Equipment List 3. Lavatory Service Truck SLS-350-PL-G.pdf

Internal Air Transport Certification

AFLCMC/EZFC (ATTLA)

2145 Monahan Way

WPAFB, OH 45433-7017

https://cs3.eis.af.mil/sites/AFLCMCEZF/AirCerts

Date: 13 January 2015 Item Nomenclature: Lavatory Service Truck SLS-350-PL-G File Number: 2011.07.21 Rev 2 Requestor: On File Superseded Certification Date: 30 November 2012

New Information Summary: Added the 2014 Model Truck which has an increased GVWR.

Item Description: The subject item is identified to be two models of Lavatory Service Truck (LST) with a hydraulic pedestal lift on a Ford F-350 Chassis. Approximate dimensions are 289” L x 98” W x 82” H. The weights and vehicle ratings are given in Table 1 for the 2012 and 2014 Models.

Table 1: Weights and Ratings for Two Models of the Lavatory Service Truck

2012 Model 2014 Model Gross vehicle weight 11,580 lbs 12,160 lbs Gross vehicle weight rating (GVWR) 13,300 lbs 14,000 lbs Front axle weight 3,940 lbs 4,240 lbs Front axle rating 5,250 lbs 5,250 lbs Rear axle weight 7,640 lbs 7,920 lbs Rear axle rating 9,750 lbs 9,750 lbs

NOTE: The listed dimensions are approximations. Actual dimensions can vary as long as aircraft limitations published in applicable cargo loading manuals and the conditions of certification listed below are not violated. Adjustments to approach shoring and/or loading methods shall be reported to ATTLA.

Figure 1: Lavatory Service Truck

Certified Aircraft: USAF C-130, C-17 and C-5

Conditions of Certification:

1. Maximum Weight for Air Transport:

a. Gross Vehicle Weight: 2012 Model – 13,300 lbs; 2014 Model – 14,000 lbs

File Number 2011.07.21 Rev 2

b. Axle Limits:

Front - 4,200 lbs (without sleeper shoring); 5,250 lbs (with sleeper shoring)

Rear - 7,800 lbs (without sleeper shoring); 9,750 lbs (with sleeper shoring)

2. Item Preparation:

a. Shipper is responsible for providing all shoring materials. See paragraph 5 for specifications.

b. All hazardous materials (to include fuel level, batteries, etc.) must be prepared and certified for airlift in accordance with TM 38-250/AFMAN 24-204(I). Do not consider this air transport certification as approval for hazardous materials. Authorization for airlifting hazardous material is the responsibility of 401 AFMC/A4RT (DSN 787-4503 or COM (937) 257-4503).

3. Loading Instructions:

a. The Lavatory Service Truck can be loaded using general loading procedures as listed in the respective aircraft cargo loading manual.

b. Approach shoring is required; see paragraph 5 for specifications. The option to load with over the toe shoring on the C-5 and C-17 is listed in paragraph 5.

c. Sleeper shoring (if required per paragraph 1) shall be placed under the axles or the frame near the axles on each side (4 stacks); see paragraph 5 for specifications.

4. Restraint Requirements: The Lavatory Service Truck and all accompanying cargo must be restrained to meet MIL-STD-1791 requirements of 3G forward, 1.5G aft and lateral, and 2G up. In addition, stored or installed equipment must meet these requirements and be capable of withstanding a 4.5G down load. There are six tiedown provisions installed on the LST, four are midway under the body attached to the frame and two are on the aft end, shown in Figures 2 and 3. Rated capacity of the tiedown provisions is listed in Table 2. Restraint may be applied to axles up to their rated capacity in longitudinal and lateral directions as listed in the Item Description paragraph. Do not apply more than 50% of required restraint to vehicle axles for longitudinal and lateral directions. Note that spring mounted axles provide zero vertical restraint.

Figure 2: Tiedown Locations

Example of Tie-down Pattern

Table 2: Provision Location & Rated Capacities Provision Location Rated Capacity

Chassis Frame (3 & 4) 25,000 lbs Chassis Frame (5 & 6) 25,000 lbs Rear Tiedown (9 &10) 5,000 lbs

Figure 3: Tiedown provisions under the body

5. Required Shoring Dimensions & Diagrams:

a. Approach shoring: minimum recommended dimensions for 7˚ approach angle, requirements for other configurations are in the applicable aircraft loading manual.

C-5 Shoring

C-5 Forward Shoring (Forward Kneel) Pedestal Shoring “A” 16” L x 13” W x 10” H (2 each inboard) 18” L x 15” W x 10” H (2 each outboard) “B” 15” L x 15” W x 21” H (4 each) Approach Shoring “C” 251” L x 24” W x 26” H (2 required) (Ramp toe end shall be supported by the approach shoring – min 11” L)

(C-5) CAUTION: Width of approach shoring “C” in the area under the toe must be as wide as the ramp toe it is placed under. The remaining approach shoring extending away from the ramp toe extension contact point must be a minimum of 24 inches wide.

C-5 Over the Toe Option (both forward and aft kneel drive in configuration use same shoring)

28 boards are required to make the shoring. The stacks will be placed two wide per side to achieve a width of approximately 24”.

(1) 2x12x96 4 ea

(2) 2X12X90 4ea

(3) 2X12X84 4ea

(4) 2X12X76 4ea

(5) 2X12X70 8ea

(6) 2X12X60 4ea

Figure 4: C-5 over the toe shoring (front end)

C-17 Shoring

C-17 Shoring Ramp Pedestal Shoring “A” 18” L x 30” W x 13” H Approach Shoring “B” 285” L x 30” W x 30” H (2 required)

C-17 Over the Toe Option

32 boards are required to make the shoring. The stacks will be placed two wide per side to achieve a width of approximately 24”.

(1) 2x12x96 4 ea

(2) 2X12X90 4ea

(3) 2X12X84 4ea

(4) 2X12X76 4ea

(5) 2X12X70 4ea

(6) 2X12X60 4ea

(7) 2X12X48 8ea

Figure 5: C-17 over the toe shoring

C-130 Shoring

C-130 Shoring Pedestal Shoring “A” 18” L x 18” W x 12” H Approach Shoring “B” 201” L x 24” W x 21” H (2 required)

b. Sleeper Shoring (When Required):

(1) Front Axle: 8” L x 8” W. The sleeper shoring must be stacked to within ½” of chassis/frame area and secured with cargo straps.

(2) Rear Axle: 10” L x 10” W. The sleeper shoring must be stacked to within ½” of chassis/frame area and secured with cargo straps.

Required Distribution:

1. Shipper shall give a copy of this certification to the ATOC representative when the item is presented for airlift. This certification shall be part of the official cargo manifest documentation package and shall be briefed to the aircraft loadmaster prior to loading this item.

2. AMC/A3V & AMC/A4T

3. SDDCTEA.

Point of Contact: Peggy Miedlar, at peggy.miedlar@us.af.mil or ATTLA@us.af.mil, DSN 986-9856 or Commercial (937) 656-9856. Refer to file number 2011.07.21 Rev 2 regarding this item.

Reviewed by: BRIAN L. HERRIOTT Aerial Delivery Specialist Crew Systems Branch

Approved by: MARK A. KUNTAVANISH

Aerial Delivery Technical Expert Crew Systems Branch mailto:peggy.miedlar@us.af.mil