. Maximum Takeoff Weight: 840,000 lbs. (C-5A/B) Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: 837,000 lbs. (C-5M) 379,000 lbs. (C-5A/B) 384,000 lbs. (C-5M) 130,000 lbs. (C-5A/B) 150,000 lbs. (C-5M) 38% 36% (when Pax/Bags not accounted for) Passenger Considerations Troop compartment is located above the aft end of the cargo compartment. A maximum of 73 rear facing seats are available for use. 156 162 114 228 *Cross section of C-5 Cargo Compartment PP 1 &2 Max Wt 7,500 lbs Max Ht 96 Note: 14 Aisleway one 88 side PP 35 &36 Max Wt 7,500 lbs Max Ht 70 Note: 14 Aisleway one 88 side Pallet Position (PP) 2-34 Max Weight (Wt) 10,355 lbs Max Height (Ht) 96 Excludes Tracked Vehicles Maximum Wt: 25,000 lbs Maximum Weight 3,600 lbs in any 20 Length Maximum Weight 3,600 lbs in any 20 Length Maximum Weight 20,000 lbs in any 40 Length Maximum Weight 36,000 lbs in any 40 Length Maximum Weight 36,000 lbs in any 40 Length Maximum Weight 20,000 lbs in any 40 Length 3 9 5 5 1 7 7 2 4 1 5 1 8 1 8 8 4 1 9 7 1 2 1 3 1 1 4 5 8 **Items with heights of 114 to 162 WILL have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-17 CHARACTERISTICS Tracked Vehicles Beside Single Axle Restrictions Maximum Takeoff Weight: 585,000 lbs. Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: Passenger Considerations 53 Sidewall Seats 48 Centerline Seats NOTE: Sidewall seats adjacent to cargo extending past +/- 85 inches of aircraft centerline will NOT be used Compartments D, F and G: 284,945 lbs. 90,000 lbs. 40% = ZFW less than 400K 39% = ZFW between 400K - 425K 38% = ZFW between 425K - 447K Tracked Vehicle Wt 35,000 lbs or less 35,001 - 65,000 lbs Max Single Axle Wt 16,000 lbs 11,000 lbs Compartment E: Tracked Vehicle Wt 35,000 lbs or less 35,001 - 65,000 lbs Max Single Axle Wt 24,000 lbs 22,000 lbs Logistic Rail System (LRS)Pallet Positions 1R/L-9R/L Loaded on 88 width basis Max Weight: 10,355 lbs Max Height: 96 Aerial Delivery System (ADS)Pallet Positions 1-11 Loaded on 108 width basis Max Weight: 10,355 lbs Max Height: 96 Compartment F Maximum Wt: 35,000 lbs Compartment D Floor Limits Compartment E Floor Limits Maximum Weight: 170,900 lbs Compartment G Floor Limits Maximum Weight: 40,000 lbs Maximum Weight: 72,000 lbs Maximum Axle: 27,000 lbs (+/- 8 center) Maximum Axle: Maximum Axle: Maximum Axle: 36,000 lbs (+/- 8 inches of centerline) 27,000 lbs (Side-by-Side) 27,000 lbs (+/- 8 inches of centerline) 22,000 lbs (Side-by-Side) 27,000 lbs (+/- 8 inches of centerline) 22,000 lbs (Side-by-Side) 22,000 lbs (Side-by-Side) 3 4 7 5 7 8 1 0 7 4 1 1 6 5 1 4 0 3 **Items with heights of 148 to 162 WILL have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-130E/H CHARACTERISTICS Passenger Considerations Most seats deploy as a set of two(2). Seat sets are bolded when passengers occupy one of the seats. Maximum Takeoff Weight: 155,000 lbs. Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: Max Over Land - 90 Max Over Water - 74 (Life Raft Capacity) 28 Sidewall Seats 14 Wheel Well Seats 48 Centerline Seats Outside Wheel Wells: Up to 76 = Both Sides 77 to 96 = One Side Only Greater than 97 = No Pax 84,000 lbs. 25,000 lbs. 20-22% Inside Wheel Wells: Up to 52 = Both Sides 53 to 72 = One Side Only Greater than 73 = No Pax NOTE: Sidewall seats 1L and 15R are not visible in ICODES (reserved for aircrew) NOTE: Ensure NO cargo overlaps deployed seats. Pallet Position #2 Max Wt: 10,355 lbs Max Ht 96 Pallet Position #6 Max Wt: 4,664 lbs Max Ht 76 Note: 20 inset on one side for safety aisle Pallet Position #1 Max Wt: 10,355 lbs Max Ht 96 Pallet Position #3 Max Wt: 10,355 lbs Max Ht 96 Note: 6 inset one 88 side for safety aisle Pallet Position #4 Max Wt: 10,355 lbs Max Ht 96 Note: 6 inset one 88 side for safety aisle Pallet Position #5 Max Wt: 8,500 lbs Max Ht 96 Note: 12 inset on one or both 88 sides about 76 height Outside the Treads NO Axles Treadway 35 Wide Starts 15 right of centerline Between the Treads Treadway 35 Wide tarts 15 left of centerline Outside the Treads NO Axles Treadways: 2,500 lbs. Axles** 2,501 3,500 lbs. Axle * / ** *Nothing else loaded on Ramp **Limited to 4,664 lbs. total Treadways: 6,000 lbs Axle Treadways: 6,000 lbs Axle Treadways: 13,000 lbs Axle 6 8 2 3 3 7 Between the Treads: 1,200 lbs. Axle 450 lbs. Tongue 2 5 7 8 6 9 7 3 7 Between the Treads: 5,000 lbs Axle 2,000 lbs Tongue **Items with heights of 102 to 108 WILL have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-130J(S) CHARACTERISTICS Passenger Considerations Most seats deploy as a set of two(2). Seat sets are bolded when passengers occupy one of the seats. Maximum Takeoff Weight: 164,000 lbs. Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: Max Over Land - 90 Max Over Water - 74 (Life Raft Capacity) 28 Sidewall Seats 14 Wheel Well Seats 48 Centerline Seats Outside Wheel Wells: Up to 76 = Both Sides 77 to 96 = One Side Only Greater than 97 = No Pax 84,000 lbs. 25,000 lbs. 20-22% Inside Wheel Wells: Up to 52 = Both Sides 53 to 72 = One Side Only Greater than 73 = No Pax NOTE: Sidewall seats 1L and 15R are not visible in ICODES (reserved for aircrew) NOTE: Ensure NO cargo overlaps deployed seats. Pallet Position #2 Max Wt: 10,355 lbs Max Ht 96 Pallet Position #6 Max Wt: 5,000 lbs Max Ht 77 Note: 20 inset on right side for safety aisle Pallet Position #1 Max Wt: 10,355 lbs Max Ht 96 Pallet Position #3 Max Wt: 10,355 lbs Max Ht 96 Note: 6 inset one 88 side for safety aisle Pallet Position #4 Max Wt: 10,355 lbs Max Ht 96 Note: 6 inset one 88 side for safety aisle Pallet Position #5 Max Wt: 8,500 lbs Max Ht 96 Note: 12 inset maybe needed on one or both 88 sides about 76 height Note: 12 inset on one or both 88 sides about 76 height Outside the Treads NO Axles Treadway 35 Wide Starts 15 right of centerline Between the Treads Treadway 35 Wide tarts 15 left of centerline Outside the Treads NO Axles Treadways: 2,500 lbs. Axles** 2,501 3,500 lbs. Axle * / ** *Nothing else loaded on Ramp **Limited to 5,000 lbs. total Treadways: 6,000 lbs Axle Treadways: 6,000 lbs Axle Treadways: 13,000 lbs Axle 6 8 2 3 3 7 Between the Treads: 1,200 lbs. Axle 450 lbs. Tongue 2 5 7 8 6 9 7 3 7 Between the Treads: 5,000 lbs Axle 2,000 lbs Tongue **Items with heights of 102 to 108 WILL have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-130J-30 CHARACTERISTICS Passenger Considerations Most seats deploy as a set of two(2). Seat sets are bolded when passengers occupy one of the seats. Maximum Takeoff Weight: 164,000 lbs. Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: Max Over Land - 126 Max Over Water - 126 Outside Wheel Wells: Up to 76 = Both Sides 77 to 96 = One Side Only Greater than 97 = No Pax 89,000 lbs. 40,000 lbs. 20-22% 46 Sidewall Seats 14 Wheel Well Seats 66 Centerline Seats Inside Wheel Wells: Up to 52 = Both Sides 53 to 72 = One Side Only Greater than 73 = No Pax NOTE: Sidewall seats 1L and 2L are not visible in ICODES (reserved for aircrew) NOTE: Ensure NO cargo overlaps deployed seats. PP #2 PP #1 PP #8 PP #3 PP #4 PP #5 PP #6 PP #7 Max Wt 10,355 lbs Max Ht 96 Note: 12 inset maybe needed on one/both 88 sides about 76 ht Max Wt 10,355 lbs Max Ht 96 Max Wt 5,000 lbs Max Ht 77 Note: 20 inset on right side for safety aisle Max Wt: 10,355 lbs Max Ht 96 Max Wt 10,355 lbs Max Ht 96 Note: 6 inset one 88 side for safety aisle Max Wt 10,355 lbs Max Ht 96 Note: 6 inset one 88 side for safety aisle Max Wt: 10,355 lbs Max Ht 96 Max Wt 8,500 lbs Max Ht 96 Note: 12 inset on one/both 88 sides about 76 height Outside the Treads NO Axles Treadway 35 Wide Starts 15 right of centerline Between the Treads Treadway 35 Wide Starts 15 left of centerline Outside the Treads NO Axles Treadways: 2,500 lbs. Axles** 2,501 3,500 lbs Axle * / ** *Nothing else load d on Ramp **Limited to 5,000 lbs. total Treadways: 6,000 lbs Axle Treadways: 13,000 lbs Axle Treadways: 6,000 lbs Axle 5 3 7 8 8 2 Between the Treads: 1,200 lbs. Axle 450 lbs. Tongue 3 4 5 1 1 3 3 1 0 1 7 Between the Treads: 5,000 lbs Axle 2,000 lbs Tongue **Items with heights of 102 to 108 have special loading procedures. Reference ATTLA Certification Letter when load planning.
C-130J-30 COMPARTMENT LIMITATIONS TO 1C-130J-9 Figure 2-4 NOTE: THESEAREFLIGHTLIMITSFORTHE C-130J-30 WITHA GROSSWEIGHTOF 155,000 LBS. AT 2.25/2.5G WITHNOARMOR (ICODES STANDARD). REFERTO FIGURE 2-4 FORAIRCRAFTWITH DIFFERENTGROSSWEIGHTSANDEQUIPPEDWITHARMOR. C 5,500 lbs. C-D C-E C-F C-G C-H 9,500 lbs. 13,700 lbs. 19,300 lbs. 23,400 lbs. 29,800 lbs. 47,800 lbs. 22,325 lbs. H-M I-M J-M K-M L-M M 15,500 lbs. THESELIMITATIONSMUSTBEUSEDALONGWITHTHEGROSSWEIGHT, CENTEROFGRAVITY, FLOORLOADINGANDMAXIMUMCARGOWEIGHT LIMITSOFTHEAIRCRAFT. THELESSEROFALLTHESEINDIVIDUAL LIMITATIONSDEFINETHEFINALLIMITATION. 5,300 lbs. 5,000 lbs. 2,500 lbs. 3 4 5 3 8 3 5 6 2 6 5 2 8 3 2 9 2 2 1 0 1 1 1 1 4 1 4 7 2 7 4 2 1 0 4 2 1 1 2 4
KC-10 CHARACTERISTICS (B-1) Passenger Considerations 16 Seats NOTE: 3-8 seats Reserved for Aircrew depending on Mission needs *PP 10 R/L and 11 R/L Special Notes: Maximum Takeoff Weight: 590,000 lbs. Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: 251,631 lbs. 65,200 lbs. 24% 10 R/L is limited to 7,000 lbs when pallet contains concentrated loads 11 R/L is limited 7,500 lbs when pallet contains concentrated loads TO 1C-10(K)A-9 Reference Charts All Cargo: Pallet Contour Chart and Aisle Configuration (Figure 4-2) Uniform Loads: Pounds per Linear Foot (PLF) Load Data (Figure 4-7) Concentrated Loads: Concentrated Load Limitations (Figure 4-19) Vehicles: Vehicle Axle Weight Limitations (Figure 4-20) Items Exceeding Coupled Pallet (T-2) Dimensions: Package Size Chart (Figure 4-3) 10 R/L and 11 R/L is limited to 8,000 lbs when loaded with axles. D Contour C Contour *PP 10R / 10L Max Wt: 10,000 lbs Max Ht 96 *7,000 lbs Concentrated *PP 11R / 11L Max Wt: 10,000 lbs Max Ht 96 *7,500 lbs Concentrated PP 2R / 2L Max Wt: 6,500 lbs Max Ht 96 PP 3R / 3L Max Wt: 6,500 lbs Max Ht 96 PP 5R / 5L Max Wt: 6,500 lbs Max Ht 96 PP 7R / 7L Max Wt: 10,000 lbs Max Ht 96 PP 4R / 4L Max Wt: 6,500 lbs Max Ht 96 PP 6R / 6L Max Wt: 6,500 lbs Max Ht 96 PP 8R / 8L Max Wt: 10,000 lbs Max Ht 96 PP 9R / 9L Max Wt: 10,000 lbs Max Ht 96 PP 12R / 12L Max Wt: 6,500 lbs Max Ht 96 Max Axle: 4,800 lbs (PP 6R/L) Max Axle: 3,200 lbs (PP 7R/L 9R/L) Max Axle: 4,500 lbs (PP 2R/L 5R/L) Max Axle: 4,000 lbs (PP 10R/L 12R/L) 1 0 6 6 1 5 0 2 1 1 7 5 1 8 2 9 6 3 0 NOTE: If distance between axles is less than 48 Refer to the Axle Reduction Chart **Items with heights over 96 WILL have special loading procedures. Reference ATTLA Certification Letter when load planning.
KC-10 CHARACTERISTICS (D-1) Maximum Takeoff Weight: 590,000 lbs. Basic Operating Weight: Planning ACL: Optimum Zero Fuel CG: Passenger Considerations 75 Seats NOTE: 3-8 seats Reserved for Aircrew depending on Mission needs *PP 10 R/L and 11 R/L Special Notes: 256,615 lbs. 65,200 lbs. 24% 10 R/L is limited to 7,000 lbs when pallet contains concentrated loads 11 R/L is limited 7,500 lbs when pallet contains concentrated loads TO 1C-10(K)A-9 Reference Charts All Cargo: Pallet Contour Chart and Aisle Configuration (Figure 4-2) Uniform Loads: Pounds per Linear Foot (PLF) Load Data (Figure 4-7) Concentrated Loads: Concentrated Load Limitations (Figure 4-19) Vehicles: Vehicle Axle Weight Limitations (Figure 4-20) Items Exceeding Coupled Pallet (T-2) Dimensions: Package Size Chart (Figure 4-3) 10 R/L and 11 R/L is limited to 8,000 lbs when loaded with axles. D Contour C Contour PP 10R / 10L Max Wt: 10,000 lbs Max Ht 96 *7,000 lbs Concentrated PP 11R / 11L Max Wt: 10,000 lbs Max Ht 96 *7,500 lbs Concentrated PP 5R / 5L Max Wt: 6,500 lbs Max Ht 96 PP 7R / 7L Max Wt: 10,000 lbs Max Ht 96 PP 6R / 6L Max Wt: 6,500 lbs Max Ht 96 PP 8R / 8L Max Wt: 10,000 lbs Max Ht 96 PP 9R / 9L Max Wt: 10,000 lbs Max Ht 96 PP 12R / 12L Max Wt: 6,500 lbs Max Ht 96 Max Axle: 4,500 lbs (PP 5R/L) Max Axle: 4,800 lbs (PP 6R/L) Max Axle: 3,200 lbs (PP 7R/L 9R/L) Max Axle: 4,000 lbs (PP 10R/L 12R/L) 1 0 6 6 1 5 0 2 1 1 7 5 9 7 5 1 8 2 9 NOTE: If distance between axles is less than 48 Refer to the Axle Reduction Chart **Items with heights over 96 WILL have special loading procedures. Reference ATTLA Certification Letter when load planning.
