Attch_1_C-130_FuT_PWS

W900KK-10-T-0043 Attachment 1

C-130 Aircrew Training System (C-130 ATS) Performance Work Statement C-130 Fuselage Trainer (FuT) Conversion 12 August 2010

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CONTENTS OBJECTIVE ....................................................................................................................................3 1.0 INTRODUCTION ....................................................................................................................3 1.1 Scope ...................................................................................................................................3 1.2 Government Furnished Equipment/Information/Property (GFE/GFI/GFP) ........................3 2.0 APPLICABLE DOCUMENTS ................................................................................................3 3.0 REQUIREMENTS .....................................................................................................................4 3.1 PROGRAM MANAGEMENT ..................................................................................................4 3.1.1 Risk Management .......................................................................................................4 3.1.2 Associate Contractor Agreements (ACA) ..................................................................4 3.2 Technical Requirements.......................................................................................................4 3.2.1 Reviews .......................................................................................................................5 3.2.1.1 Kick-Off Meeting (Meeting #1).........................................................................5 3.2.1.2 Meeting #2 .........................................................................................................5 3.2.1.3 Meeting #3 .........................................................................................................6 3.3 Test and Evaluation.............................................................................................................6 3.3.1 Inspection and Acceptance Testing ............................................................................6 3.3.2 Closure Criteria ...........................................................................................................6 3.3.2.1 Test Discrepancies .............................................................................................6 3.4 Quality Assurance/Quality Assurance Personnel (QAP) .....................................................7 3.5 Packing and Crating .............................................................................................................7 3.6 Safety ...................................................................................................................................7 4.0 DELIVERABLES ......................................................................................................................7 4.1 Technical Data Package .......................................................................................................7 4.1.1 Warranty and Licenses ................................................................................................7 4.2 Contractor Acquired Property ..............................................................................................7 4.3 Contract Data Requirements List (CDRL) ..........................................................................8 APPENDIX #1 FUT FUNCTIONALITY REQUIREMENTS .....................................................10 APPENDIX #2 FUT GOVERNMENT FURNISHED PROPERTY (GFP) .................................26 APPENDIX #3 INSTRUCTOR OPERATOR STATION EXAMPLE.......................................27 APPENDIX #4 C-130 ATS FUT FIDELITY REQUIREMENTS ................................................35 APPENDIX #5 FUT DRAWINGS, PHOTO’S .............................................................................38 APPENDIX #6 FUT DESIGNATED SAVE ITEMS LIST ..........................................................41

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W900KK-10-T-0043 Attachment 1 OBJECTIVE The overall objective of this C-130 Fuselage Trainer (FuT) Conversion effort is to provide an additional permanent C-130 FuT at Little Rock AFB. The contractor shall manage and modify the Government Furnished C-130E aircraft IAW the contractor provided Program Management Plan. 1.0 INTRODUCTION 1.1 Scope This Performance Work Statement (PWS) defines the effort accomplished by the FuT conversion contractor (herein referred to as the contractor) in providing management, labor, materials, fabrication, test, technical data package, and Government acceptance of the C-130E Fuselage Trainer (FuT) located at Little Rock AFB, AR. The contractor shall modify the Government Furnished C-130E aircraft by removing the aircraft nose radome, aircraft wings, aircraft tail section and other identified components outlined in this PWS, providing normal aircraft functionality that loadmasters would normally have in a flight worthy, operational aircraft. The delivered FuT shall also meet all requirements in Appendix #1, FuT Functionality Requirements upon delivery accompanied with a Technical Data Package. Using GFP listed in appendix #2, the contractor shall perform the required task outlined throughout this PWS. Appendix #3 provides an example of the IOS station that will be constructed by the contractor to include photos and wiring diagrams.. Appendix #4 has a list of the pre/post modification baseline fidelity requirements. The aircraft wings, after removal at the production breakpoint, shall be further removed as identified in Appendix #5 and disposed of by the Contractor. The contractor shall be responsible for shipping the aircraft nose, aircraft wings, aircraft tail section and other components listed on the SAVE List in Appendix #6. Other aircraft components removed during the fuselage modification shall be turned into the Air Force Supply System. This effort shall be coordinated with the ATS prime contractor through the Government for inclusion into the ATS program Integrated Master Schedule (IMS). The fuselage trainer will be integrated into the Air Force’s Aircrew Training System. 1.2 Government Furnished Equipment/Information/Property (GFE/GFI/GFP) The following GFE/GFI shall be included within the scope of this modification: C-130E Aircraft 63-7784. Flight Line location as directed by the Government. Aircraft Technical Orders (TO), these TO’s shall be utilized by the awarded contractor to generate the Technical Data Package (CDRL B004). 2.0 APPLICABLE DOCUMENTS The following Appendices form a part of this PWS to the extent specified herein. 1) Appendix #1 – FuT Functionality Requirements. 2) Appendix #2 – FuT Government Furnished Equipment. 3) Appendix #3 – FuT Instructor Operator Station (IOS) example. 4) Appendix #4 – C130 ATS FuT Fidelity Requirements 5) Appendix #5 - FuT Drawing to Indentify Responsibility 6) Appendix #6 – FuT Designated Save Items List

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W900KK-10-T-0043 Attachment 1 3.0 REQUIREMENTS The contractor shall provide the labor, materials, support equipment, and tools necessary to accomplish the requirements as outlined in paragraph 3 of this PWS. The contractor, in accordance with appendix # 5, shall remove the wings (at the production breakpoint), the vertical and horizontal stabilizers, the radome, and other aircraft components listed in the SAVE List of appendix #6. The contractor shall construct crates, package, and ship all components identified on the SAVE List to CONUS locations designated by the Government and turn in any remaining components to the government IAW Air Force Supply System requirements and guidelines. The contractor shall install an Instructor Operator Station (IOS, with an NVG compatible flood lamp/light that will illuminate the IOS station allowing operation under night vision condition scenarios), Air Deflector Switch (at the junction box in the aft section of the fuselage), Jump/Caution Lights switch (at the IOS and junction box in the aft section of the fuselage), and beef-up plate in accordance with this PWS. The contractor shall be responsible for “clipping” the wings from the production breakpoint back to the fuselage. The contractor shall correctly terminate all electrical, fuel, pneumatic, and hydraulic lines. The contractor shall provide a sheet metal cap that is sealed providing weather proof protection from corrosion over the wings, tail section and radar antennas that are removed. The contractor shall provide a beef-up plate for structural support across the area where the horizontal stabilizer was removed (see appendix # 5 for photos). The contractor shall deliver a Technical Data Package (TDP). 3.1 PROGRAM MANAGEMENT The Contractor shall provide program management, labor, materials, and other resources necessary to meet the requirements of the contract. The Contractor shall establish and maintain a Program Management Plan (CDRL A003) to include the contractor’s methodology to meet the requirements of paragraph 3 and 4 of this PWS, planning, scheduling, directing, and controlling the administrative, management, technical, logistical, financial production, and support functions of this contract. The contractor’s Program Management Plan shall discuss the contractor’s Test & Evaluation and Inspection & Acceptance Testing programs. The Contractor shall designate a management point of contact for interface with the Government for all issues regarding this program. The Contractor shall monitor the progress of all the work performed and costs incurred under the contract. The Contractor shall be fully responsible to exercise due diligence in managing any subcontractors and vendors. 3.1.1 Risk Management The Contractor shall implement its standard risk management processes and shall identify low, medium, and high risks for the project, including cost, performance, schedule, and supportability risks. The Contractor shall track medium risks, shall manage and mitigate high risks, shall perform a program risk analysis, and shall report results to the Government Program Office at each review. 3.1.2 Associate Contractor Agreements (ACA) The Contractor shall implement ACAs, as required, for the purposes of exchanging data, accessing and using third party equipment, receiving technical support, establishing working interface issues, and/or agreeing on equipment use and time for the modification. 3.2 Technical Requirements The Contractor shall provide the necessary engineering, equipment, testing, technical, supervisory, and logistics support in accordance with the requirements of this PWS. The Contractor shall comply with all specifications in Appendix #1, FuT Functionality Requirements. Physical characteristics of any new or modified components (Instructor Operator Station (IOS), Air Deflector Switch, Jump/Caution Lights Page 4

W900KK-10-T-0043 Attachment 1 switch, Beef-up plate) of the C-130 FuT shall be compatible with all other elements of the ATS, and in accordance with best commercial practice for transportation, storage, and durability. The Contractor shall not make unauthorized modifications to the training system or equipment. The contractor shall comply with all Air Force Technical Orders in the disassembly and removal of all aircraft components and parts applicable to this conversion effort. All movement of the aircraft will be by and under the direction of the government. The design for this modification shall mirror the configuration and operation of the existing FuT devices and shall be structurally configured in the same manner as current FuT devices (i.e. tail stiffening beam, wing root caps, IOS, Air Deflector Switch (junction box in the aft section of the fuselage), Jump/Caution Lights switch (at the IOS and junction box in the aft section of the fuselage, etc.). The IOS faceplate should closely replicate the drawing in Appendix #3 and be more consistent with other aircraft panels. The Contractor shall have full responsibility for analyzing received data and developing work-around or migration solutions. 3.2.1 Reviews The Contractor shall support, participate in, or host (as appropriate) the reviews listed in the following paragraphs. Schedule and technical status issues shall be discussed at all reviews. Contractor shall prepare agendas and minutes for all reviews (CDRLs A001, A002). 3.2.1.1 Kick-Off Meeting (Meeting #1) The Contractor shall conduct a Kick-Off meeting within 15 days after contract award at the Government’s facility (Det 3, Little Rock AFB, AR). The purpose of this meeting is to review requirements line-by-line, and to resolve any conflicts early in the program. The Kick-Off meeting shall include a review of the following items: Contractor Modification Program Schedule, including activities and milestones PWS requirements Contractor Data Requirements List (CDRL) Supply System Turn-in process Configuration management process Acceptance Test Procedure (ATP) (CDRL B001) System Safety process Program Risk Assessment 3.2.1.2 Meeting #2 The contractor shall conduct a meeting after Kick-Off, but prior to the beginning of the conversion effort. A date for the meeting shall be agreed upon by all parties during Kick-Off. Additionally, ATP (CDRL B001), shall be due prior to meeting #2, which shall include, at a minimum, reviews of the following items: Updated Contractor Modification Program Schedule (include start/completion date) Contractor Data Requirements List (CDRL), if revised Supply System Turn-in process Configuration management process review ATP (CDRL B001) discussion and finalization System Safety process review Page 5

W900KK-10-T-0043 Attachment 1 Program Risk Assessment review 3.2.1.3 Meeting #3 The Contractor shall conduct a meeting at the modification site in accordance with the Modification Program Schedule. The Contractor shall conduct a Test Readiness Review during meeting #3, which shall immediately precede acceptance testing with the Government. Meeting #3 shall include a thorough review of any test discrepancies reported during the contractor’s internal testing and the actions taken to correct those discrepancies. 3.3 Test and Evaluation The contractor shall utilize their Test and Evaluation (T&E) Program to ensure that the FuT fulfills its established requirements as set forth in this PWS. The contractor shall be responsible for the performance of all inspection and test requirements for the modification. The Government reserves the right to witness and/or perform any tests considered necessary to assure that no system degradation or incompatibility exists after the modification is incorporated. The contractor shall disclose all known discrepancies and support the Government and the ATS prime contractor in identification of modification deficiencies. The contractor shall establish a pre-modification baseline to document any pre-modification issues that may help to relieve any potential degradation claims. The Government shall certify proper operation of the FuT after modification. 3.3.1 Inspection and Acceptance Testing The Contractor shall utilize the Inspection & Acceptance Testing program to outline all inspection and acceptance activities to be conducted during modification acceptance. The Contractor shall present the System Test Plan to the Government for review at meeting #2. An ATP working group may be held in conjunction with meeting #2 to finalize the ATP. All requirements defined in this PWS shall be verified by the execution of the Government approved ATP (Appendix 1 can be used for the basis of the ATP) (CDRL B001). Final Acceptance Testing shall be conducted at Little Rock AFB, AR. The following conditions also apply: a. The Government may inspect all work at reasonable times and places. Contractor shall provide all information and assistance necessary for safe and convenient inspection. No such inspection shall relieve the Contractor of its obligation to furnish all work in accordance with the requirements of this contract. The Government final inspection and acceptance shall be accomplished at Little Rock AFB, AR. b. The Contractor shall provide the Government the right to witness, examine, test, measure, and evaluate all aspects of the modification during each test phase to assure its appropriate performance/operation. The Government may utilize the ATS prime contractor for these actions. 3.3.2 Closure Criteria Successful completion of the ATP (CDRL B001) and delivery of the Test/inspection Report (B002) and TDP (B003) will result in a declaration that the device is Ready For Training (RFT). 3.3.2.1 Test Discrepancies The Contractor shall work with the Government to identify modification deficiencies. The Contractor shall utilize a test discrepancy tracking system and shall correct any deficiency/degradation to the trainer

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W900KK-10-T-0043 Attachment 1 operation resulting from the modification activities. All test deficiencies shall be evaluated against the modification requirements. The Contractor shall provide the Government a Test/Inspection Report (CDRL B002) listing all test discrepancies and final resolution after successful completion of acceptance testing. 3.4 Quality Assurance/Quality Assurance Personnel (QAP) The government will evaluate the contractor’s performance by appointing a representative(s) to monitor performance to ensure services are received. The government representative will evaluate the contractor’s performance through intermittent on-site inspections of the contractor's quality control program and receipt of complaints from base personnel. The government may inspect each task as completed or increase the number of quality control inspections if deemed appropriate. Subsequent to contract award, the identity of the QAP(s), with a letter defining their duties and authority will be promptly furnished by the Contracting Officer to the successful contractor. The QAP(s) will inform the Contracting Officer when discrepancies occur. The QAP(s) shall not obligate the Government. 3.5 Packing and Crating The Contractor shall be responsible for fabricating crates to Government provided specifications as identified in the Special Packaging Instructions website (https://spires.wpafb.af.mil/sindex.cfm). The contractor shall provide shipping to CONUS locations as required by the government for items identified in the Designated Save Items List identified in Appendix 6 FuT SAVE Items List. 3.6 Safety The contractor shall provide a Safety Plan as part of the Program Management Plan (CDRL A003). 4.0 DELIVERABLES 4.1 Technical Data Package After contract award, the government will provide to the winning Contractor, Technical Orders essential in the development of the Technical Data Package. The Contractor shall develop and deliver a Technical Data Package (TDP) (CDRL B004) to include applicable drawings and schematics that have been modified as part of this conversion effort. Maximum use shall be made of existing Air Force provided Technical Orders. The Government will evaluate any Contractor-produced TDP to ensure technical adequacy and acceptability. 4.1.1 Warranty and Licenses The government retains unlimited rights to any and all deliverables developed under this effort. Contractor is notified that the end user of this product will be the United States Air Force (USAF) and its Air Mobility Command (AMC), Air Education Training Command (AETC), and as managed by Ogden Air Logistics Command (ALC)/GHMSA. All rights shall be transferable to the US Government, AMC, AETC, and Ogden ALC for continued operation and maintenance of this system. The Contractor shall provide a warranty on its portion of the FuT products and modifications for one year from the date of DD250 sign off. 4.2 Contractor Acquired Property The contractor shall purchase and deliver the following items:

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W900KK-10-T-0043 Attachment 1 1.

Propeller Dolly: Qty 1: Please provide the following support equipment or its Air Force Certified approved equivalent equipment. NSN 4920-00-167-0262; P/N: 34J6222-2, which is a C-130 propeller dolly used to transport the C-130 propeller. 100 In. Long; 79.88 In. Wide; 70.25 In. High; 0.5 TN Rated Cap.; Steel body 1 propeller accommodated 13.5 Ft Maximum Diameter W/O Tool Compartment; Wheel arrangement single axle, single wheel front and rear mount; Parking Brakes, Pin Coupler; W/O retractable support. Predominant material manufactured Steel.

2. Storage Containers: (various quantities); Please provide the following containers or its equivalent. STANLEY Vidmar or its equivalent, Qty; 1Ea., Cabinet P/N (PKL071510C000001) 60"W X 27 3/4"D X 59"H; Qty: 1 Ea, Cabinet P/N (PKL071510C-000002), 60"W X 27 3/4"D X 35"H; Qty; 2Ea., Cabinet P/N (PKL071510C-000003), 45"W X 27 3/4"D X 59"H; Qty; 2Ea., Cabinet P/N (PKL071510C-000005), 45"W X 27 3/4"D X 35"H; Qty: 1 Ea, Cabinet P/N (PKL071510C-000007); Qty; 1Ea.; Cabinet P/N (PKL071510C-000008), 30"W X 21 3/8"D X 35"H; Qty; 2Ea., Cabinet P/N (PKL071510C-000009), 45"W X 27 3/4"D X 37"H; Qty; 2Ea., Cabinet P/N (PKL071510C-000010), 60"W X 27 3/4"D X 37"H. 3. Inspection Lights: Qty 26: Please provide the following tools or its equivalent. Pelican M6 LED, Model #M6, P/N 2330-010-110; LED, Black, Batteries & Holster, water tight, equipment Protector Case. Black, Batteries & Holster, Clam Features: - Batteries Included: Yes - Bulb: LED, White - Burn Time: 4 Hours - Carry System: Holster - Finish: Black - Material: Aluminum - Output (lumens): 41 - Overall Length (inches): 5.51 - Packaging: Clamshell - Power Source: 2 x CR123 - Submersible: No - Switch: Push Button Constant On/Off or Momentary - Made In: United States. 4. High Boy Engine Trailer: Qty 2; Please provide the following support equipment or its Air Force Certified approved equivalent equipment. NSN: 1740-00-106-8512, P/N 200-000-101; MODEL 200-000-101 Quick Engine Change (QEC) Dolly is designed to support and transport the T56-A-1A, T56-A-7, AND T56-A-9 Turboprop aircraft engines during change in aircraft power packages, during storage, and for transportation of the engine; it is a towed vehicle incorporating hand lever operated cable controlled brakes, leveling jacks, and wheel covered splash fenders. 5. Digital Portable Radios: Qty, 3; Please provide the following support equipment or its equivalent. Motorola ASTRO XTS 5000, Model II Receiver Typical Performance Specifications, 700/800 MHz VH1 UHF R1 UHF R2, Frequency Range/Bandsplits. 4.3 Contract Data Requirements List (CDRL) The modification Data Item Descriptions (DIDs) in Table 4.4-1 includes the preliminary data items in support of the FuT #4. The Contractor shall use electronic media and shall deliver data in USAF standard office suite software when applicable. The Contractor shall deliver the following data items to the Government in accordance with the initial delivery and frequency outlined in Table 4.4-1. Distribution of these DIDs shall be determined after contract award. Table 4.3-1. Data Item Deliverables CDRL A001 A002 A003

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Data Deliverables Conference Agenda Conference Minutes Program Management Plan

DID (use as guide) DI-ADMN-81249A DI-ADMN-81250A DI-MGMT-80004A

Frequency As Required As Required As Required

W900KK-10-T-0043 Attachment 1 B001 B002 B003

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Acceptance Test Procedure (ATP) Test/Inspection Report Technical Data Package

DI-NDTI-80603A DI-NDTI-80809B DI-CMAN-80776

As Required As Required As Required

W900KK-10-T-0043 Attachment 1 APPENDIX #1 FUT FUNCTIONALITY REQUIREMENTS Using the Instructor Operators Station (IOS) panel [constructed by the contractor] and located in the Technical Order cabinet, will operate the Aerial Delivery System without the necessity of being on the on the flight deck (All flight deck switches shall retain their current functionality). Appendix #3 provides an example of the current FuT devices IOS and aft junction box. The IOS shall be configured so that it is interchangeable with the existing FuT IOS’s (see appendix 3). The functionality shall include; 1. The ADS switch opens and closes the Ramp and Door in the same manner as the switch on the ADS panel (Center Console). 2. The ADS Light illuminates when the Ramp and Door are in the full open position. 3. The Touchdown Relay switch allows the instructor to by-pass the relay to simulate flight. 4. The Red and Green “Jump/Caution Lights” switches operate the same as the Side Panel Switches. 5. The “Chute Release” push-button serves the same function as the center console button…bomb rack chute release. 6. The “Aux Pump” switch turns the Auxiliary Hydraulic Pump on or off. 7. An Night Vision Goggles compatible floodlight Additionally, two (2) switches shall be provided at the aft junction box; 1. One for operation of the Air-deflector doors. 2. One for operation of the Red and Green “Jump/Caution Lights”. The FuT fidelity shall be such that the following checklists shall be capable of being performed. All required equipment and systems shall be functional and operational. ** Note for Contractor - Items in light font should not be affected by the FuT conversion modification. PRIOR TO ENTRANCE 1. Nose landing gear pin -Installed 2. Ground wires -Installed 3. Chocks -In place 4. Armament placard APPLYING POWER This procedure checks only switches that many cause damage to the airplane if not in proper position during application of external power. All other switches should be in their normal power off position. POWER OFF INSPECTIONS Battery Compartment 1 AC EXT PWR CONTROL circuit breaker -Closed 2 DC EXT PWR CONTROL circuit breaker -Closed Cargo Compartment 1 Defensive system safety pins -Installed 2 Aft fuselage junction box circuit breakers -Checked 3 Ramp and door controls, valves and switches -6N, NEUTRAL, OFF

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Flight Station (Right Side) 1. Status of airplane a. AFTO Form 781A and K 2. Landing gear lever -Down 3. Hydraulic panel switches -Set a. AUX pump switch -OFF b. Anti-skid switch -ON c. Engine pump switches -ON d. Suction boost pump switches -OFF 4. Airdrop/Troop Jump computer-manual select -AD/TJ MAN switch NOTE Must be in AD/T J MANUAL to prevent depletion of the airplane battery. 5. Air deflectors switch -OFF ** - Jump Lights - Check 6. Copilot's circuit breaker panels -Checked a. Tachometer test switch -OFF b. Iron lung outlets -OFF Navigation Station 1. Radar altimeter -Off 2. Radar PWR function switch -OFF 3. IFF radar transponder (some airplanes) -OFF 4. SCNS control panel -Set a. SCNS power switch -OFF b. INU power switches -OFF c. GPS power switch -OFF d. DVS power switch -OFF 5. RWR-OFF 6. Nose radome anti-icing switches (some airplanes) -OFF 7. AN/ALE-40/AN/ALE-47 CONTROL panel GND TEST/EMER switch -NORMAL 8. AN/ALE-40 CCU arming switch -OFF 9. AN/AAR-47 power indicator/switch -OFF 10. AN/ALE-47 CDU mode switch -OFF 11. AN/ALQ-131 control indicators OFF ISTBYIOPR switches (some airplanes) -OFF 12. SCNS power bypass switch -OFF, safetied 13. Circuit breakers -Checked a. AN/ALE-40/AN/ALE-4 7 circuit breakers -As required b. AN/ALQ-131 circuit breakers -As required 14. Aerial reconnaissance weather officer's console -Set a. Check all switches -OFF/CLOSED 15. Test operation panel-GUARD DOWN

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W900KK-10-T-0043 Attachment 1 Crew Bunk/Galley Area 1. Upper main AC distribution panel circuit breakers -Checked WARNING Use extreme care when working in or around the FS-245 area. Electrical shock hazard exists because of uninsulated, high voltage wires. Flight Station (Left Side) 1. Pilot's circuit breaker panels -Checked a. Emergency INS battery bus tie switch -OFF, safetied 2. Air deflectors switch -OFF ** Jump Lights - Check 3. Air conditioning master switch -Off 4. Anti-icing panel-Set a. NESA windshield switches -OFF b. Nacelle preheat switches -OFF c. Propeller and engine anti-icing master switch -AUTO d. Pitot heat switches -OFF e. Engine inlet air duct anti-icing switches -OFF f. Propeller ice control switches -OFF g. Anti-icing wing and anti-icing empennage switches -OFF 5. Bleed Air Valve switches -Set a. Wing isolation valve switches -NORMAL b. Engine bleed air valve switches -CLOSED 6. External AC and DC power switches -OFF 7. Fuel panel -Set a. Dump pump switches -OFF, safetied; ~OFF b. ~Dump valve switches -NORMAL, safetied c. Fuel boost pump switches -OFF d. No. 2 crossfeed valve switch -OPEN, all others CLOSED 8. ADS ramp and door control switch -OFF Power Connection 1. Power cart -Positioned a. Position generator a minimum of 50 feet from airplane and fuel sources, and a minimum of 25 feet from fuel vents. 2. Power cable plug -Inspected a. Inspect pins in power cable plug for foreign objects and remove as required. 3. Power cable - Connected to receptacle 4. Power cart - On Power ON Inspection 1. Electrical panel -Set NOTE Ensure external power is OFF prior to performing electrical panel checks.

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W900KK-10-T-0043 Attachment 1 a. INS battery charge switch -OFF b. Generator switches -OFF c. Generator disconnect switches -OFF, safetied d. Inverter switches -OFF e. Airplane battery voltage -Checked f. External AC power light -On g. Check voltage and frequency (1) Check volts for A, B, and C phases are between 110 -125. (2) Checks freqs for A, B, and C phases are between 380 -420. h. External AC power switch -EXT AC PWR i. DC loadmeters -Checked (1) Ensure all four loadmeters are functional and indicating a load above zero. FLIGHT STATION 1. Status of airplane -Checked 2. ADS control panel ramp and door control switch -OFF 3. PA system main power switch -ON, speakers as required 4. Weight and balance data -Checked, on board CARGO COMPARTMENT (GENERAL) 1. AFTO Form 46/Emergency equipment -Checked and secured 2. Oxygen -Checked 3. Cargo floor -Checked 4. Dual rail pip pins -Checked (11 each) 5. Dual rail system/core bolts/ critical attachment bolts, roller conveyors -Checked, installed CARGO COMPARTMENT (LEFT SIDE) 1. Emergency exit light -Checked, ARM, safe tied 2. Escape ladder -Checked, secured 3. Tiedown devices/straps -Checked, secured 4. Forward seats and seat belts -Check condition, installed, as required 5. Defensive system safety pins -Installed 6. Wheel well seats and seat belts -Check condition, if installed 7. Static-line retriever cable clips -Check condition, as required 8. Fire extinguisher -Checked, secured 9. Center seat support extensions -Stowed (FS 617) 10. Wheel well seat supports -Checked, secured 11. Center seat support beams -Checked, secured 12. Seats and seat belts -Check condition, installed as required 13. Defensive system safety pins -Installed 14. Emergency exit light -Checked, ARM, safetied 15. Left paratroop door master door warning light shutoff switch NORMAL, safe tied 16. Pistol grip remote dispenser switch -Checked, stowed 17. Paratroop door and warning light -Check for operation 18. Oxygen regulator -Checked, 100%, OFF (if not in use) 19. Tiedown container -Checked for proper contents, secured

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W900KK-10-T-0043 Attachment 1 20. Ramp and door controls, manual control valves, and switches NEUTRAL, 6N, OFF, handle secured 21. Latrine facilities -Checked for cleanliness, serviceable 22. Tiedown devices -Checked, secured 23. Anchor cable center support and pins -Checked, as required 24. Left and right paratroop jump platforms -Stowed, serviceable, secured 25. Auxiliary hydraulic system -Checked for leaks, reservoir level 26. Ramp locks and ADS arm -Engaged, connected/secured 27. Liquid containers (if installed) -Checked, secured 28. Litter stanchion -Checked, secured 29. Anchor cable reels -Checked, secured 30. Anchor cable aft support -Checked 31. Emergency exit light -Checked, ARM, safetied 32. Aft overhead escape hatch and rope -Installed, locking pin removed 33. Ground loading ramps -Checked, serviceable, secured 34. Door storage compartments -Checked for proper contents, secured 35. Static-line extension Y-cables/ Towed Parachutist Retrieval System (TPRS) -Checked, as required 36. Cargo door locks -Engaged 37. Cargo door uplock -Unlocked CARGO COMPARTMENT (RIGHT SIDE) 1. Tiedown devices -Checked, secured 2. Anchor cable aft support -Checked 3. Anchor cable reels -Checked, secured 4. Litter stanchion -Checked, secured 5. Liquid containers (if installed) -Checked, secured 6. Tiedown containers -Checked for proper contents, secured 7. Waste container -Checked, clean, secured 8. Ramp locks and ADS arm -Engaged, connected/secured 9. Fire extinguisher and hand ax -Checked, secured 10. Latrine facilities -Checked for cleanliness, serviceable 11. Tiedown devices -Checked, secured 12. Tiedown containers -Checked for proper contents, secured 13. Truck loading ramps -Checked, secured 14. Anchor cable center support braces -Check for pins, proper stowage 15. Anchor cable center support and pins -Checked, as required 16. Oxygen regulator-Checked, 100%, OFF (if not in use) 17. Life raft release handles -Checked, safetied 18. Right paratroop door, ramp and door master door warning light shutoff switches NORMAL, safetied 19. Paratroop door and warning light -Checked for operation 20. Emergency exit light -Checked, ARM, safetied 21. Pistol grip remote dispenser switch -Checked, stowed 22. Center seat support beams -Checked, secured 23. Wheel well seat supports -Checked, secured

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W900KK-10-T-0043 Attachment 1 24. Paratroop retrieval bar -Checked, secured 25. Seats and seat belts -Check condition, installed as required 26. Emergency exit light (center overhead hatch) Checked, ARM, safetied 27. Arm emergency exit light if escape ladder is installed or an overwater leg is to be accomplished. 28. Center overhead escape hatch and rope -Installed, locking pin removed 29. Oxygen bottle and smoke/quick-don mask -Checked, serviced, smoke mask attached to or near bottle, hose disconnected/quick-don hose connected, harness checked, quick-don purge pin 30. Static-line retriever cable clips -Check condition 31. Wheel well seats and seat belts -Check condition, if installed 32. Defensive system safety pins -Installed 33. Forward seats and seat belts -Check condition, installed as required 34. Emergency exit light -Checked, ARM, safe tied 35. Side emergency exit -Checked, unobstructed, secured, safetied 36. Center seat back support beams -Checked, secured 37. Oxygen regulators -Checked, 100%, OFF 38. Oxygen bottle and smoke/quick-don mask -Checked, serviced, smoke mask attached to or near bottle, hose disconnected/quick-don hose connected, harness checked, quick don purge pin 39. Defensive system safety pins -Installed 40. Internal portable winch snatch block(s) -Checked 41. Seat and litter stanchions -Checked, secured 42. Tiedown devices -Checked, secured 43. Fire extinguisher and hand ax -Checked, secured 44. Urinal facilities -Checked for cleanliness, serviceable POWER ON 1. Forward auxiliary control panel -Checked 2. Cargo winch (if installed) -Check operation, serviceable as required, secured 3. Aft fuselage junction box panel -Checked 4. Cargo ramp and door and warning lights -Check for proper operation 5. Aft right interphone cord -Checked 6. FWD right interphone cord -Checked 7. Galley -Checked, OFF BEFORE TAXI 1. Crew entrance door -Closed, locked BEFORE LEAVING AIRPLANE 1. Airplane and equipment -Cleaned, stowed, secured 2. Cargo ramp and door -Closed, ADS arms connected 3. Cargo compartment emergency exit lights switch -OFF 4. Cargo compartment oxygen regulators -Off 5. Pendulum release pivot arm cover -Installed 6. Cargo floor restraint rail detent latches -Extended 7. Electrical panel switches -Set 8. Emergency exit light off button -Pressed

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W900KK-10-T-0043 Attachment 1 9. Power cart -Off CARGO DOOR AND RAMP OPERATION WARNING The ADS control panel ramp and door control switch must be set to OFF and the ramp manual control knob, above the ramp control panel must be set at the 6N (neutral) position before operating the pump switch on the ramp control panel. CAUTION Wait at least 10 seconds after the auxiliary hydraulic pump is turned OFF, to allow the accumulator to discharge before turning the pump switch back on. Failure to do this will overload the motor and open the pump circuit breakers. With the pump switch set to ON the cargo door is opened by holding the cargo door control switch in the OPEN position until the door is fully opened and retained by the uplock; the ramp then is moved to the desired position by holding the ramp control switch at LOWER. NOTE The ramp can be stopped at any position by releasing the ramp control switch. The cargo door will free fall back to the closed position if the door control switch is released prior to the moment the door reaches the up-and-locked position. The ramp is closed by holding the ramp control switch in the RAISE position until the ramp is up and locked. CAUTION Prior to raising the ramp, ensure that locks are retracted and the ramp seal area is clear. NOTE When being raised the ramp call be stopped in any position by releasing the ramp control switch. On E airplanes prior to AF72-1288 H and 3> airplanes the door is closed by holding the cargo door switch to the OPEN position and pulling the cargo door manual release until the uplock is released. After the uplock is released allow the cargo door to free fall to the closed position. If door does not lock, hold the cargo door switch to the CLOSE position until the door is closed and locked.

Manual Operation of Cargo Door and Ramp with Handpump Pressure OPENING CARGO DOOR AND RAMP To open the cargo door and lower the ramp by use of the handpump: WARNING Before manual handpump operation, check that the AUX hydraulic pump switches on the flight station and the ramp control panel are in the OFF position.

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W900KK-10-T-0043 Attachment 1 1. Move the cargo door manual control valve handle to OPEN and operate the handpump until the door is up and locked. 2. Move the cargo door manual control valve handle to the NEUT (center) position. 3. Move the ramp manual control knob to the NO. I (unlock) position: operate the handpump until the handpump pressure indicator on the ramp control panel shows 3,000 PSI and all the ramp locks are visibly disengaged. 4. Move the ramp manual control knob to the NO. 2 (lower) position. Operate the handpump until the ramp is lowered. 5. Move the ramp manual control knob to the 3N (neutral) position. CLOSING CARGO DOOR AND RAMP To close the cargo door and raise the ramp by using the handpump, proceed as follows: WARNING Before manual handpump operation, check that the AUX hydraulic pump switches on the flight station and the ramp control panel arc in the OFF position. 1. Check that the pump switch on the ramp control panel is at the OFF position. 2. Move the ramp manual control knob to the NO.4 (raise) position and operate the handpump until the ramp is fully closed. 3. Move the ramp manual control knob to the NO.5 (lock) position. Operate the handpump until the handpump pressure indicator registers 3.000 PSI and all ramp locks are visibly engaged. 4. Move the ramp manual control knob to 6N (neutral).and leave it in that position. 5. Move the cargo door manual control valve handle to OPEN position. Operate the handpump until the pressure indicator reads a minimum of 500 PSI, pull the aft cargo door uplock manual release to the unlock position and move the manual control valve to NEUT. Door will free fall 6. Move the cargo door manual control valve handle to CLOSE, and operate the hand pump until the door is locked. 7. Move the cargo door manual control valve handle to the NEUT (center) position. The handle does not have a positive stop at the NEUT (center) position. so it should be checked to ensure that is has not been inadvertently moved beyond this setting. Operation of Cargo Door and Ramp from Flight Station 1. Depressurize the airplane. 2. Operate the auxiliary hydraulic system electric-driven pump by placing the pump switch. on the hydraulic system control panel, in the ON position. Check the system pressure. ** Bypass Touchdown Relay with IOS. 3. Move the ramp and door control switch on the ADS panel to the OPEN position. 4. When the ramp and door open light and the master door warning light illuminate, move the ramp and door control switch to the OFF position. 5. When the loadmaster signals that the cargo is dropped and the ramp and door area is clear, move the ramp and door control switch to OPEN then CLOSE position. 6. When the ramp and door open light and the master door warning light go off, move the ramp and door control switch to the OFF position. 7. Turn auxiliary hydraulic pump OFF.

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W900KK-10-T-0043 Attachment 1 ** Repeat 1 – 7 utilizing IOS controls in lieu of Flight Station controls. AIRLAND CARGO HANDLING SYSTEM PREFLIGHT 1. Left and right control handles -Repositioned a. LH SIMUL handle to AFT RESTRAINT RELEASE then to SIMULTANEOUS position. b. RH EMERG REL handle to EMER then to LOAD position. 2. Left and right detents Retracted 3. Left control handles Repositioned a. LH SIMUL handle retuned to STOWED position, stowage pin installed. b. Sequentially unlock all left detent latched in sequence, drum counter opposite ALL OPEN, stow handle with LOCK position on knob facing up, 4, Critical attachment bolts and roller conveyors -. Checked a, Critical attachment bolts -Physically checked b. Attachment bolts visually inspected c. Roller conveyors –installed/secure 5, Left and right ramp release handles Checked a. Engage detents and flanges b, Pull release handles to fh1l forward position, ensure detent and flanges fully retract. c, Release handles stowed, stowage pins installed. 6. Discrepancies Entered into AFTO Fom1 781 A PALLETIZED AIRDROP CARGO HANDLING I SYSTEM PREFLIGHT 1. Left control handles -Checked a. LH SIMUL handle down, stowage pin installed. b. SEQ LOCK handle, check that drum counter is opposite number 11 position and the handle is stowed with LOCK position on knob facing up. 2. Right-hand master control handle and crossover linkage -Connected a. Move RH EMERG REI handle to CHECK, ensure handle will stay in CHECK, move to NORMAL. 3. Left rails --Checked a. Proceeding aft, check the following: (1) Cargo compartment inboard attachment bolts and washers installed. (2) Draw bars connected and sleeves secured in full forward position. (3) Detent latches will not depress into rail, detent restraint arm parallel to detent body, no yellow showing on actuator arm, and emergency release arms connected to SIMUL control rods. (4) A-30 critical attachment bolt and washer installed. Right Rails --Checked a. Proceeding forward, check the following: (1) G-30 critical attachment bolt and washer installed. (2) Cargo compartment inboard attachment bolts and washers installed. (3) Detent latches will not depress into rail, release spacer between roller, alignment mark satisfactory, lock out pins stowed, lock tension at minimum settings, horizontal oval point screw installed, slippage mark satisfactory, and vertical set screw installed. (4) Draw bars connected and sleeves secured in full forward position. Left and right control handles Positioned 5. Left and right control handles -Positioned

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W900KK-10-T-0043 Attachment 1 a. LH SIMUL handle to AFT RESTRAINT RELEASE. b. RH EMERG REL handle to EMERG 6, Left and right detents -Checked a, Check for freedom of aft movement. 7, Left and right control handles Repositioned a. LH SIMUL handle to SIMULTANEOUS, b. RH EMERG REI, handle to LOAD, 8, Left and right detents and guard assembly doors Retracted/closed, as required 9, Left control handles Checked a. LH SIMUL handle returned to STOWED position, stowage pin installed, b, Sequentially unlock all left detent latches, drum counter opposite ALL OPEN, stow handle with LOCK position on knob facing up. 10. Cargo compartment and ramp intermediate roller conveyors '.'. Checked, secure, serviceable 11. Discrepancies Entered in AFTO FORM 781 A CARGO LOADING PREPARATION 1, Manifest/load plan Checked 2. Cargo inspection -Completed 3, Pallet and net conditions Checked 4. Pallet/vehicle safety aisles Checked, verified 5, Soil contamination and pest Checked 6, Mounted equipment/cargo -Secured to carrier or Vehicle 7, Engines and brakes Checked, if applicable 8, Fuel levels Checked, if applicable 9, Fuel, battery, and oil caps Tightened 10. Tanker-type vehicles Checked 11. Contact area pressures Computed 12. Hazardous materials Checked, properly documented 13 , Ramp support/ramp –Installed/positioned as required 14, Cargo loading preparation checklist-Completed CARGO LOADING (PALLETIZED/FLOOR LOAD) 1. Cargo loading preparation check list Completed 2. Left-hand and right-hand locks and vertical restraint flanges Retracted, as required 3. Cargo compartment and ramp 110m area -Cleared and unobstructed 4. Load inspection ·-Completed 5. Loading team duties -Assigned, briefed 6. Vehicle chocks Positioned 7. Auxiliary truck loading ramps -Installed, as required 8. Loading chocks -Installed, (for bare tine loading only) 9. Vehicle Positioned, adjusted 10. Brakes Set 11. Bridge plates Installed, as required 12. Pallet(s)/platform(s)/cargo -Loaded 13. Dual rail detent latches/tiedown Engaged/installed 14. Remaining pallet (s}/platform(s)/cargo Loaded

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W900KK-10-T-0043 Attachment 1 15. Floor retractable flanges -Engaged, as required 16. Ramp pallet, detent latches, and retractable flanges -Loaded, engaged, as required 17. Loading vehicle ---Released 18. Tiedown Computed, installed, checked 19. Cargo loading (palletized/floor loaded) checklist - complete WINCHING CHECKLIST 1. Winch --Positioned 2. Power cable (portable winch only) Connected 3. Winch condition Checked 4. Winch oil level (portable winch only) Checked 5. Control pendant power cable not in path of cargo (HCU-9/A only) IC] --Checked 6. Operational checkout Completed 7. Winch cable condition Checked 8. Loading team duties Assigned, briefed 9. Cargo compartment and ramp floor area .. Clear 10. Steering yoke _. Installed, if required 11. Auxiliary loading ramp/bridge plates Installed/positioned, if required 12. Vehicle chocks -Positioned 13. Winching vehicle (external/self winching) 14. Cargo/vehicle to be loader – Positioned 15. Cable attached – completed 16. Cable slack removed, snatch block and cable attachment – Completed, as required 17. Ratchet brake release lever (Bulldog) – Up position 18. Vehicle/cargo – Loaded, positioned, transmission set 19. Tiedown – Computed, installed, checked 20. Winching checklist – Completed VEHICLE LOADING 1. Cargo loading preparation checklist -Completed 2. Auxiliary loading ramps/bridge plates aligned for proper axle width Checked 3. Ventilation Checked 4. Loading team duties Assigned, briefed 5. Vehicles to be loaded/prime mover Aligned, low gear, if applicable 6. Vehicles Loaded, parked, transmission set 7. Parking brakes and ignition --Set, off 8. Tiedown Computed, installed, checked 9. Vehicle Loading Checklist --Completed PALLETIZED/CARGO/VEHICLE OFFLOADING 1. Offloading team duties. Assigned, briefed 2. Ramp support/bridge plates/auxiliary truck loading ramps/auxiliary ground loading ramps Installed/positioned, if required 3. Vehicle chock -Positioned, as required 4. Offloading vehicle/equipment Positioned 5. Ventilation As required

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W900KK-10-T-0043 Attachment 1 6. Winch -Positioned, secured and attached to load, as required 7. Vehicle/cargo Restraints, removed 8. Cargo compartment and ramp floor area Cleared 9. Cargo ramp right-hand and left-hand detent latches Unlocked, if applicable 10. Cargo compartment vertical restraint flanges Retracted, as required 11. Cargo compartment right-hand and left-hand detent latches Unlocked, if applicable 12. Off1oad Completed 13. Offloading vehicle(s) --Released 14. Palletized/cargo/vehicle offloading checklist Completed PASSENGER ONLOADING/OFFLOADING 1. Cargo compartment and ramp floor area Clear 2, Ramp and door/crew entrance door -Positioned/opened 3, Passengers -Boarded/deplaned 4, Seat belts - As required 5, Manifest Checked 6, Passenger briefing --Completed 7, Baggage/loose equipment –Secured/offloaded 8, Passenger onloading/offloading checklist-Completed GENERAL AIRCRAFT PREPARATION FOR AIRDROP CHECKLIST 1. Litter stanchion brackets -Positioned (as required) 2. Static-line retriever (forward control) Checked, if required 3. CDS arming switches -Safetied/checked, dearmed, 4. Anchor cable Support arms (forward controls) --Checked, if required 5. Anchor cables, fittings, and U-bolts-Installed and checked (as required) 6. Seat/seat support beams Secured/removed 7. Anchor cable support arms (aft controls) Checked, if required 8. Aft auxiliary control panel -Checked 9. Anchor cable stowage brackets -Rotated, secured (as required) 10. Litter stanchion brackets -Taped (as required) 11. Engine exhaust covers -Secured forward of load 12. Anchor cable reels Secured/removed 13. Aft cargo door contents --checked 14. Urinal steps, toilet assembly, modesty curtains, cargo net stowage boxes, and trash containers Stowed and secured Type III nylon cord 15. Vertical restraint flanges and ramp locks - Retracted and secured 16. Pendulum release pivot arm cover -Removed, stowed (as required) 17. Pendulum release system Checked (if required) 18. Tiedown tab 30D -Checked (if required) 19. Anchor cable stops -Positioned and taped (as required) 20. Roller conveyors Secured/removed and stowed (as required) 21. Cargo door and ramp - Opened to ADS position 22. General aircraft preparation for airdrop checklist Completed AIRCRAFT PREPARATION FOR PARATROOP AIRDROP

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W900KK-10-T-0043 Attachment 1 1. General aircraft preparation for airdrop checklist Completed, if required 2, Restraint rail sections 5B and 6B -Removed, stowed (if required) 3, Seats and safety belts –Checked 4. Center anchor cable supports Installed, checked (if required) 5, Static-line retriever extensions, V-cables. TPRS Checked (as required) 6, Paratroop retrieval bar (some aircraft) Positioned, secured 7. Jump platforms and door area - Inspected, installed, checked (if required) 8, Aircraft exterior inspection –Completed 9. Passenger onloading/offloading checklist -Completed 10, Cargo loading (palletized/floor load) checklist -Completed (as required) 11, Aircraft preparation for paratroop airdrop checklist. Completed AIRCRAFT PREPERATION FOR EQUIPMENT AIRDROP PRIOR TO LOADING 1. General aircraft preparation for airdrop checklist - Completed 2. Left rail lock inspection covers taped open Completed 3. Right-hand master control handle - Normal position 4. Right rail detents -Pinned-out, as required 5. Iron lung switch -On, as required 6. EPJS control box -Installed/connected and secured, as required 7. EPJS Y· connector(s) and mounting box(es) Installed and secured, as required 8. EPJS main cable Installed and secured, as required 9. EPJS interconnect cable(s) -Installed and secured, as required 10. Right-hand master control handle Load position 11. Load acceptance inspection Completed 12. Cargo loading (palletized/floor loading) checklist --Completed AFTER LOADING 1. Left rail detents -Engaged, checked 2. Right rail detents Engaged, set 3. Vertical restraint flanges -Engaged, as required 4, EFTC actuators Installed 5. Extraction system --Installed, checked 6. EPJS platform cable (s) - Installed, as required 7, EPJS squib cable(s) Installed, as required 8. EPJS continuity check -Completed, as required 9. Emergency restraint chains --Positioned 10. Load inspection Accomplished 11. Aircraft preparation for equipment airdrop checklist -Completed AIRCRAFT PREPARATION FOR CONTAINER DELIVERY SYSTEM (CDS) AIRDROP PRIOR TO LOADING 1. General aircraft preparation for airdrop Checklist Completed 2. Seat support beam(s) - Removed (as required)

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W900KK-10-T-0043 Attachment 1 3. Buffer stop assembly/alternate forward barrier Installed 4. Center vertical restraint (CVR) Installed (as required) 5. Detents beside and aft of load Retracted and pinned-out (as required) 6. Pulley assembly Installed 7. Retriever winch cable loop Installed (as required) 8. Load Acceptance Inspection –Completed 9. Cargo loading (palletized/f1oor load) checklist Completed AFTER LOADING 1. Container rigging 2. Tiedown restraint --Installed and checked (if required) 3. Load inspection –Accomplished 4 Aircraft preparation for container delivery system (CDS) airdrop checklist Completed AIRCRAFT PREPARATION FOR COMBAT RUBBER RAIDING CRAFT (CRRC) AIRDROP 1. General aircraft preparation for airdrop checklist/aircraft preparation For paratroop airdrop checklists 2. Left and right detents - Retracted and pinned out, as required 3. Retriever winch cable loop -Installed 4, Load acceptance inspection Completed 5, Cargo loading (palletized/floor load) checklist -Completed AFTER LOADING 1. CRRC platform(s) Positioned 2. Pulley assembly Installed 3. Type VIII nylon release gate Installed 4. Static-line retriever cable --Attached to guillotine knife 5. Static-lines attached to anchor cable Completed 6. Forward barrier - Installed 7. Tiedown restraint Installed and checked 8, Load inspection – Accomplished 9. Aircraft preparation for combat rubber raiding craft (CRRC) air drop Completed AIRCRAFT PREPARATION FOR HIGH SPEED LOW LEVEL AERIAL DELIVERY SYSTEM (HSLLADS) AIRDROP 1. General aircraft preparation for airdrop checklist Completed 2. Sling ejection delivery system (SEDS) Checked 3. Load acceptance - inspection -Completed 4, Cargo loading (palletized/floor load) checklist -Completed AFTER LOADING 1. Container(s) Positioned 2. Multiple container belly band (if applicable) 3. Sling ejection delivery system (SEDS) 4, Sling retention lines Attached 5, Release assembly –Attached 6. Electrical cable -Connected

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W900KK-10-T-0043 Attachment 1 7, Static-line(s) –Attached 8. Load inspection Accomplished 9. Sling Disconnected 10. Tiedown restraint · Installed 11. Aircraft preparation for high speed low level aerial delivery system (HSLLADS) airdrop checklist Completed AIRCRAFT PREPARATION FOR CONTAINER RELEASE SYSTEM (CRS) AIRDROP PRIOR TO LOADING 1. General aircraft preparation for airdrop checklist -Completed 2. Release assembly - Checked 3. Load acceptance inspection Completed 4, Cargo loading (palletized/floor load) checklist Completed AFTER LOADING 1. Container(s) Positioned 2. Multiple container belly band (if applicable) - Installed 3. Release assembly Attached 4. Forward restrain/tension strap Installed 5. Electrical cable Connected 6. Static-line(s) Attached 7. Load inspection -Accomplished 8. Tiedown restraint -installed 9. Aircraft preparation for container release system (CRS) airdrop checklist Completed ABFDS CREW EMERGENCY JETTISONING PROCEDURES 1. Notify Pilot Notified LM 2. OXYGEN ON/l00% ALL 3. Pressurization Emergency Depressurize FE 4. DESCENT As required p 5. Forward and aft tank valves closed. 25-foot vent hose disconnected from forward vent fitting and stowed under aft lank straps. Fuel Specialist/LM 6. 20-fool hose, disconnected from vent at FS 642 and stowed under aft tank straps. Fuel Specialist/LM 7. 28-foot and 8-fool hose disconnected at FWD and AFT tank valves and capped. Stow the above hose on the pump modules and secure with one 5,000 pound strap for jettisoning. Fuel Specialist/LM 8. Cargo ramp and door -Clear to Open/OPEN and locked LM 9. Left and right ramp lock release handles Pulled LM 10. Loadmaster informs pilot Clear to jettison pump modules. Pilot will establish a slight nose high attitude to jettison modules. LM,P 11. Vertical restraint flanges -Released/retracted LM 12. All tank restraint straps Clear LM 13. All personnel forward of load LM 14. Loadmaster informs pilot ready to jettison LM 15. Pilot will establish an approximate IO-degree nose high attitude to assist in jettisoning.

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W900KK-10-T-0043 Attachment 1 16. Upon the pilot's command "JETTISON " the LM immediately positions RH EMERG REL handles to EMERG and LH SIMUL handle to aft restraint removed position. 17. Pilot notified of load – Load clear/or condition

END OF APPENDIX # 1

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APPENDIX #2 FUT GOVERNMENT FURNISHED PROPERTY (GFP)

The following is a list of Government furnished support equipment provided for this requirement. AGE Support Equipment a. b. c. d.

e. f. g. h.

-86 Hobart Generator (1 Ea.) Lo-Paks (up to a maximum 5 Ea.) FL1D Light Carts (up to a maximum of 5 Ea.) Maintenance Stands a. B-4 (2 Ea.) b. B-5 (2 Ea.) c. B-1 (2 Ea.) d. C-1 (2 Ea.) Hydraulic Mule (1 Ea.) Browsers (2 Ea.) Fuel Foam Carts (2 Ea.) Flight Control Surfaces Dollies (1 Ea.)

C-130E Aircraft 63-7784. Flight Line location as directed by the Government. Aircraft Technical Orders (TO), these TO’s shall be utilized by the awarded contractor to generate the Technical Data Package (CDRL B004).

END OF APPENDIX # 2

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W900KK-10-T-0043 Attachment 1 APPENDIX #3 INSTRUCTOR OPERATOR STATION EXAMPLE

5.25” H; 5.25” D; 7” W

An NVG compatible flood lamp/light Instructor Operation Station (IOS) pictured above. Pictured will Below is the Aft Junction Box. illuminate the IOS Station The Aft Fuselage Junction Box requires adding a Jump/Caution Lights switch, beside the Air Deflector Switch. There is approximately 70 feet from the IOS to the Aft Fuselage Junction Box.

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ADS panel that the IOS is wired to. There is approximately 30 feet from the IOS to the ADS panel located on the Center Control Pedestal.

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Jump Lights Panel that the IOS is wired to. There is approximately 30 feet from the IOS to the Jump Lights panel located on the Pilot and Co-Pilot Side Panel.

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The Male Connector attached to the IOS Control Box.

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APPENDIX #4 C-130 ATS FUT FIDELITY REQUIREMENTS DEFINITIONS Failure - A failure is defined as any C-130 FuT malfunction which results in the loss or delay of scheduled training. Functional - Shall be identical to the C-130 aircraft or in accordance with delivered drawings and shall include all associated aircraft hardware in accordance with C-130 technical data and technical orders. Functional Non-Operational - Shall be identical to C-130 aircraft but related system(s) does not have to function or be operational. Must, twist, switch, etc. but not operate or manipulate a system. Operational - Shall be identical in operation to the C-130 aircraft. An Instructor Operators Station (IOS) panel, located at the TO cabinet, shall be installed to allow Aerial Delivery System (ADS) and Jump/Caution Light operations without the necessity of being in the cockpit (All cockpit switches shall retain their current functionality). Appendix #3 provides an example of the current FuT devices IOS. The functionality shall include; 1. The ADS switch opens and closes the Ramp and Door in the same manner as the switch on the ADS panel (Center Console). 2. The ADS Light illuminates when the Ramp and Door are in the full open position. 3. The Touchdown Relay switch allows the instructor to by-pass the relay to simulate flight. 4. The Red and Green “Jump/Caution Lights” switches operate the same as the Side Panel Switches. 5. The “Chute Release” push-button serves the same function as the center console button…bomb rack chute release. 6. The “Aux Pump” switch turns the Auxiliary Hydraulic Pump on or off. 7. An NVG compatible floodlight Additionally, two (2) switches shall be provided at the aft junction box; 1. One for operation of the Air-deflector doors. 2. One for operation of the Red and Green “Jump/Caution Lights”. The following is a list of aircraft equipment the contractor shall be responsible for providing the initial inspection, diagnostic and reassembly, to convert the FuT as a learning device to meet the PWS requirement based on the indicated state of fidelity: Exterior AC Exterior Power Receptacle - Operational Flight Deck - Pilot's Station Pilot's left side console (PA/interphone switch, hand held microphone) - Operational Flight Deck - Copilot Station Auxiliary Hydraulic System panel - Operational Functional Copilot's right side console (inter-phone panel, handheld microphone) - Operational Flight Deck - Center Console Copilots ADS panel - Operational ADS Chute Release – Functional Flight Deck - Overhead Center Console (top)

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W900KK-10-T-0043 Attachment 1 Emergency exit light switch - Functional Operational Ceiling PA speaker and switch - Functional Inter-phone panel - Functional Electrical control panel top row - Functional Battery switch - Functional Non-Operational Bus tie switch - Operational External power switch - Functional Fuel panel - Functional Non-Operational Flight Engineer and Navigator Seats and safety belts – Functional Circuit breaker panel - Modified Functional (Some must be operational for FuT Operations. Rest should be pulled and strapped.) Flight Deck - Navigator Station Inter-phone Panel - Functional Operational Seat and safety belts - Functional Oxygen regulators - Functional Non-Operational Flight Deck - Other Forward escape hatch - Functional Wing life raft T-handles - Functional Non-Operational All oxygen regulators - Functional Non-Operational Crew oxygen recharger hoses - Functional Non-Operational Cargo Compartment - Bulkhead Crew galley (oven/CB/light/hot cup receptacle/ coffee jug receptacle) - Operational Crew galley (refrigerator door and bottom drawer) - Functional Non-Operational Cargo winch (attachment points/pendent/oil level/cable) - Functional Crew oxygen re-charge hoses (3) - Functional Non-Operational Instructor loadmaster station - Functional Operational Cargo Compartment - Left Side (Fwd to Aft) Crew entrance door - Operational Forward PA/Inter-phone panel and cord - Functional Cargo compartment dome light switches - Functional Left troop door jump signal lights - Functional Left troop door ADS control panel - Functional Left troop door PA/Interphone panel and cord - Functional Hydraulic system manual override selector valve system Functional Aft jump signal lights - Functional Aft anchor line arm switch - Functional Aft anchor cable support - Functional Cargo Compartment - Right Side (Aft to Fwd) Aft anchor cable actuator - Functional Aft jump signal lights - Functional Right troop door jump signal lights - Functional Right troop door PA/Interphone panel and cord - Functional

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W900KK-10-T-0043 Attachment 1 Auxiliary Hydraulic system pump and all associated plumbing, fittings and filters Functional Cargo Compartment - Right Side (Aft to Fwd) Cargo compartment dimming switches - Functional Oxygen manual shutoff valve - Functional Non-Operational Oxygen regulators - Functional Non-Operational Cargo Compartment - Other Oxygen recharge hoses (2) - Functional Non-Operational All cargo compartment and ramp loading lights - Functional Escape ropes and ladders - Functional Ramp and cargo door - Functional All emergency exit lights - Functional Warning bells - Functional PA speakers - Functional Restraint rails, left and right - Functional Cargo compartment and ramp roller conveyors - Functional 12 each litter stanchions - Functional Snatch blocks - Functional Anchor cable attachment points - Functional Wing life raft T-handles - Functional Non-Operational Side emergency escape hatches/interior handles - Functional Emergency escape overhead hatches/interior releases Functional Escape ropes - Functional Auxiliary ground loading ramps - Functional Strap stowage boxes - Functional Chain storage boxes - Functional Cargo floor (good general condition) - Functional Pendulum release assembly (bomb rack) - Functional Anchor cables - Functional Cargo Compartment - Other Aerial delivery system - Functional Static line retriever winches - Functional Aft retriever winch remote control assembly - Functional Scanners cord - Functional Protective clothing kit - Functional Non-Operational Miscellaneous Emergency hand ax (2) - Functional Crew entrance door - Functional Flight Station ladder - Functional Restraint rail end bumpers - Functional Door open lights - Functional Aft anchor cable supports/motors - Functional Air deflector doors – Functional

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W900KK-10-T-0043 Attachment 1 END OF APPENDIX # 4 APPENDIX #5 FUT DRAWINGS, PHOTO’S Legend: "A"-Blue = Require Removal and Shipment, Blue Lined (///) = Sub-Components Require Removal and Shipment "B"-Red/Green = Require Shipment [Currently Removed] "C"-Orange = Wing Section To Be Cut "D"-Yellow = FuT Completed Project

Dorsal Fin Assembly “A”

Wing Section “C” To Be Cut

3A. Outer Wing Dry)………………………………………………………………....……………..3962 LB 4B. Aileron………………………………………………………………………………………….190 LB 5B. Outer Wing Flap…………….………………………………………………………………….217 LB 6B. Center Section Flap…………………….…..…………………………………………………..119 LB 7A. Horizontal Stabilizer Assembly……………………..…………………………………………2589 LB 8B. Elevator (Inboard Counterweight Removed)…………………………………………………...218 LB 9A. Vertical Stabilizer……………………………….……………………………………………..869 LB 10B. Rudder (Not Including Balance)…………………………….………………………………..193 LB 11A. Tail Cone……………………………………………………………………………………..72 LB 12D. Main Gear Wheel (Complete With Tire And Tube)…............................................................365 LB 13D. Main Gear Wheel (One Gear Complete With Wheel, Tire, And Brake)…………………….825 LB 14D. Nose Landing Gear……….………………………………………………………………………….….573 LB

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18A. Radome………………………………………………………………………………………200 LB 19D. Cargo Ramp…………..…………………………………………………………….……….1,109 LB 20D. Aft Cargo Door………………………………………………..…………………………….731 LB *NOTE: Weights are approximate


The top photo shows an example of a the beef-up beam, and the bottom photo shows how the beefup beam is attached on the tail section after the tail sectin is removed. Page 39


The picture above show an example of a combination beef-up beam/cover plate above the ramp and cargo door after the tail section is removed. END OF APPENDIX # 5

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W900KK-10-T-0043 Attachment 1 APPENDIX #6 FUT DESIGNATED SAVE ITEMS LIST a. DESIGNATED SAVE ITEMS LIST FOR FuT #4 DISPOSITION *These parts require shipment (CONUS) as identified in the PWS and Attachment 5. #'s 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35

Component O/B Flap O/B Flap Vertical Horz Tip I/B Nacell Upper Access Pnl Assy O/B Wing Leading Edge Horz Stab Lt Leading Edge O/B Wing Leading Edge O/B Wing Leading Edge O/B Wing Leading Edge Wing Leading Edge Wing Leading Edge Nose Radome Assy Wing Leading Edge LH I/B Flap RH I/B Flap Rt Aileron Lt External Fuel Tank Rt External Fuel Tank Pylon ? Synchrophaser Assy Synchrophaser Assy Heat Exchanger Heat Exchanger Jackscrew Assy, Flap Jackscrew Assy, Flap Fire Extinguisher (Bottle) Pneumatic Valve Anti Ice Valve Butterfly Valve Butterfly Valve Regulating Float Valve Speech Security Equipment Remote Control Unit Electrical Equip Rack Radio Set

Page 41

Qty

Turn-In/Ship

1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 7 7 1 1 20 1 5 1 1 1 1 1

Ship Ship Crate/Ship Turn-In Crate/Ship Crate/Ship Crate/Ship Crate/Ship Crate/Ship Crate/Ship Crate/Ship Crate/Ship Crate/Ship Ship Ship Ship Crate/Ship Crate/Ship Crate/Ship Turn-In Turn-In Turn-In Turn-In Crate/Ship Crate/Ship Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in

Shipping Location Robins AFB, GA Robins AFB, GA Robins AFB, GA LRAFB Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA LRAFB LRAFB LRAFB LRAFB Robins AFB, GA Robins AFB, GA LRAFB Robins AFB, GA Tinker AFB Tinker AFB Tinker AFB Tinker AFB LRAFB LRAFB Robins AFB, GA LRAFB

W900KK-10-T-0043 Attachment 1 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76

Amplifier Direction Control Radio Reciever Radio Reciever Radio Nav Receiver Radio Nav Receiver Radar Reciever Transmitter Reciever Transmitter Reciever Transmitter Reciever Radar Set Control Radar Data Computer Ground Collision Avoidance ETCAS Processor / GCA AN/APX-119 Rec Transmitter Radar Processor Countermeasure Receiver Countermeasure Receiver Countermeasures Dispenser Countermeasures Rec Control Countermeasures Processor Countermeasure Switching Unit AN/AAR-44A Signal Processor AN/AAR-44A Sensor Tuning Drive Power Supply Amplifier Amplifier Control Amplifier Detector Communications Modem Electromagnet Relay Electromagnet Relay Electrical Chassis Prop Deicer Contact Ring Assy Antenna Antenna Antenna Control Antenna Control Electronic Amplifier Power Supply Amplifier Circuit card Assy Circuit card Assy

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50 1 1 1 34 53 1 1 1 1 1 1 1 1 1 1 1 1 18 1 1 9 21 1 1 1 1 1 1 1 1 1 4 19 2 1 2 1 1 1 22

Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in

LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB LRAFB Robins AFB, GA Robins AFB, GA

W900KK-10-T-0043 Attachment 1 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117

Circuit card Assy Circuit card Assy Circuit card Assy Circuit card Assy Generator Control Unit Light Source Control Generator Stator Special Cable Assembly Light Indicating Panel Remote Magnetic Compensator Navigation Computer Flight Director Computer Flight Controller Flight Controller Airdrop Computer Antenna ATM A/C Generator Auto Pilot Box Auxilary Tank Bladder/Foam Clam Shells Cowlings Flight Data Accquisition Unit Fuel Qty Totalizer/Power Supply GTC Horse Collar Horzontal Stabilizer

1 7 6 2 4 1 1 1 1 1 1 1 1 1 1 7 2 1 2 4 1 1 1 4 1

Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Turn-in Crate/Ship Turn-in Turn-in Turn-in Crate/Ship Crate/Ship

I/B Flapp Comnnecting Links IFF KY5-5 RCU Lt Aileron Lt Elevator Mode "C" / Rt Cargo Mode "C" Data Converter Nose Radome Antenna Radio Reciever/Hog Trough Radio RT Receiver Transmitter Receiver Transmitter/Hog Trough Rt Elevator Rudder SKE/KY58 Computers TACAN Coupler

14 1 1 1 1 1 2 1 1 1 1 1 1 1

Crate/Ship Turn-in Turn-in Ship Ship Turn-in Turn-in Crate/Ship Turn-in Turn-in Turn-in Turn-in Ship Ship Turn-in Turn-in

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1

Robins AFB, GA Robins AFB, GA Robins AFB, GA Robins AFB, GA Tinker AFB San Antonio Tinker AFB Robins AFB, GA San Antonio Hill AFB Grand Rapids Tinker AFB Tinker AFB Tinker AFB LRAFB LRAFB LRAFB LRAFB LRAFB Robins AFB, GA LRAFB LRAFB LRAFB Robins AFB, GA Air Force Academy LRAFB LRAFB LRAFB Robins AFB, GA Robins AFB, GA LRAFB LRAFB Robins AFB, GA LRAFB LRAFB LRAFB LRAFB Robins AFB, GA Robins AFB, GA LRAFB LRAFB

W900KK-10-T-0043 Attachment 1 118 119 120

Transponder/Hog Trough Vertical Stabilizer

1 1

Turn-in Crate/Ship

Aircraft Wings

2

Ship

Total Components

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421

LRAFB Air Force Academy Robins AFB, GA

Attch_1_C-130_FuT_PWS

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