6 Steps to Load Planning 1. I DENTIFY E QUIPMENT / P ERSONNEL FOR AIRLIFT  +/- 5 PERCENT VARIANCE FROM TPFDD 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 / 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 LOSE TO O PTIMAL AS POSSIBLE ( WITHIN +/- 1 PERCENT FOR CLASS ) 6. C OMPLETE HAZ DIP S WORKSHEET FOR EACH C HALK

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 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.

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” 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: Tracked Vehicle WtMax Single Axle Wt 35,000 lbs or less16,000 lbs 35, ,000 lbs11,000 lbs Tracked Vehicle WtMax Single Axle Wt 35,000 lbs or less24,000 lbs 35, ,000 lbs22,000 lbs **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 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 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 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 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 Max Over Water 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 Treadways: 6,000 lbs Axle Treadways: 13,000 lbs Axle Between the Treads: 5,000 lbs Axle 2,000 lbs Tongue 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 **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

C-130J-30 COMPARTMENT LIMITATIONS TO 1C-130J-9 Figure 2-4 C5,500 lbs. C-D9,500 lbs. C-E13,700 lbs. C-F19,300 lbs. C-G23,400 lbs. C-H29,800 lbs. 47,800 lbs.H-M 22,325 lbs.I-M 15,500 lbs.J-M 5,300 lbs.K-M 5,000 lbs.L-M 2,500 lbs.M 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” 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” 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 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.